[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

WO2021196137A1 - Convenient protection box for unmanned aerial vehicle - Google Patents

Convenient protection box for unmanned aerial vehicle Download PDF

Info

Publication number
WO2021196137A1
WO2021196137A1 PCT/CN2020/083040 CN2020083040W WO2021196137A1 WO 2021196137 A1 WO2021196137 A1 WO 2021196137A1 CN 2020083040 W CN2020083040 W CN 2020083040W WO 2021196137 A1 WO2021196137 A1 WO 2021196137A1
Authority
WO
WIPO (PCT)
Prior art keywords
box body
wall
box cover
connecting plug
outer box
Prior art date
Application number
PCT/CN2020/083040
Other languages
French (fr)
Chinese (zh)
Inventor
杨思强
Original Assignee
南京达索航空科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 南京达索航空科技有限公司 filed Critical 南京达索航空科技有限公司
Publication of WO2021196137A1 publication Critical patent/WO2021196137A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U80/00Transport or storage specially adapted for UAVs
    • B64U80/70Transport or storage specially adapted for UAVs in containers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D25/00Details of other kinds or types of rigid or semi-rigid containers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D43/00Lids or covers for rigid or semi-rigid containers
    • B65D43/14Non-removable lids or covers
    • B65D43/16Non-removable lids or covers hinged for upward or downward movement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D81/00Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents
    • B65D81/02Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage
    • B65D81/05Containers, packaging elements, or packages, for contents presenting particular transport or storage problems, or adapted to be used for non-packaging purposes after removal of contents specially adapted to protect contents from mechanical damage maintaining contents at spaced relation from package walls, or from other contents
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D85/00Containers, packaging elements or packages, specially adapted for particular articles or materials
    • B65D85/68Containers, packaging elements or packages, specially adapted for particular articles or materials for machines, engines or vehicles in assembled or dismantled form

Definitions

  • the utility model belongs to the technical field of unmanned aerial vehicles, in particular to a convenient protective box for unmanned aerial vehicles.
  • the prior art mainly adopts a convenient protective box. Putting the drone into the protective box can not only improve the convenience of carrying the drone, but also reduce the risk of collision of the drone, thereby realizing the protection of the drone.
  • a convenient protective box for unmanned aerial vehicles is provided to solve the above-mentioned problems existing in the prior art.
  • a convenient protection box for unmanned aerial vehicles comprising: a protection box, a protection airbag arranged in the protection box, and an impact sensor arranged on the protection box;
  • the box covers are respectively provided with protective grooves for placing drones; the protective airbags are respectively arranged on the side inner wall, the bottom inner wall, and the top inner wall of the outer box cover; when the impact sensor detects the impact force, the protection The airbag pops up to fill the gap between the inner box body and the outer box body and the gap between the inner box cover and the outer box cover.
  • the number of the impact sensors is 14, and the impact sensors are respectively arranged on the 4 bottom corners of the outer box, the bottom surface of the outer box, the 4 sides of the outer box, and the outer box.
  • the connecting assembly includes a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel.
  • the inner wall of the surface is fixedly connected, and the end of the connecting plug away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top outer wall of the inner box cover, and a first ring shape is opened on the side inner wall of the connecting plug barrel.
  • the side wall of the connecting plunger is provided with a first annular protrusion adapted to the first annular groove; when the first annular protrusion on the connecting plunger is located in the first annular groove, the inner box Supported in the outer box body through the connecting component, while the inner box cover is connected to the outer box cover through the connecting component, the drone is housed in the protection groove of the inner box body and the inner box cover; when the protective box body is impacted, the airbag is protected Bounce and support the inner box body and the inner box cover, so that the first annular protrusion of the connecting insert rod is separated from the first annular groove of the connecting insert cylinder, so as to prevent the impact force of the protective box from being transmitted from the connecting component to the inner box The body and the inner box cover cause damage to the drone.
  • the connecting assembly includes a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel.
  • the inner wall of the surface is fixedly connected, and the end of the connecting plug away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top outer wall of the inner box cover, and the side inner wall of the connecting plug barrel is provided with a second ring shape
  • the side wall of the connecting rod is provided with a second annular groove that is adapted to the second annular protrusion; when the protective box body is impacted, the protective airbag bounces and causes the inner box body and the inner box cover
  • the support enables the realization of the connection component to be detached, and prevents the impact force of the protection box from being transmitted from the connection component to the inner box body and the inner box cover, thereby protecting the drone.
  • connection assembly includes a connection plug barrel and a connection plug rod inserted into the connection plug barrel, and the end of the connection plug barrel away from the connection plug rod is connected to the inner wall of the bottom surface of the outer box body or the outer box cover.
  • the inner wall of the top surface is fixedly connected, and the end of the connecting plug far away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top outer wall of the inner box cover, and a magnet is fixed in the connecting plug barrel.
  • the connecting plunger is made of stainless steel; when the protective box is impacted, the protective airbag bounces and supports the inner box and the inner box cover, so that the connecting plunger is separated from the magnet to avoid the impact of the protective box It is conducted from the connecting components to the inner box body and the inner box cover to protect the drone. .
  • the inner box body and the inner box cover are made of foam material, and the foam has certain elasticity.
  • the inner box made of foam material The body and inner box cover can reduce the risk of damage to the drone.
  • Fig. 2 is a cross-sectional view of the protective box when the airbag of the present invention is closed.
  • Fig. 3 is a cross-sectional view of the protective box of the present invention when the airbag bounces.
  • Fig. 4 is a schematic diagram of the structure of the connecting assembly of the first embodiment of the present invention.
  • Fig. 5 is a schematic diagram of the structure of the connecting assembly of the second embodiment of the present invention.
  • Fig. 6 is a schematic diagram of the structure of the connecting assembly of the third embodiment of the present invention.
  • the reference signs are: protective box body 10, outer box body 11, outer box cover 12, inner box body 13, inner box cover 14, gap 15, protective groove 16, protective airbag 20, impact sensor 30, connection assembly 40, connection Insert barrel 41, first annular groove 411, second annular protrusion 412, connecting plunger 42, first annular protrusion 421, second annular groove 422, magnet 43, chamfer 44.
  • the present invention provides a convenient protection box for drones.
  • the convenient protection box for drones includes a protective box body 10, a protective airbag 20 and an impact sensor 30.
  • the protective box body 10 includes an outer box body 11, an outer box cover 12, an inner box body 13, and an inner box cover 14.
  • the outer box body 11 and the outer box cover 12 are connected by a hinge.
  • the outer box cover 12 can be opened or closed relative to the outer box body 11.
  • the outer box cover 12 When the outer box cover 12 is closed relative to the outer box body 11, the outer box cover 12 And the outer box body 11 constitute a complete box body.
  • the inner box body 13 is arranged in the outer box body 11, and the inner box cover 14 is arranged in the outer box cover 12.
  • the size of the inner box body 13 is smaller than the size of the outer box body 11, and a gap 15 is left between the inner box body 13 and the outer box body 11.
  • the size of the inner box cover 14 is smaller than the size of the outer box cover 12, and the inner box cover 14 is provided in the outer box cover 12.
  • the bottom outer wall of the inner box 13 and the bottom inner wall of the outer box 11 and the top outer wall of the inner box cover 14 and the top inner wall of the outer box cover 12 are connected by a detachable connecting component 40.
  • the inner box body 13 has a protection groove 16 for placing the drone from the top surface to the bottom surface
  • the inner box cover 14 has a protection groove 16 for placing the drone from the bottom surface to the top surface.
  • Both the inner box body 13 and the inner box cover 14 are made of foam materials. When the drone is put into the protective slot 16 or taken out, the drone will rub against the inner box body 13 or the inner box cover 14 or Collision, because the foam material has a certain degree of elasticity, it can reduce the risk of damage to the drone.
  • the number of protective airbags 20 is six, which are respectively provided on the four side inner walls of the outer box 11, the bottom inner wall of the outer box 11, and the top inner wall of the outer box cover 12.
  • the protective airbag 20 has two states: closed and bounced. When the protective box 10 is not impacted, the protective airbag 20 is in the closed state; when the protective box 10 is impacted, the protective airbag 20 is in the bounced state, and the protective airbag 20 rapidly expands and fills into the gap 15 between the inner box body 13 and the outer box body 11 and between the outer box cover 12 and the inner box cover 14 to protect the inner box body 13 and the inner box cover 14 when the airbag 20 is inflated Squeeze to disengage the connecting assembly 40, and the impact force received by the outer box body 11 or the outer box cover 12 cannot be transmitted to the inner box body 13 or the inner box cover 14, thereby effectively protecting the drone in the protection slot 16 .
  • the protective airbag 20 will squeeze the inner box body 13 and the inner box cover 14, thereby detaching the connecting assembly 40.
  • the opening end of the inner box 13 is There is a certain distance between the open end of the outer box body 11 and the open end of the inner box cover 14 to the open end of the outer box cover 12.
  • the inner box body There is a gap between the open end of 13 and the open end of the outer box body 11.
  • the 14 impact sensors 30 are respectively arranged on the 4 bottom corners of the outer box 11, the center of the bottom of the outer box 11, the 4 sides of the outer box 11, and the 4 top sides of the outer box cover 12. The corners and the center of the top surface of the outer box cover 12.
  • the impact sensor 30 is in communication connection with the trigger of the protection airbag 20.
  • the 14 impact sensors 30 can detect the impact received by the protective box 10 from multiple directions. When the impact sensor 30 detects that the impact intensity is greater than the set value, the trigger of the protective airbag 20 is quickly triggered to quickly open the protective airbag 20 , So as to actively protect the drone in the protective box 10.
  • the impact sensor 30 in this embodiment adopts a pressure sensor model MPX2102, the pressure value range of the pressure sensor is 100KPa, and the measurement accuracy is ⁇ 1%.
  • the connecting assembly 40 includes a connecting plug 41 and a connecting plug 42, and the connecting plug 42 is inserted into the connecting plug 41.
  • One end of the connecting plug barrel 41 away from the connecting plug rod 42 is fixedly connected to the inner wall of the bottom surface of the outer box body 11 or the inner wall of the top surface of the outer box cover 12.
  • One end of the connecting plug rod 42 away from the connecting plug cylinder 41 is fixedly connected to the bottom outer wall of the inner box body 13 or the top outer wall of the inner box cover 14.
  • a first annular groove 411 is formed on the inner wall of the side of the connecting plug barrel 41, and a first annular protrusion 421 that fits with the first annular groove 411 is provided on the side wall of the connecting plug rod 42.
  • the inner box body 13 When the first annular protrusion 421 on the connecting rod 42 is located in the annular groove, the inner box body 13 is supported in the outer box body 11 through the connecting assembly 40, and the inner box cover 14 is connected to the outer box cover 12 through the connecting assembly 40. .
  • the drone is housed in the inner box body 13 and the protective groove 16 of the inner box cover 14.
  • the protective airbag 20 bounces and squeezes and supports the inner box 13 and the inner lid 14 to make the connecting rod 42
  • the first annular protrusion 421 is disengaged from the first annular groove 411 of the connecting plug barrel 41, and the impact force received on the outer box body 11 or the outer box cover 12 cannot be transmitted to the inner box body 13 or the inner box cover 14 through the connecting assembly 40 , So as to form an active protection for the UAV and reduce the risk of damage to the UAV.
  • the connecting assembly 40 includes a connecting plug 41 and a connecting plug 42, and the connecting plug 42 is inserted into the connecting plug 41.
  • One end of the connecting plug barrel 41 away from the connecting plug rod 42 is fixedly connected to the inner wall of the bottom surface of the outer box body 11 or the inner wall of the top surface of the outer box cover 12.
  • One end of the connecting plug rod 42 away from the connecting plug cylinder 41 is fixedly connected to the bottom outer wall of the inner box body 13 or the top outer wall of the inner box cover 14.
  • a second annular protrusion 412 is provided on the inner wall of the side of the connecting plug barrel 41, and a second annular groove 422 that is adapted to the second annular protrusion 412 is opened on the side wall of the connecting plug 42.
  • the working principle is similar to that of Embodiment 1.
  • the connecting rod 42 is far away from the connecting tube 41, the second annular protrusion 412 is separated from the second annular groove 422, and the outer box 11 or the outer box
  • the impact force received on the cover 12 cannot be transmitted to the inner box body 13 or the inner box cover 14 through the connecting assembly 40, thereby reducing the risk of damage to the drone.
  • the connecting assembly 40 includes a connecting plug 41 and a connecting plug 42, and the connecting plug 42 is inserted into the connecting plug 41.
  • One end of the connecting plug barrel 41 away from the connecting plug rod 42 is fixedly connected to the inner wall of the bottom surface of the outer box body 11 or the inner wall of the top surface of the outer box cover 12.
  • One end of the connecting plug rod 42 away from the connecting plug cylinder 41 is fixedly connected to the bottom outer wall of the inner box body 13 or the top outer wall of the inner box cover 14.
  • a magnet 43 is fixed on the inner wall of the bottom of the connecting plug barrel 41, and the connecting plug 42 is made of stainless steel.
  • the protective airbag 20 bounces to disengage the end of the connecting rod 42 from the magnet 43, thereby preventing the impact force received on the outer box body 11 or the outer box cover 12 from being transmitted to the inner box through the connecting assembly 40 On the box body 13 or the inner box cover 14 to form active protection for the drone.
  • the end of the connecting plug 41 close to the connecting pin 42 and the end of the connecting plug 42 close to the connecting plug 41 are both There is a chamfer 44.
  • the connecting rod 42 can be inserted into the connecting plug barrel 41 very conveniently through the guidance of the chamfer 44, thereby improving the convenience of assembling the protective box.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Transportation (AREA)
  • Buffer Packaging (AREA)

Abstract

A convenient protection box for an unmanned aerial vehicle, the box comprising a protection box body (10), protection air bags (20) provided in the protection box body and an impact sensor provided on the protection box body. The protection box body comprises an outer box body (11), an outer box cover (12) hinged to the outer box body, an inner box body (13) provided in the outer box body and an inner box cover (14) provided in the outer box cover. A gap (15) is left between the inner box body and the outer box body, and a gap is left between the inner box cover and the outer box cover. The outer wall of a bottom surface of the inner box body is connected to the inner wall of a bottom surface of the outer box body and the outer wall of a top surface of the inner box cover is connected to the inner wall of a top surface of the outer box cover by means of detachable connection assemblies, and protection slots (16) for accommodating the unmanned aerial vehicle are provided in the inner box body and the inner box cover respectively. The protection air bags are respectively provided on the inner walls of both of a side surface and the bottom surface of the outer box body, and on the inner wall of the top surface of the outer box cover. When the impact sensor detects an impact force, the protection air bag pops up to fill the gap between the inner box body and the outer box body and the gap between the inner box cover and the outer box cover. The convenient protection box for the unmanned aerial vehicle can effectively protect the unmanned aerial vehicle when the protection box receives impact, thereby reducing the risk of damage to the unmanned aerial vehicle.

Description

一种无人机便捷保护箱Convenient protection box for unmanned aerial vehicle 技术领域Technical field
本实用新型属于无人机技术领域,尤其是一种无人机便捷保护箱。 The utility model belongs to the technical field of unmanned aerial vehicles, in particular to a convenient protective box for unmanned aerial vehicles.
背景技术Background technique
无人驾驶飞机简称无人机,是利用无线电遥控设备和自备程序控制装置操纵的不载人飞机。无人机作为一种新概念设备,具有机动灵活、反应迅速、无人飞行以及易于操作的有点,被广泛运用与气象、勘探、摄影等领域。Unmanned aircraft is abbreviated as unmanned aerial vehicle, which is an unmanned aircraft operated by radio remote control equipment and self-provided program control devices. As a new concept equipment, UAV has the advantages of flexibility, rapid response, unmanned flight and easy operation. It is widely used in meteorology, exploration, photography and other fields.
由于无人机的各个部件极易损坏,尤其是旋翼以及摄像装置,一旦发生碰撞很容易造成无人机的损坏,为了解决这一问题,现有技术中主要采用便捷式保护箱的方式,将无人机放入保护箱内,既能提升携带无人机的便利性同时还可以降低无人机发生碰撞的风险,从而实现对无人机的保护。Since the various components of the drone are extremely easy to damage, especially the rotor and the camera device, once a collision occurs, it is easy to cause damage to the drone. In order to solve this problem, the prior art mainly adopts a convenient protective box. Putting the drone into the protective box can not only improve the convenience of carrying the drone, but also reduce the risk of collision of the drone, thereby realizing the protection of the drone.
但是,在无人机在运输过程中车辆经过颠簸路段以及在保护箱不慎跌落时,保护箱会受到一定的冲击力,这种硬性的冲击力会通过保护箱传导至无人机上,造成无人机部件的损坏。However, when the vehicle passes through a bumpy road during the transportation of the UAV and when the protection box accidentally falls, the protection box will receive a certain impact force. This rigid impact force will be transmitted to the UAV through the protection box, causing no damage. Damage to man-machine parts.
技术问题technical problem
提供一种无人机便捷保护箱,以解决现有技术存在的上述问题。A convenient protective box for unmanned aerial vehicles is provided to solve the above-mentioned problems existing in the prior art.
技术解决方案Technical solutions
一种无人机便捷保护箱,包括:保护箱体、设于保护箱体内的保护气囊以及设于保护箱体上的冲击传感器;所述保护箱体包括外箱体、与外箱体铰接的外箱盖、设于外箱体内的内箱体以及设于外箱盖内的内箱盖,所述内箱体和外箱体之间留有空隙,所述内箱盖和外箱盖之间留有空隙,所述内箱体底面外壁和外箱体底面内壁之间以及内箱盖顶面外壁和外箱盖顶面内壁之间通过可拆卸连接组件连接,所述内箱体和内箱盖分别开有放置无人机的保护槽;所述保护气囊,分别设于外箱体的侧面内壁、底面内壁以及外箱盖的顶面内壁;所述冲击传感器检测到冲击力时,保护气囊弹开填充内箱体和外箱体之间的空隙以及内箱盖和外箱盖之间的空隙。A convenient protection box for unmanned aerial vehicles, comprising: a protection box, a protection airbag arranged in the protection box, and an impact sensor arranged on the protection box; The outer box cover, the inner box body arranged in the outer box body, and the inner box cover arranged in the outer box cover, there is a gap between the inner box body and the outer box body, and the inner box cover and the outer box cover A gap is left between the bottom surface of the inner box body and the bottom surface of the outer box body, and between the top surface of the inner box cover and the top surface of the outer box cover are connected by detachable connecting components. The box covers are respectively provided with protective grooves for placing drones; the protective airbags are respectively arranged on the side inner wall, the bottom inner wall, and the top inner wall of the outer box cover; when the impact sensor detects the impact force, the protection The airbag pops up to fill the gap between the inner box body and the outer box body and the gap between the inner box cover and the outer box cover.
在进一步的实施例中,所述冲击传感器的数量为14个,所述冲击传感器分别设于外箱体的4个底部边角部、外箱体的底面、外箱体的4个侧面、外箱盖的4个顶部边角部以及外箱盖的顶面;通过此设置使得冲击传感器能够从多个方向检测到保护箱体受到的冲击,从而促使保护气囊迅速打开保护内箱体中的无人机。In a further embodiment, the number of the impact sensors is 14, and the impact sensors are respectively arranged on the 4 bottom corners of the outer box, the bottom surface of the outer box, the 4 sides of the outer box, and the outer box. The four top corners of the box cover and the top surface of the outer box cover; through this setting, the impact sensor can detect the impact of the protective box from multiple directions, thereby prompting the protective airbag to quickly open to protect the inner box. Man-machine.
在进一步的实施例中,所述连接组件包括连接插筒以及插于连接插筒的连接插杆,所述连接插筒远离连接插杆的一端与外箱体的底面内壁或外箱盖的顶面内壁面固定连接,所述连接插杆远离连接插筒的一端与内箱体的底面外壁或内箱盖的顶面外壁面固定连接,所述连接插筒的侧面内壁上开有第一环形槽,所述连接插杆的侧面壁上设有一个与第一环形槽适配的第一环形凸起;当连接插杆上的第一环形凸起位于第一环形槽内时,内箱体通过连接组件支撑于外箱体中,同时内箱盖通过连接组件与外箱盖连接,无人机收容于内箱体和内箱盖的保护槽内;当保护箱体受到冲击时,保护气囊弹开并对内箱体和内箱盖进行支撑,使连接插杆的第一环形凸起从连接插筒的第一环形槽脱离,避免保护箱体受到的冲击力从连接组件传导至内箱体和内箱盖上造成无人机的损坏。In a further embodiment, the connecting assembly includes a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel. The inner wall of the surface is fixedly connected, and the end of the connecting plug away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top outer wall of the inner box cover, and a first ring shape is opened on the side inner wall of the connecting plug barrel. Groove, the side wall of the connecting plunger is provided with a first annular protrusion adapted to the first annular groove; when the first annular protrusion on the connecting plunger is located in the first annular groove, the inner box Supported in the outer box body through the connecting component, while the inner box cover is connected to the outer box cover through the connecting component, the drone is housed in the protection groove of the inner box body and the inner box cover; when the protective box body is impacted, the airbag is protected Bounce and support the inner box body and the inner box cover, so that the first annular protrusion of the connecting insert rod is separated from the first annular groove of the connecting insert cylinder, so as to prevent the impact force of the protective box from being transmitted from the connecting component to the inner box The body and the inner box cover cause damage to the drone.
在进一步的实施例中,所述连接组件包括连接插筒以及插于连接插筒的连接插杆,所述连接插筒远离连接插杆的一端与外箱体的底面内壁或外箱盖的顶面内壁面固定连接,所述连接插杆远离连接插筒的一端与内箱体的底面外壁或内箱盖的顶面外壁面固定连接,所述连接插筒的侧面内壁上设有第二环形凸起,所述连接插杆的侧面壁上开有一个与第二环形凸起适配的第二环形槽;当保护箱体受到冲击时,保护气囊弹开并对内箱体和内箱盖支撑,使连接组件的实现脱离,避免保护箱体的受到的冲击力从连接组件传导至内箱体和内箱盖,对无人机进行保护。In a further embodiment, the connecting assembly includes a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel. The inner wall of the surface is fixedly connected, and the end of the connecting plug away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top outer wall of the inner box cover, and the side inner wall of the connecting plug barrel is provided with a second ring shape The side wall of the connecting rod is provided with a second annular groove that is adapted to the second annular protrusion; when the protective box body is impacted, the protective airbag bounces and causes the inner box body and the inner box cover The support enables the realization of the connection component to be detached, and prevents the impact force of the protection box from being transmitted from the connection component to the inner box body and the inner box cover, thereby protecting the drone.
在进一步的实施例中,所述连接组件包括连接插筒以及插于连接插筒的连接插杆,所所述连接插筒远离连接插杆的一端与外箱体的底面内壁或外箱盖的顶面内壁面固定连接,所述连接插杆远离连接插筒的一端与内箱体的底面外壁或内箱盖的顶面外壁面固定连接,所述连接插筒内固定有一块磁铁,所述连接插杆为采用不锈钢材质制成;当保护箱体受到冲击时,保护气囊弹开并对内箱体和内箱盖支撑,使连接插杆与磁铁脱离,避免保护箱体的受到的冲击力从连接组件传导至内箱体和内箱盖,对无人机进行保护。。In a further embodiment, the connection assembly includes a connection plug barrel and a connection plug rod inserted into the connection plug barrel, and the end of the connection plug barrel away from the connection plug rod is connected to the inner wall of the bottom surface of the outer box body or the outer box cover. The inner wall of the top surface is fixedly connected, and the end of the connecting plug far away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top outer wall of the inner box cover, and a magnet is fixed in the connecting plug barrel. The connecting plunger is made of stainless steel; when the protective box is impacted, the protective airbag bounces and supports the inner box and the inner box cover, so that the connecting plunger is separated from the magnet to avoid the impact of the protective box It is conducted from the connecting components to the inner box body and the inner box cover to protect the drone. .
在进一步的实施例中,所述连接插筒靠近连接插杆的端部以及连接插杆靠近连接插筒的端部均开有倒角,通过设置倒角,便于连接插杆插入连接插筒内,提升保护箱装配时的便利性。In a further embodiment, the end of the connecting plug barrel near the connecting plug and the end of the connecting plug near the connecting plug barrel are chamfered. By setting the chamfer, it is convenient for the connecting plug to be inserted into the connecting plug barrel. , Improve the convenience of the protective box assembly.
在进一步的实施例中,所述内箱体和内箱盖采用泡沫材质制成,泡沫具有一定的弹性,无人机与内箱体或内箱盖之间发生碰撞时,泡沫材质的内箱体和内箱盖能够降低无人机损坏的风险。In a further embodiment, the inner box body and the inner box cover are made of foam material, and the foam has certain elasticity. When the drone collides with the inner box body or the inner box cover, the inner box made of foam material The body and inner box cover can reduce the risk of damage to the drone.
有益效果Beneficial effect
本实用新型提供的无人机便捷保护箱包括:保护箱体、保护气囊以及冲击传感器。其中,保护箱体包括外箱体、外箱盖、内箱体和内箱盖。内箱体和外箱体之间以及内箱盖和外箱盖之间通过可拆卸的连接组件连接。当冲击传感器检测到保护箱体受到的冲击力,保护气囊迅速打开填充至内箱体和外箱体以及内箱盖和外箱盖之间的空隙,并使连接组件脱离连接,避免外箱体或外箱盖受到的冲击力通过连接组件传导至内箱体和内箱盖上,从而实现对无人机的保护。与现有技术相比,本实用新型提供的无人机便捷保护箱能够在保护箱受到冲击时对无人机进行有效的保护,降低无人机损坏的风险。The convenient protection box for unmanned aerial vehicles provided by the utility model includes a protection box body, a protection airbag and an impact sensor. Among them, the protective box body includes an outer box body, an outer box cover, an inner box body and an inner box cover. The inner box body and the outer box body and between the inner box cover and the outer box cover are connected by detachable connecting components. When the impact sensor detects the impact force received by the protective box, the protective airbag quickly opens and fills the gap between the inner box and the outer box, and the inner box cover and the outer box cover, and disconnects the connecting components to avoid the outer box. Or the impact force received by the outer box cover is transmitted to the inner box body and the inner box cover through the connecting component, thereby realizing the protection of the drone. Compared with the prior art, the convenient protective box for drones provided by the utility model can effectively protect the drone when the protective box is impacted, and reduce the risk of damage to the drone.
附图说明Description of the drawings
图1是本实用新型的无人机便捷保护箱的结构示意图。Figure 1 is a schematic diagram of the structure of the utility model's convenient protection box for unmanned aerial vehicles.
图2是本实用新型的气囊闭合时的保护箱的剖视图。Fig. 2 is a cross-sectional view of the protective box when the airbag of the present invention is closed.
图3是本实用新型的气囊弹开时的保护箱的剖视图。Fig. 3 is a cross-sectional view of the protective box of the present invention when the airbag bounces.
图4是本实用新型的实施例1的连接组件的结构示意图。Fig. 4 is a schematic diagram of the structure of the connecting assembly of the first embodiment of the present invention.
图5是本实用新型的实施例2的连接组件的结构示意图。Fig. 5 is a schematic diagram of the structure of the connecting assembly of the second embodiment of the present invention.
图6是本实用新型的实施例3的连接组件的结构示意图。Fig. 6 is a schematic diagram of the structure of the connecting assembly of the third embodiment of the present invention.
附图标记为:保护箱体10、外箱体11、外箱盖12、内箱体13、内箱盖14、空隙15、保护槽16、保护气囊20、冲击传感器30、连接组件40、连接插筒41、第一环形槽411、第二环形凸起412、连接插杆42、第一环形凸起421、第二环形槽422、磁铁43、倒角44。The reference signs are: protective box body 10, outer box body 11, outer box cover 12, inner box body 13, inner box cover 14, gap 15, protective groove 16, protective airbag 20, impact sensor 30, connection assembly 40, connection Insert barrel 41, first annular groove 411, second annular protrusion 412, connecting plunger 42, first annular protrusion 421, second annular groove 422, magnet 43, chamfer 44.
本发明的实施方式Embodiments of the present invention
在下文的描述中,给出了大量具体的细节以便提供对本实用新型更为彻底的理解。然而,对于本领域技术人员而言显而易见的是,本实用新型可以无需一个或多个这些细节而得以实施。在其他的例子中,为了避免与本实用新型发生混淆,对于本领域公知的一些技术特征未进行描述。In the following description, a lot of specific details are given in order to provide a more thorough understanding of the present invention. However, it is obvious to those skilled in the art that the present invention can be implemented without one or more of these details. In other examples, in order to avoid confusion with the present invention, some technical features known in the art are not described.
经研究人员研究发现,无人机应用极其广泛。由于无人机的零部件极易损坏,为了防止无人机损坏,通常将无人机放入便携式保护箱内,既能提高携带的便利性也能对无人机进行保护。但是在无人机运输过程中,尤其是车辆经过颠簸路段或者使用者使用不当造成保护箱跌落时,保护箱会受到冲击,这种硬性冲击会通过保护箱传导无人机上,造成无人机零部件的损坏。因此如何对保护箱进行改进,降低无人机收到的冲击,成为亟需解决的问题。Researchers have found that UAVs are extremely widely used. Since the parts of the drone are extremely easy to damage, in order to prevent the drone from being damaged, the drone is usually placed in a portable protective box, which can not only improve the convenience of carrying but also protect the drone. However, during the transportation of the drone, especially when the vehicle passes through a bumpy road or the protective box is dropped due to improper use by the user, the protective box will be impacted. This hard impact will be transmitted to the drone through the protective box, causing zero damage to the drone. Damage to components. Therefore, how to improve the protective box and reduce the impact received by the drone has become an urgent problem to be solved.
为了解决上述问题,本实用新型提供一种无人机便捷保护箱,如图1至图3所示,该无人机便捷保护箱包括:保护箱体10、保护气囊20以及冲击传感器30。In order to solve the above problems, the present invention provides a convenient protection box for drones. As shown in FIGS. 1 to 3, the convenient protection box for drones includes a protective box body 10, a protective airbag 20 and an impact sensor 30.
结合图1和图2,保护箱体10包括外箱体11、外箱盖12内箱体13以及内箱盖14。其中,外箱体11和外箱盖12之间通过铰链连接,外箱盖12可相对于外箱体11打开或者闭合,当外箱盖12相对于外箱体11闭合时,外箱盖12和外箱体11构成一个完整的箱体。内箱体13设于外箱体11内,内箱盖14设于外箱盖12内。内箱体13的尺寸小于外箱体11的尺寸,内箱体13和外箱体11之间留有空隙15。内箱盖14的尺寸小于外箱盖12的尺寸,内箱盖14设于外箱盖12中。内箱体13底面外壁和外箱体11底面内壁之间以及内箱盖14顶面外壁和外箱盖12顶面内壁之间通过可拆卸连接组件40连接。内箱体13自顶面向底面开有放置无人机的保护槽16,同时内箱盖14自底面向顶面开有放置无人机的保护槽16。放置无人机时,先将无人机放入内箱体13的保护槽16内,然后将外箱盖12闭合,使无人机的顶部部件置于内箱盖14的保护槽16内。内箱体13和内箱盖14均采用泡沫材料制成,在将无人机放入保护槽16或者将无人机取出时,无人机会与内箱体13或内箱盖14发生摩擦或者碰撞,由于泡沫材料具有一定的弹性,能够降低无人机损坏的风险。1 and 2, the protective box body 10 includes an outer box body 11, an outer box cover 12, an inner box body 13, and an inner box cover 14. Wherein, the outer box body 11 and the outer box cover 12 are connected by a hinge. The outer box cover 12 can be opened or closed relative to the outer box body 11. When the outer box cover 12 is closed relative to the outer box body 11, the outer box cover 12 And the outer box body 11 constitute a complete box body. The inner box body 13 is arranged in the outer box body 11, and the inner box cover 14 is arranged in the outer box cover 12. The size of the inner box body 13 is smaller than the size of the outer box body 11, and a gap 15 is left between the inner box body 13 and the outer box body 11. The size of the inner box cover 14 is smaller than the size of the outer box cover 12, and the inner box cover 14 is provided in the outer box cover 12. The bottom outer wall of the inner box 13 and the bottom inner wall of the outer box 11 and the top outer wall of the inner box cover 14 and the top inner wall of the outer box cover 12 are connected by a detachable connecting component 40. The inner box body 13 has a protection groove 16 for placing the drone from the top surface to the bottom surface, and the inner box cover 14 has a protection groove 16 for placing the drone from the bottom surface to the top surface. When placing the drone, first put the drone into the protection slot 16 of the inner box 13 and then close the outer box cover 12 so that the top part of the drone is placed in the protection slot 16 of the inner box cover 14. Both the inner box body 13 and the inner box cover 14 are made of foam materials. When the drone is put into the protective slot 16 or taken out, the drone will rub against the inner box body 13 or the inner box cover 14 or Collision, because the foam material has a certain degree of elasticity, it can reduce the risk of damage to the drone.
结合图2和图3,保护气囊20的数量为6个,分别设于外箱体11的4个侧面内壁、外箱体11的底面内壁以及外箱盖12的顶面内壁。所述保护气囊20存在闭合和弹开两种状态,当保护箱体10未受到冲击时,保护气囊20处于闭合状态;当保护箱体10受到冲击时,保护气囊20处于弹开状态,保护气囊20迅速膨胀并填充至内箱体13和外箱体11之间以及外箱盖12和内箱盖14之间的空隙15内,保护气囊20膨胀时对内箱体13和内箱盖14形成挤压,使连接组件40脱离,外箱体11或外箱盖12受到的冲击力无法传导至内箱体13或者内箱盖14上,从而对保护槽16内的无人机进行有效的保护。在保护气囊20膨胀过程中,保护气囊20会对内箱体13以及内箱盖14形成挤压,从而使连接组件40脱离,为了便于连接组件40的完全脱离,内箱体13的开口端到外箱体11的开口端设有一定的距离,内箱盖14的开口端到外箱盖12的开口端设有一定的距离,当外箱体11和外箱盖12闭合时,内箱体13的开口端与外箱体11的开口端留有间隙,当保护气囊20挤压内箱体13和内箱盖14时,内箱体13和内箱盖14相向运动,从而便于连接组件40的有效脱离。2 and 3, the number of protective airbags 20 is six, which are respectively provided on the four side inner walls of the outer box 11, the bottom inner wall of the outer box 11, and the top inner wall of the outer box cover 12. The protective airbag 20 has two states: closed and bounced. When the protective box 10 is not impacted, the protective airbag 20 is in the closed state; when the protective box 10 is impacted, the protective airbag 20 is in the bounced state, and the protective airbag 20 rapidly expands and fills into the gap 15 between the inner box body 13 and the outer box body 11 and between the outer box cover 12 and the inner box cover 14 to protect the inner box body 13 and the inner box cover 14 when the airbag 20 is inflated Squeeze to disengage the connecting assembly 40, and the impact force received by the outer box body 11 or the outer box cover 12 cannot be transmitted to the inner box body 13 or the inner box cover 14, thereby effectively protecting the drone in the protection slot 16 . During the expansion of the protective airbag 20, the protective airbag 20 will squeeze the inner box body 13 and the inner box cover 14, thereby detaching the connecting assembly 40. In order to facilitate the complete detachment of the connecting assembly 40, the opening end of the inner box 13 is There is a certain distance between the open end of the outer box body 11 and the open end of the inner box cover 14 to the open end of the outer box cover 12. When the outer box body 11 and the outer box cover 12 are closed, the inner box body There is a gap between the open end of 13 and the open end of the outer box body 11. When the protective airbag 20 squeezes the inner box body 13 and the inner box cover 14, the inner box body 13 and the inner box cover 14 move towards each other, thereby facilitating the connection of the assembly 40 Effective detachment.
结合图2和图3,冲击传感器30的数量为14个,均设于保护箱体10上。具体的,这14个冲击传感器30分别设于外箱体11的4个底部边角部、外箱体11的底面中心、外箱体11的4个侧面、外箱盖12的4个顶部边角部以及外箱盖12的顶面中心。冲击传感器30与保护气囊20的触发器通讯连接。这14个冲击传感器30能够从多个方向对保护箱体10受到的冲击进行检测,当冲击传感器30检测到冲击强度大于设定值时,保护气囊20的触发器迅速触发使保护气囊20迅速打开,从而对保护箱体10内的无人机进行主动保护。本实施例中的冲击传感器30采用型号为MPX2102压力传感器,该压力传感器的压力值范围为100KPa,测量精度为±1%。With reference to FIGS. 2 and 3, there are 14 impact sensors 30, all of which are provided on the protective box 10. Specifically, the 14 impact sensors 30 are respectively arranged on the 4 bottom corners of the outer box 11, the center of the bottom of the outer box 11, the 4 sides of the outer box 11, and the 4 top sides of the outer box cover 12. The corners and the center of the top surface of the outer box cover 12. The impact sensor 30 is in communication connection with the trigger of the protection airbag 20. The 14 impact sensors 30 can detect the impact received by the protective box 10 from multiple directions. When the impact sensor 30 detects that the impact intensity is greater than the set value, the trigger of the protective airbag 20 is quickly triggered to quickly open the protective airbag 20 , So as to actively protect the drone in the protective box 10. The impact sensor 30 in this embodiment adopts a pressure sensor model MPX2102, the pressure value range of the pressure sensor is 100KPa, and the measurement accuracy is ±1%.
实施例1:结合图2至图4,连接组件40包括连接插筒41和连接插杆42,连接插杆42插于连接插筒41内。连接插筒41远离连接插杆42的一端与外箱体11的底面内壁或外箱盖12的顶面内壁面固定连接。连接插杆42远离连接插筒41的一端与内箱体13的底面外壁或内箱盖14的顶面外壁面固定连接。连接插筒41的侧面内壁上开有第一环形槽411,连接插杆42的侧面壁上设有一个与第一环形槽411适配的第一环形凸起421。当连接插杆42上的第一环形凸起421位于环形槽内时,内箱体13通过连接组件40支撑于外箱体11中,同时内箱盖14通过连接组件40与外箱盖12连接。无人机收容于内箱体13和内箱盖14的保护槽16内。当保护箱体10受到冲击时,冲击传感器30检测到冲击强度大于设定的强度时,保护气囊20弹开并对内箱体13和内箱盖14进行挤压支撑,使连接插杆42的第一环形凸起421从连接插筒41的第一环形槽411脱离,外箱体11或者外箱盖12上受到的冲击力无法通过连接组件40传导至内箱体13或者内箱盖14上,从而对无人机形成主动保护,降低无人机损坏的风险。Embodiment 1: With reference to FIGS. 2 to 4, the connecting assembly 40 includes a connecting plug 41 and a connecting plug 42, and the connecting plug 42 is inserted into the connecting plug 41. One end of the connecting plug barrel 41 away from the connecting plug rod 42 is fixedly connected to the inner wall of the bottom surface of the outer box body 11 or the inner wall of the top surface of the outer box cover 12. One end of the connecting plug rod 42 away from the connecting plug cylinder 41 is fixedly connected to the bottom outer wall of the inner box body 13 or the top outer wall of the inner box cover 14. A first annular groove 411 is formed on the inner wall of the side of the connecting plug barrel 41, and a first annular protrusion 421 that fits with the first annular groove 411 is provided on the side wall of the connecting plug rod 42. When the first annular protrusion 421 on the connecting rod 42 is located in the annular groove, the inner box body 13 is supported in the outer box body 11 through the connecting assembly 40, and the inner box cover 14 is connected to the outer box cover 12 through the connecting assembly 40. . The drone is housed in the inner box body 13 and the protective groove 16 of the inner box cover 14. When the protective box 10 is impacted, and the impact sensor 30 detects that the impact strength is greater than the set strength, the protective airbag 20 bounces and squeezes and supports the inner box 13 and the inner lid 14 to make the connecting rod 42 The first annular protrusion 421 is disengaged from the first annular groove 411 of the connecting plug barrel 41, and the impact force received on the outer box body 11 or the outer box cover 12 cannot be transmitted to the inner box body 13 or the inner box cover 14 through the connecting assembly 40 , So as to form an active protection for the UAV and reduce the risk of damage to the UAV.
实施例2:结合图2、图3和图5,连接组件40包括连接插筒41和连接插杆42,连接插杆42插于连接插筒41内。连接插筒41远离连接插杆42的一端与外箱体11的底面内壁或外箱盖12的顶面内壁面固定连接。连接插杆42远离连接插筒41的一端与内箱体13的底面外壁或内箱盖14的顶面外壁面固定连接。连接插筒41的侧面内壁上设有第二环形凸起412,连接插杆42的侧面壁上开有一个与第二环形凸起412适配的第二环形槽422。其工作原理与实施例1类似,当保护箱体10受到冲击时,连接插杆42远离连接插筒41,第二环形凸起412从第二环形槽422内脱离,外箱体11或者外箱盖12上受到的冲击力无法通过连接组件40传导至内箱体13或者内箱盖14上,从而降低无人机损坏的风险。Embodiment 2: With reference to FIGS. 2, 3 and 5, the connecting assembly 40 includes a connecting plug 41 and a connecting plug 42, and the connecting plug 42 is inserted into the connecting plug 41. One end of the connecting plug barrel 41 away from the connecting plug rod 42 is fixedly connected to the inner wall of the bottom surface of the outer box body 11 or the inner wall of the top surface of the outer box cover 12. One end of the connecting plug rod 42 away from the connecting plug cylinder 41 is fixedly connected to the bottom outer wall of the inner box body 13 or the top outer wall of the inner box cover 14. A second annular protrusion 412 is provided on the inner wall of the side of the connecting plug barrel 41, and a second annular groove 422 that is adapted to the second annular protrusion 412 is opened on the side wall of the connecting plug 42. The working principle is similar to that of Embodiment 1. When the protective box 10 is impacted, the connecting rod 42 is far away from the connecting tube 41, the second annular protrusion 412 is separated from the second annular groove 422, and the outer box 11 or the outer box The impact force received on the cover 12 cannot be transmitted to the inner box body 13 or the inner box cover 14 through the connecting assembly 40, thereby reducing the risk of damage to the drone.
实施例3:结合图2、图3和图6,连接组件40包括连接插筒41和连接插杆42,连接插杆42插于连接插筒41内。连接插筒41远离连接插杆42的一端与外箱体11的底面内壁或外箱盖12的顶面内壁面固定连接。连接插杆42远离连接插筒41的一端与内箱体13的底面外壁或内箱盖14的顶面外壁面固定连接。连接插筒41的底部内壁固定有一块磁铁43,同时,连接插杆42采用不锈钢材质制成。当保护箱体10受到冲击时,保护气囊20弹开使连接插杆42的端部与磁铁43脱离,从而避免外箱体11或者外箱盖12上受到的冲击力通过连接组件40传导至内箱体13或者内箱盖14上,进而对无人机形成主动保护。Embodiment 3: In combination with FIGS. 2, 3 and 6, the connecting assembly 40 includes a connecting plug 41 and a connecting plug 42, and the connecting plug 42 is inserted into the connecting plug 41. One end of the connecting plug barrel 41 away from the connecting plug rod 42 is fixedly connected to the inner wall of the bottom surface of the outer box body 11 or the inner wall of the top surface of the outer box cover 12. One end of the connecting plug rod 42 away from the connecting plug cylinder 41 is fixedly connected to the bottom outer wall of the inner box body 13 or the top outer wall of the inner box cover 14. A magnet 43 is fixed on the inner wall of the bottom of the connecting plug barrel 41, and the connecting plug 42 is made of stainless steel. When the protective box body 10 is impacted, the protective airbag 20 bounces to disengage the end of the connecting rod 42 from the magnet 43, thereby preventing the impact force received on the outer box body 11 or the outer box cover 12 from being transmitted to the inner box through the connecting assembly 40 On the box body 13 or the inner box cover 14 to form active protection for the drone.
结合图4至图6,为了提升保护箱装配时的便利性,在进一步的实施例中,连接插筒41靠近连接插杆42的端部以及连接插杆42靠近连接插筒41的端部均开有倒角44。在保护箱体10装配时,通过倒角44的引导能够极为便利的将连接插杆42插入连接插筒41内,从而提升保护箱装配的便利性。4 to 6, in order to improve the convenience of the assembly of the protective box, in a further embodiment, the end of the connecting plug 41 close to the connecting pin 42 and the end of the connecting plug 42 close to the connecting plug 41 are both There is a chamfer 44. When the protective box body 10 is assembled, the connecting rod 42 can be inserted into the connecting plug barrel 41 very conveniently through the guidance of the chamfer 44, thereby improving the convenience of assembling the protective box.
以上结合附图详细描述了本实用新型的优选实施方式,但是,本实用新型并不限于上述实施方式中的具体细节,在本实用新型的技术构思范围内,可以对本实用新型的技术方案进行多种等同变换,这些等同变换均属于本实用新型的保护范围。The preferred embodiments of the present utility model are described in detail above with reference to the accompanying drawings. However, the present utility model is not limited to the specific details in the above-mentioned embodiments. Within the scope of the technical concept of the present utility model, various technical solutions of the present utility model can be made. These equivalent transformations all belong to the protection scope of the present invention.

Claims (7)

  1. 一种无人机便捷保护箱,其特征在于,包括:保护箱体、设于保护箱体内的保护气囊以及设于保护箱体上的冲击传感器;所述保护箱体包括外箱体、与外箱体铰接的外箱盖、设于外箱体内的内箱体以及设于外箱盖内的内箱盖,所述内箱体和外箱体之间留有空隙,所述内箱盖和外箱盖之间留有空隙,所述内箱体底面外壁和外箱体底面内壁之间以及内箱盖顶面外壁和外箱盖顶面内壁之间通过可拆卸连接组件连接,所述内箱体和内箱盖分别开有放置无人机的保护槽;所述保护气囊,分别设于外箱体的侧面内壁、底面内壁以及外箱盖的顶面内壁;所述冲击传感器检测到冲击力时,保护气囊弹开填充内箱体和外箱体之间的空隙以及内箱盖和外箱盖之间的空隙。 A convenient protective box for drones, which is characterized by comprising: a protective box, a protective air bag arranged in the protective box, and an impact sensor arranged on the protective box; the protective box includes an outer box, and an outer box. The outer box cover hinged to the box body, the inner box body arranged in the outer box body, and the inner box cover arranged in the outer box cover, a gap is left between the inner box body and the outer box body, and the inner box cover and A gap is left between the outer box cover, and the outer wall of the bottom surface of the inner box body and the inner wall of the bottom surface of the outer box body, and the outer wall of the top surface of the inner box cover and the inner wall of the top surface of the outer box cover are connected by detachable connecting components. The box body and the inner box cover are respectively provided with protective grooves for placing the drone; the protective airbags are respectively arranged on the side inner wall, the bottom inner wall and the top inner wall of the outer box cover; the impact sensor detects the impact When the force is applied, the protective airbag bounces to fill the gap between the inner box body and the outer box body and the gap between the inner box cover and the outer box cover.
  2. 根据权利要求1所述的保护箱,其特征在于,所述冲击传感器的数量为14个,所述冲击传感器分别设于外箱体的4个底部边角部、外箱体的底面、外箱体的4个侧面、外箱盖的4个顶部边角部以及外箱盖的顶面。 The protective box according to claim 1, wherein the number of the impact sensors is 14, and the impact sensors are respectively arranged on the four bottom corners of the outer box, the bottom surface of the outer box, and the outer box. The 4 sides of the body, the 4 top corners of the outer box cover, and the top surface of the outer box cover.
  3. 根据权利要求1所述的保护箱,其特征在于,所述连接组件包括连接插筒以及插于连接插筒的连接插杆,所述连接插筒远离连接插杆的一端与外箱体的底面内壁或外箱盖的顶面内壁面固定连接,所述连接插杆远离连接插筒的一端与内箱体的底面外壁或内箱盖的顶面外壁面固定连接,所述连接插筒的侧面内壁上开有第一环形槽,所述连接插杆的侧面壁上设有一个与第一环形槽适配的第一环形凸起。 The protective box according to claim 1, wherein the connecting assembly comprises a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel, and an end of the connecting plug barrel away from the connecting plug rod and the bottom surface of the outer box body The inner wall or the inner wall surface of the top surface of the outer box cover is fixedly connected, the end of the connecting rod away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top surface outer wall surface of the inner box cover, and the side surface of the connecting plug barrel A first annular groove is opened on the inner wall, and a first annular protrusion adapted to the first annular groove is provided on the side wall of the connecting plunger.
  4. 根据权利要求1所述的保护箱,其特征在于,所述连接组件包括连接插筒以及插于连接插筒的连接插杆,所述连接插筒远离连接插杆的一端与外箱体的底面内壁或外箱盖的顶面内壁面固定连接,所述连接插杆远离连接插筒的一端与内箱体的底面外壁或内箱盖的顶面外壁面固定连接,所述连接插筒的侧面内壁上设有第二环形凸起,所述连接插杆的侧面壁上开有一个与第二环形凸起适配的第二环形槽。 The protective box according to claim 1, wherein the connecting assembly comprises a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel, and an end of the connecting plug barrel away from the connecting plug rod and the bottom surface of the outer box body The inner wall or the inner wall surface of the top surface of the outer box cover is fixedly connected, the end of the connecting rod away from the connecting plug barrel is fixedly connected with the bottom outer wall of the inner box body or the top surface outer wall surface of the inner box cover, and the side surface of the connecting plug barrel A second annular protrusion is provided on the inner wall, and a second annular groove adapted to the second annular protrusion is opened on the side wall of the connecting rod.
  5. 根据权利要求1所述的保护箱,其特征在于,所述连接组件包括连接插筒以及插于连接插筒的连接插杆,所所述连接插筒远离连接插杆的一端与外箱体的底面内壁或外箱盖的顶面内壁面固定连接,所述连接插杆远离连接插筒的一端与内箱体的底面外壁或内箱盖的顶面外壁面固定连接,所述连接插筒内固定有一块磁铁,所述连接插杆为采用不锈钢材质制成。 The protective box according to claim 1, wherein the connecting assembly includes a connecting plug barrel and a connecting plug rod inserted into the connecting plug barrel, and an end of the connecting plug barrel away from the connecting plug rod is connected to the outer box body. The inner wall of the bottom surface or the inner wall surface of the top surface of the outer box cover is fixedly connected, and the end of the connecting rod away from the connecting plug barrel is fixedly connected with the outer wall of the bottom surface of the inner box body or the top surface of the inner box cover. A magnet is fixed, and the connecting rod is made of stainless steel.
  6. 根据权利要求3-5任一项所述的保护箱,其特征在于,所述连接插筒靠近连接插杆的端部以及连接插杆靠近连接插筒的端部均开有倒角。 The protective box according to any one of claims 3 to 5, wherein the end of the connecting plug cylinder close to the connecting plug rod and the end of the connecting plug rod close to the connecting plug cylinder are chamfered.
  7. 根据权利要求1所述的保护箱,其特征在于,所述内箱体和内箱盖采用泡沫材质制成。 The protective box according to claim 1, wherein the inner box body and the inner box cover are made of foam material.
PCT/CN2020/083040 2020-03-31 2020-04-02 Convenient protection box for unmanned aerial vehicle WO2021196137A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN202020446396.3U CN211970349U (en) 2020-03-31 2020-03-31 Convenient guard box of unmanned aerial vehicle
CN202020446396.3 2020-03-31

Publications (1)

Publication Number Publication Date
WO2021196137A1 true WO2021196137A1 (en) 2021-10-07

Family

ID=73382842

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2020/083040 WO2021196137A1 (en) 2020-03-31 2020-04-02 Convenient protection box for unmanned aerial vehicle

Country Status (2)

Country Link
CN (1) CN211970349U (en)
WO (1) WO2021196137A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114604529A (en) * 2022-03-18 2022-06-10 云南体育运动职业技术学院 Unmanned aerial vehicle simulated training device based on simulation platform

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113086384A (en) * 2021-02-19 2021-07-09 深圳供电局有限公司 Unmanned aerial vehicle transportation mount
CN113277233A (en) * 2021-05-21 2021-08-20 浙江德欧化工制造有限公司 Solid airtight feeding device for disperse red 3B production
CN117963313A (en) * 2024-03-29 2024-05-03 四川省天域航通科技有限公司 Parachute-free air drop box for large-sized fixed wing unmanned aerial vehicle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2500934A1 (en) * 1981-02-27 1982-09-03 Barringer Research Ltd Drogue tower by aircraft for geophysical surveying - is coated with layer of soft flexible material to reduce noise induced in sensor by vibration of bird
CN105217406A (en) * 2015-09-26 2016-01-06 梁纲 The inner box body device with air bag
KR20170017365A (en) * 2015-08-06 2017-02-15 장성훈 Air Bag of Drone or Quad Cop for safe Landing
CN106576980A (en) * 2016-11-30 2017-04-26 深圳前海弘稼科技有限公司 Planting device and protection method for falling of planting device
CN107554792A (en) * 2017-07-25 2018-01-09 南昌航空大学 A kind of unmanned aerial vehicle onboard equipment safety case
CN210063362U (en) * 2019-01-10 2020-02-14 山东鸿鹄测绘科技有限公司 Protection device convenient to unmanned aerial vehicle transportation

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2500934A1 (en) * 1981-02-27 1982-09-03 Barringer Research Ltd Drogue tower by aircraft for geophysical surveying - is coated with layer of soft flexible material to reduce noise induced in sensor by vibration of bird
KR20170017365A (en) * 2015-08-06 2017-02-15 장성훈 Air Bag of Drone or Quad Cop for safe Landing
CN105217406A (en) * 2015-09-26 2016-01-06 梁纲 The inner box body device with air bag
CN106576980A (en) * 2016-11-30 2017-04-26 深圳前海弘稼科技有限公司 Planting device and protection method for falling of planting device
CN107554792A (en) * 2017-07-25 2018-01-09 南昌航空大学 A kind of unmanned aerial vehicle onboard equipment safety case
CN210063362U (en) * 2019-01-10 2020-02-14 山东鸿鹄测绘科技有限公司 Protection device convenient to unmanned aerial vehicle transportation

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114604529A (en) * 2022-03-18 2022-06-10 云南体育运动职业技术学院 Unmanned aerial vehicle simulated training device based on simulation platform

Also Published As

Publication number Publication date
CN211970349U (en) 2020-11-20

Similar Documents

Publication Publication Date Title
WO2021196137A1 (en) Convenient protection box for unmanned aerial vehicle
US10266245B2 (en) Folding heavy-lift unmanned aerial vehicle frame
US8770840B2 (en) Airbag structure with inner shade cover and manufacturing method thereof
CN206407121U (en) Multi-rotor unmanned aerial vehicle structure
TWI755051B (en) Parachute device for drone and method for opening parachute thereof
CN207060411U (en) A kind of anti-high-altitude dropping device of unmanned plane
CN207454851U (en) It is a kind of to be applied to the explosion-proof vent valve with metallic rupture disk on new-energy automobile
CN110341961A (en) A kind of unmanned plane loading mechanism
AU2017391876B2 (en) Battery and mobile terminal
WO2019019357A1 (en) Accompanying flight backpack for unmanned aerial vehicle and accompanying flight system for unmanned aerial vehicle
CN210592446U (en) Unmanned aerial vehicle cargo hold that can put in
CN208291475U (en) Unmanned plane skeleton and unmanned plane
CN210126718U (en) Foldable packing box
CN211507603U (en) Electronic component packaging structure
KR102229766B1 (en) Build material containers
CN214932319U (en) Unmanned aerial vehicle strorage device
CN210503909U (en) Convenient portable unmanned aerial vehicle anticollision shock attenuation transport case
CN209410320U (en) A kind of hollow vertical touching lever fold mechanism
CN208165494U (en) Buffer packing case
CN106144194A (en) Packing box based on unmanned plane
JP3220853U (en) Foldable club protective cover
CN217554577U (en) Reusable finished board packaging box
CN215795559U (en) Cosmetic packaging box with good sealing effect
CN109264213A (en) A kind of multifunctional packing box
JP2004033363A (en) Protective cover of golf club

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 20929644

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 20929644

Country of ref document: EP

Kind code of ref document: A1

122 Ep: pct application non-entry in european phase

Ref document number: 20929644

Country of ref document: EP

Kind code of ref document: A1

32PN Ep: public notification in the ep bulletin as address of the adressee cannot be established

Free format text: NOTING OF LOSS OF RIGHTS PURSUANT TO RULE 112(1) EPC (EPO FORM 1205A DATED 17.05.2023)

122 Ep: pct application non-entry in european phase

Ref document number: 20929644

Country of ref document: EP

Kind code of ref document: A1