CN107985597A - A kind of shipping unmanned plane with modularization cargo hold - Google Patents
A kind of shipping unmanned plane with modularization cargo hold Download PDFInfo
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- CN107985597A CN107985597A CN201711067645.7A CN201711067645A CN107985597A CN 107985597 A CN107985597 A CN 107985597A CN 201711067645 A CN201711067645 A CN 201711067645A CN 107985597 A CN107985597 A CN 107985597A
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- cargo hold
- wing
- fuselage
- modularization
- unmanned plane
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- 238000009434 installation Methods 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 4
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005183 dynamical system Methods 0.000 description 2
- 238000012546 transfer Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/54—Floats
- B64C25/56—Floats inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/06—Fins
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/22—Taking-up articles from earth's surface
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
- B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C2009/005—Ailerons
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of shipping unmanned plane with modularization cargo hold, mainly including propeller, fuselage, parachute compartment, boxlike wing, modularization cargo hold, vertical fin, elevon, undercarriage, outer aileron, air bag cabin and rudder etc..The configuration of the present invention is simple, safe, cargo hold is easy to loading and unloading efficiently.Using boxlike wing configurations form, floor space is small, structural strength is high, can reduce the area of required aircraft gate in warehouse, meets that the transport of branch line efficient logistics requires；The versatility and high efficiency of unmanned plane logistics transportation can be improved using modularization cargo hold, make the sorting of cargo, handling and transport can efficiently, operate independently from.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, and in particular to a kind of shipping unmanned plane with modularization cargo hold.
Background technology
Current logistics and shipping company mainly use the shape of Automobile Transportation for medium or short range branch road transportation task inside the province
Formula is transported through and sends with charge free, due to being limited be subject to automobilism speed and driver's labour cost, this means of transportation when
Effect property and economy are poor.Therefore, many companies have the advantage of high efficiency and low cost using unmanned plane, appoint for logistics transportation
Logistics transportation unmanned plane is developed in business.Current express delivery unmanned plane is mainly multi-rotor unmanned aerial vehicle, such as " the Prime of Amazon Company
More rotor express mails of Air " multi-rotor unmanned aerial vehicles and suitable rich company send unmanned plane etc. with charge free, and this type unmanned plane is to be directed to express delivery most
Latter kilometer sends task research and development with charge free, generally can only once deliver a cargo, and there are cruising time is short, payload is small, boat
The problems such as journey is short.To solve the above-mentioned problems, the patent of Application No. 201620513151.1 disclose " a kind of express delivery nobody
Machine ", cruising time and the loading mass of unmanned plane is improved using fixed-wing normal arrangement form, by being arranged in middle fuselage
Dismountable cargo hold improves the warehousing space of unmanned plane.But its there are problems with：First, using middle fuselage integrally as
Cargo hold, first respectively must all dismantle wing, head and tail when loading and unloading goods, heavy workload and be difficult to realize efficient automatic
Makeup is unloaded；The wing of the express delivery unmanned plane uses the straight wing formula of high aspect ratio, takes up a large area, and is unfavorable for improving logistics workshop
Interior unmanned plane accommodates quantity；Express delivery unmanned plane inevitably can be by populated area in flight course, but the unmanned plane is simultaneously
The safety Design of unmanned plane is not accounted for, easily the security of the lives and property of ground staff is made after unmanned plane generation accident
Into threat.Therefore, it is necessary to develop a kind of brand-new unmanned plane to meet the actual demand of branch line logistics transportation task.
The content of the invention
For overcome the deficiencies in the prior art, the present invention provides a kind of shipping unmanned plane with modularization cargo hold, it is adopted
With boxlike wing distribution form, there is the modularization cargo hold of big volume in body upper installation, it is possible to achieve the automation of cargo hold is fast
Quick-mounting unloads, and improves conevying efficiency.
A kind of shipping unmanned plane with modularization cargo hold, it is characterised in that：Mainly include propeller (1), fuselage (2),
Parachute compartment (3), preceding wing (4), rear wing (5), modularization cargo hold (6), vertical fin (7), elevon (8), main landing gear
(9), outer aileron (10), end plate (11), nose-gear (12), forebody air bag cabin (13), rear body air bag cabin (14) and side
To rudder (15), wherein, the propeller (1) immediately ahead of fuselage (2) passes through drive shaft and the hair being installed in front of fuselage interior
Motivation connects, and undercarriage is installed on machine using nose-gear (12) in the posterior tricycle layout form of preceding, main landing gear (9)
Below body, vertical fin (7) is installed on above afterbody, and modularization cargo hold (6) is installed on above waist, parachute compartment (3)
It is installed on above fore-body, forebody air bag cabin (13) is installed on the front of nose-gear (12), rear body air bag cabin (14)
It is installed on the afterbody at main landing gear (9) rear.
The wing tip of the preceding wing (4) is connected with the wing tip of rear wing (5) by end plate (11), forms boxlike machine
The wing, wherein, preceding wing (4) is installed on below fore-body, and aspect ratio is 6~12, and angle of sweep is 10 °~30 °, and the upper counterangle is 0 °
~10 °, rear wing (5) is installed on above fuselage afterbody, and aspect ratio is 6~12, and sweepforward angle is 25 °~45 °, inverted diherdral for 0 °~
5°；The elevon (8) is installed on the posterior border position of preceding wing (4) and rear wing (5) close to fuselage side, for nobody
The manipulation of machine landing and in-flight pitch orientation；The outer aileron (10) is installed on preceding wing (4) and rear wing (5) is remote
The posterior border position of fuselage side；Elevon (8) and outer aileron (10) collective effect realize unmanned plane landing and in-flight horizontal stroke
To manipulation.
Rudder (15) is installed on rear side of the vertical fin (7), for unmanned plane landing and the in-flight manipulation in course.
The modularization cargo hold (6) uses rectangular parallelepiped, and for storing cargo, length is unmanned aerial vehicle body length
50%, width is the 90%~95% of fuselage width, highly 60%~80% for fuselage height；Modularization cargo hold (6) it is upper
Side is provided with the cargo hold handling auricle (16) for being moved and being loaded and unloaded to cargo hold, the front and rear sides point of modularization cargo hold (6)
Cargo hold for being connected fixation with fuselage is not installed and fixes auricle (17).
Be mounted in the forebody air bag cabin (13) and rear body air bag cabin (14) folding air bag and
Aerating device, when unmanned plane, which breaks down, needs forced landing, air bag is ejected and is inflated using aerating device；The air bag
Width after expansion is twice of fuselage width.
The beneficial effects of the invention are as follows：The configuration of the present invention is simple, safe, cargo hold is easy to loading and unloading efficiently, beneficial to realization
Automatic operating.Due to using fixed-wing form, it can meet that the transport of branch line efficient logistics requires；Boxlike wing configurations form accounts for
Ground area is small, structural strength is high, can reduce the area of required aircraft gate in warehouse, and that improves unmanned plane parks quantity；Pass through
The versatility and high efficiency of unmanned plane logistics transportation are improved using modularization cargo hold, makes the sorting, handling and transport of cargo equal
Can efficiently, operate independently from；The cargo hold of rectangular parallelepiped can improve the space availability ratio in warehouse easy to discharge.
Brief description of the drawings
Fig. 1 is a kind of structure diagram of shipping unmanned plane with modularization cargo hold of the present invention；
Fig. 2 is a kind of bottom view of shipping unmanned plane with modularization cargo hold of the present invention；
Fig. 3 is a kind of modularization cargo hold schematic diagram of shipping unmanned plane with modularization cargo hold of the present invention.
In figure, 1- propellers；2- fuselages；3- parachute compartments；Wing before 4-；Wing after 5-；6- modularization cargo holds；7- hangs down
Tail；8- elevons；9- main landing gears；10- outer ailerons；11- end plates；12- nose-gears；13- forebody air bags cabin；14-
Rear body air bag cabin；15- rudders；16- cargo holds load and unload auricle；17- cargo holds fix auricle.
Embodiment
The present invention is further described with reference to the accompanying drawings and examples, and the present invention includes but are not limited to following implementations
Example.
As depicted in figs. 1 and 2, a kind of shipping unmanned plane with modularization cargo hold of the present embodiment, mainly including spiral
It is paddle 1, fuselage 2, parachute compartment 3, preceding wing 4, rear wing 5, modularization cargo hold 6, vertical fin 7, elevon 8, main landing gear 9, outer
Side aileron 10, end plate 11, nose-gear 12, forebody air bag cabin 13, rear body air bag cabin 14, rudder 15.The middle part of fuselage 2
Section is rounded corner rectangle, is respectively forwardly tapered backward at head and tail；Propeller 1 is installed on the front position of fuselage 2
Put, be connected by drive shaft with the engine being installed on inside forebody, for producing the pulling force needed for unmanned plane during flying；Landing
Umbrella cabin 3 is installed on the anterior top of fuselage 2；Modularization cargo hold 6 is installed on the top at the middle part of fuselage 2；Vertical fin 7 is installed on fuselage 2
The top at rear portion；Forebody air bag cabin 13 and rear body air bag cabin 14 are respectively arranged in the front and rear of the lower section of fuselage 2；Rise and fall
Frame is installed on the lower section of fuselage 2 using nose-gear 12 in preceding, 9 posterior form of main landing gear, forms tricycle layout；Two
A preceding wing 4 is respectively arranged in 2 lower front both sides of fuselage, its aspect ratio is 8, and angle of sweep is 16 °, and the upper counterangle is 5 °；Two
Wing 5 is respectively arranged in both sides above fuselage afterbody afterwards, its aspect ratio is 8, and sweepforward angle is 35 °, and inverted diherdral is 1 °, machine behind left side
The wing tip of the wing and the wing tip of wing before the wing tip of wing behind the wing tip of wing, right side before left side and right side pass through 11 phase of end plate respectively
Connection, forms boxlike wing；Four elevons 8 are respectively arranged in preceding wing 4 and rear wing 5 close to the trailing edge position of fuselage side
Put；Four outer ailerons 10 are respectively arranged in the preceding posterior border position of wing 4 and rear wing 5 away from fuselage side；Rudder 15 is pacified
Rearward position loaded on vertical fin 7.
As shown in figure 3, modularization cargo hold 6 uses rectangular parallelepiped, length is the 50% of unmanned aerial vehicle body length, and width is
The 90% of fuselage width, highly 70% for fuselage height.The front side of modularization cargo hold 6 and rear side are separately installed with two cargo holds
Fixed auricle 17, cargo hold are fixed auricle 17 and are fixed for the connection of cargo hold and fuselage；The top center of modularization cargo hold 6 is provided with
Cargo hold loads and unloads auricle 16, and cargo hold handling auricle 16 is used to cargo hold is moved and loaded and unloaded.
Folding air bag and aerating device be installed, the width after airbag deployment is fuselage in the air bag cabin
Twice of width.
When performing cargo transport task, gantry is used in the shipping transfer workshop for be built in landing near airports first
The ancillary equipment such as hang auricle 16 is loaded and unloaded by cargo hold and the modularization cargo hold 6 for installing cargo to be transported is moved and lift into unmanned plane
The cargo hold installation site of the middle part of fuselage 2 top, modularization cargo hold 6 fix auricle 17 by four cargo holds set in its front and rear side
It is connected with unmanned aerial vehicle body 2 and fixed, the rotation of propeller 1 in 2 front of startup dynamical system driving fuselage, which produces pulling force, makes nobody
Machine slips into runway and accelerates to take off.Preceding wing 4 and rear wing 5 lift required when providing flight jointly for unmanned plane, wing lean on
The elevon 8 of the posterior border position installation of nearly fuselage side is used for unmanned plane landing and the in-flight manipulation of pitch orientation；Laterally
Flight control is relied on installed in the outer aileron 10 of posterior border position of the wing away from fuselage side and installed in wing close to fuselage
The elevon 8 of the posterior border position of side is completed jointly；Course flight control relies on the rudder 15 for being installed on the rear side of vertical fin 7.
Arrive at rear unmanned plane to drop to airport of destination and slip into neighbouring shipping transfer workshop, set using auxiliary such as gantry cranes
Standby to be sorted and sent with charge free by cargo hold handling auricle 16 by 6 unloading of modularization cargo hold and by its interior cargo, unmanned plane, which slips into, to stop
Seat in the plane, completes transport task.
When breaking down in unmanned plane in the air flight course or generation accident collision accident can not continue normal flight,
Dynamical system is closed, parachute, which is ejected and opened from parachute compartment 3, makes unmanned plane low speed fall, and closely face is dropped down onto under
When, two air bags eject simultaneously inflatable open from forebody air bag cabin 13 and rear body air bag cabin 14 respectively, when unmanned plane contacts
Air bag can play cushioning effect, protection unmanned plane and the safety for delivering cargo during ground.
Claims (1)
- A kind of 1. shipping unmanned plane with modularization cargo hold, it is characterised in that：Mainly include propeller (1), fuselage (2), drop Fall umbrella cabin (3), preceding wing (4), rear wing (5), modularization cargo hold (6), vertical fin (7), elevon (8), main landing gear (9), Outer aileron (10), end plate (11), nose-gear (12), forebody air bag cabin (13), rear body air bag cabin (14) and rudder (15), wherein, the propeller (1) immediately ahead of fuselage (2) passes through drive shaft and the engine being installed in front of fuselage interior Connection, undercarriage are installed under fuselage using nose-gear (12) in the posterior tricycle layout form of preceding, main landing gear (9) Side, vertical fin (7) are installed on above afterbody, and modularization cargo hold (6) is installed on above waist, parachute compartment (3) installation Above fore-body, forebody air bag cabin (13) is installed on the front of nose-gear (12), rear body air bag cabin (14) installation Afterbody in main landing gear (9) rear；The wing tip of the preceding wing (4) is connected with the wing tip of rear wing (5) by end plate (11), forms boxlike wing, its In, preceding wing (4) is installed on below fore-body, and aspect ratio is 6~12, and angle of sweep is 10 °~30 °, the upper counterangle for 0 °~ 10 °, rear wing (5) is installed on above fuselage afterbody, and aspect ratio is 6~12, and sweepforward angle is 25 °~45 °, inverted diherdral for 0 °~ 5°；The elevon (8) is installed on the posterior border position of preceding wing (4) and rear wing (5) close to fuselage side, for nobody The manipulation of machine landing and in-flight pitch orientation；The outer aileron (10) is installed on preceding wing (4) and rear wing (5) is remote The posterior border position of fuselage side；Elevon (8) and outer aileron (10) collective effect realize unmanned plane landing and in-flight horizontal stroke To manipulation；Rudder (15) is installed on rear side of the vertical fin (7), for unmanned plane landing and the in-flight manipulation in course；The modularization cargo hold (6) uses rectangular parallelepiped, and for storing cargo, length is unmanned aerial vehicle body length 50%, width is the 90%~95% of fuselage width, highly 60%~80% for fuselage height；Modularization cargo hold (6) it is upper Side is provided with the cargo hold handling auricle (16) for being moved and being loaded and unloaded to cargo hold, the front and rear sides point of modularization cargo hold (6) Cargo hold for being connected fixation with fuselage is not installed and fixes auricle (17)；Folding air bag and inflation are mounted in the forebody air bag cabin (13) and rear body air bag cabin (14) Device, when unmanned plane, which breaks down, needs forced landing, air bag is ejected and is inflated using aerating device；The airbag deployment Width afterwards is twice of fuselage width.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711067645.7A CN107985597A (en) | 2017-11-03 | 2017-11-03 | A kind of shipping unmanned plane with modularization cargo hold |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711067645.7A CN107985597A (en) | 2017-11-03 | 2017-11-03 | A kind of shipping unmanned plane with modularization cargo hold |
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| CN107985597A true CN107985597A (en) | 2018-05-04 |
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|---|---|---|---|
| CN201711067645.7A Pending CN107985597A (en) | 2017-11-03 | 2017-11-03 | A kind of shipping unmanned plane with modularization cargo hold |
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Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108725787A (en) * | 2018-07-19 | 2018-11-02 | 广州天狼航空科技发展有限公司 | Transport the unmanned plane of express delivery |
| CN109573078A (en) * | 2018-12-31 | 2019-04-05 | 江西冠通用飞机有限公司 | A kind of fixed wing aircraft shell with anti-unexpected function |
| CN109987223A (en) * | 2019-04-02 | 2019-07-09 | 夏季风 | A kind of new vertical landing unmanned plane coupling wing configuration |
| CN110228590A (en) * | 2019-06-30 | 2019-09-13 | 郑州航空工业管理学院 | A kind of detachable cargo hold connection wing twin fuselage logistics unmanned plane |
| CN111516867A (en) * | 2020-05-13 | 2020-08-11 | 陈厚然 | Multi-power-mode fixed-wing aircraft |
| CN111572773A (en) * | 2020-05-22 | 2020-08-25 | 中国民用航空飞行学院 | Medium-sized tactical transporter |
| CN112623186A (en) * | 2020-12-24 | 2021-04-09 | 中国航空工业集团公司西安飞机设计研究所 | Lift type statically stable airplane |
| CN113753217A (en) * | 2021-09-19 | 2021-12-07 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft configuration with mission cabin |
| US11767111B1 (en) | 2022-07-14 | 2023-09-26 | Wing Aviation Llc | Slotted receptacle for payload handle to secure payload within a UAV |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108725787B (en) * | 2018-07-19 | 2024-01-16 | 广州天狼航空科技发展有限公司 | Unmanned aerial vehicle for carrying express delivery |
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| CN109573078A (en) * | 2018-12-31 | 2019-04-05 | 江西冠通用飞机有限公司 | A kind of fixed wing aircraft shell with anti-unexpected function |
| CN109573078B (en) * | 2018-12-31 | 2024-01-30 | 江西冠一通用飞机有限公司 | Fixed wing aircraft casing with accident prevention function |
| CN109987223A (en) * | 2019-04-02 | 2019-07-09 | 夏季风 | A kind of new vertical landing unmanned plane coupling wing configuration |
| CN109987223B (en) * | 2019-04-02 | 2023-03-10 | 夏季风 | Novel VTOL unmanned aerial vehicle of hookup wing configuration |
| CN110228590A (en) * | 2019-06-30 | 2019-09-13 | 郑州航空工业管理学院 | A kind of detachable cargo hold connection wing twin fuselage logistics unmanned plane |
| CN111516867A (en) * | 2020-05-13 | 2020-08-11 | 陈厚然 | Multi-power-mode fixed-wing aircraft |
| CN111572773A (en) * | 2020-05-22 | 2020-08-25 | 中国民用航空飞行学院 | Medium-sized tactical transporter |
| CN111572773B (en) * | 2020-05-22 | 2024-08-27 | 中国民用航空飞行学院 | Medium-sized tactical transport plane |
| CN112623186A (en) * | 2020-12-24 | 2021-04-09 | 中国航空工业集团公司西安飞机设计研究所 | Lift type statically stable airplane |
| CN113753217A (en) * | 2021-09-19 | 2021-12-07 | 中国航空工业集团公司西安飞机设计研究所 | Aircraft configuration with mission cabin |
| US11767111B1 (en) | 2022-07-14 | 2023-09-26 | Wing Aviation Llc | Slotted receptacle for payload handle to secure payload within a UAV |
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Application publication date: 20180504 |