CN210942265U - Novel aerial commodity circulation of puting in transports unmanned aerial vehicle - Google Patents
Novel aerial commodity circulation of puting in transports unmanned aerial vehicle Download PDFInfo
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- CN210942265U CN210942265U CN201921780214.XU CN201921780214U CN210942265U CN 210942265 U CN210942265 U CN 210942265U CN 201921780214 U CN201921780214 U CN 201921780214U CN 210942265 U CN210942265 U CN 210942265U
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Abstract
The utility model provides a novel aerial delivery logistics transportation unmanned aerial vehicle, which comprises a body, a nose, wings and a plurality of rotors; the top of aircraft nose with the front end of fuselage is articulated, the end of fuselage is equipped with the V-arrangement fin, the wing symmetry sets up the both sides of fuselage, the wing with the fuselage is integrated into one piece, the lower extreme of wing still is equipped with two straight-bars, the both ends of straight-bar respectively are equipped with a rotor, be equipped with control system in the aircraft nose, the utility model discloses a wing fuses with the fuselage mutually, conventional fuselage storing cabin, the unmanned aerial vehicle that has V-arrangement fin structural style, and still is equipped with the rotor in the below of wing, has fully combined two types of commodity circulation unmanned aerial vehicle's advantage, has increased the stability of unmanned aerial vehicle's storing space and organism, can also carry out the accurate piece of throwing when guaranteeing high-speed transportation, has improved the transportation speed of commodity circulation, has promoted unmanned aerial vehicle's duration, has improved the degree of accuracy that the article were put in.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a novel aerial commodity circulation transportation unmanned aerial vehicle of puting in.
Background
At present, the unmanned aerial vehicle technology has great development in stability, endurance and load capacity, and can also be used in rapid air logistics transportation in provinces, islands, plateaus and regions with underdeveloped traffic, the types of unmanned aerial vehicles used in the current logistics are generally multi-rotor unmanned aerial vehicles and fixed-wing unmanned aerial vehicles, and the two unmanned aerial vehicles also have defects, the multi-rotor unmanned aerial vehicles have flexible performance, can realize quite complex and accurate flight motion, and can realize vertical take-off and landing and air hovering, which makes the space requirements and restrictions on take-off and landing smaller, and makes the positions of parts sent by the multi-rotor unmanned aerial vehicles more accurate, but because of the low energy conversion rate of rotors, the endurance time and flight distance are quite restricted, and the flight speed is low, while the fixed-wing unmanned aerial vehicles have high energy utilization rate, and because of the principle of generating lift force, can reach very high flying speed, but its difficult complicated and accurate flight motion of realizing, can't realize VTOL and hover in the air, make the easy deviation in position of its commodity circulation of puting in, not accurate, the storing space of fuselage is also less moreover, and the storing is also few, because the completion commodity circulation that existence commodity circulation unmanned aerial vehicle of defect also can't be faster, more accurate is carried.
SUMMERY OF THE UTILITY MODEL
The technique that exists is not enough to the aforesaid, the utility model aims at providing a novel commodity circulation transportation unmanned aerial vehicle is put in air, fuse mutually for wing and fuselage, conventional fuselage storing cabin, the unmanned aerial vehicle that has V-arrangement fin structural style, and still be equipped with the rotor in the below of wing, two kinds of commodity circulation unmanned aerial vehicle's advantage has fully been combined, unmanned aerial vehicle's storing space and the stability of organism have been enlarged, effectual solution transport speed is low, the time of endurance is short, throw a not accurate problem.
In order to solve the technical problem, the utility model adopts the following technical scheme:
a novel unmanned aerial vehicle for aerial delivery logistics transportation comprises a body, a nose, wings and a plurality of rotors; the aircraft nose articulates the front end in the fuselage, the front end both sides of fuselage respectively are equipped with an electronic hydraulic press, the hydraulic stem of electronic hydraulic press with the aircraft nose is articulated, the end of fuselage is equipped with the V-arrangement fin, uses the V-arrangement fin to be convenient for reduce the interference resistance of air to the organism when putting in, the wing symmetry sets up in the both sides of fuselage, the wing with the fuselage is integrated into one piece, forms the structural style that the wing fuses with the fuselage, is convenient for increase the space of organism storing, the lower extreme of wing is fixed and is equipped with two-generation turboprop engine, still be equipped with a plurality of oil tank in the wing, the end of fuselage still is equipped with the propulsion propeller that promotes the generator and with promotion generator electric connection, the lower extreme of fuselage is equipped with the undercarriage, the commodity circulation cabin has been seted up in the fuselage, the commodity circulation under-cabin is equipped with, the both sides of fuselage respectively are equipped with a straight-bar, the both ends of straight-bar respectively are equipped with a rotor, be equipped with control system in the aircraft nose, control system includes controller, wireless communication device, a plurality of display, be equipped with infrared imaging device and 4 high definition digtal cameras on the outer wall of aircraft nose, electronic hydraulic press double-turbine propeller engine promote the generator the rotor infrared imaging device high definition digtal cameras the display hoisting apparatus respectively with controller electric connection, the controller passes through wireless communication device and user terminal communication connection.
Preferably, the controller is a main control MCU, and the wireless communication device is OFDM.
Preferably, the user terminal is a computer.
Preferably, a throwing cabin door is arranged on the logistics cabin and electrically connected with the controller.
Preferably, the display includes with last screen, well screen, the screen down that the controller is connected, go up the screen and be the HUD screen, well screen is used for showing flight plan and position, gives consideration to the mission planning and the route operation of aircraft, and the screen is the operation instruction interface down, shows information such as diversion, height, speed adjustment.
Preferably, an inner supporting beam is arranged in the wing.
Preferably, the landing gear is a rear three-point landing gear.
Preferably, the hoisting device is a small overhead crane.
Preferably, the infrared imaging device is an infrared thermal imager.
The beneficial effects of the utility model reside in that: this design fuses mutually for wing and fuselage, conventional fuselage storing cabin, the unmanned aerial vehicle that has V-arrangement fin structural style, and still be equipped with the rotor in the below of wing, two types of commodity circulation unmanned aerial vehicle's advantage has fully been combined, unmanned aerial vehicle's storing space and the stability of organism have been increased, can also carry out the accurate piece of throwing when guaranteeing high-speed transportation, the transport speed of commodity circulation has been improved, unmanned aerial vehicle's duration has been promoted, the degree of accuracy that the article was put in is improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is a schematic structural view of a novel unmanned aerial vehicle for aerial logistics transportation provided by an embodiment of the present invention;
fig. 2 is a top view of a novel unmanned aerial vehicle for aerial logistics transportation provided by an embodiment of the present invention;
fig. 3 is a schematic view of a bottom view structure of a novel aerial logistics transportation unmanned aerial vehicle;
fig. 4 is a schematic position diagram of an electric hydraulic press of a novel aerial delivery logistics transportation unmanned aerial vehicle.
Description of reference numerals:
1-machine head, 2-machine body, 3-wing, 4-V-shaped empennage, 5-rotor wing, 6-double-engine turboprop engine, 7-propulsion propeller, 8-undercarriage, 9-straight rod, 10-electric hydraulic machine, 11-oil tank, 12-logistics cabin and 13-overhead crane.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
As shown in fig. 1 to 3, a novel aerial delivery logistics transportation unmanned aerial vehicle comprises a fuselage 2, a nose 1, wings 3, and four rotors 5; the aircraft nose 1 is hinged at the front end of the aircraft nose 2, two sides of the front end of the aircraft nose 2 are respectively provided with an electric hydraulic machine 10, a hydraulic rod of the electric hydraulic machine 10 is hinged with the aircraft nose 1, the opening and closing of the aircraft nose can be controlled by the electric hydraulic machine 10, the tail end of the aircraft nose 2 is provided with a V-shaped tail wing 4, the V-shaped tail wing 4 is used for reducing the interference resistance of air to an engine body when the aircraft nose is thrown in, the wings 3 are symmetrically arranged at two sides of the aircraft nose 2, the wings 3 and the aircraft nose 2 are integrally formed, a structural form that the wings 3 and the aircraft nose 2 are fused can be formed, the space for storing the engine body is convenient to increase, the lower end of each wing 3 is fixedly provided with a double-engine turboprop engine 6, when goods are thrown in a hovering fixed point, the airflow on the lower surface of the wings 3 can be corrected, the fuel oil storage is greatly increased, the improvement of the cruising ability of the unmanned aerial vehicle is facilitated, the tail end of the machine body 2 is also provided with a push generator and a propulsion propeller 7 electrically connected with the push generator, when goods are thrown in at a hovering fixed point, the airflow on the lower surfaces of the wings 3 can be corrected and weakened to separate, the pneumatic efficiency is improved, the transportation speed of the unmanned aerial vehicle is also improved, the transportation time is saved, the lower end of the machine body 2 is provided with an undercarriage 8, a logistics cabin 12 is arranged in the machine body 2, the logistics cabin 12 is used for storing parcels to be transported, a conventional machine body cargo hold can be used, a hoisting device is arranged in the logistics cabin 12, a small-sized suspension type crane 13 is used for picking up and throwing in a fixed point the parcels in the logistics cabin, two sides of the machine body 2 are respectively provided with a straight rod 9, two ends of the straight rod 9, the machine head 1 is internally provided with a control system which comprises a controller, a wireless communication device and a plurality of displays, wherein the controller is a main control MCU, the wireless communication device is OFDM, the outer wall of the machine head 1 is provided with an infrared imaging device and four high-definition cameras, the infrared imaging device is an infrared thermal imager, the electric hydraulic machine 10, the double-engine turboprop engine 6, the push generator, the rotor wing 5, the infrared thermal imager, the high-definition camera, the display and the hoisting device are respectively and electrically connected with the main control MCU, accessible main control MCU adjusts and monitors the component part on to unmanned aerial vehicle to ensure unmanned aerial vehicle's stable transportation, main control MCU passes through OFDM and is connected with the computer, and user's accessible computer carries out real-time control to unmanned aerial vehicle.
Furthermore, a throwing cabin door is arranged on the logistics cabin 12 and electrically connected with the main control MCU, and when the designated place is reached, the main control MCU opens the throwing cabin door to throw the dispatch at a fixed point.
Further, the display include with last screen, well screen, the screen down that the controller is connected, it is the HUD screen to go up the screen, and well screen is used for showing flight plan and position, considers mission planning and the route operation of aircraft, and the screen is the operating instruction interface down, shows information such as change of course, height, speed adjustment.
Further, an inner supporting beam is arranged in the wing 3, and plays a role in supporting and fixing the wing 3.
Further, the undercarriage 8 is a rear three-point undercarriage, which facilitates rapid loading and unloading of goods.
During the use, control electric hydraulic press 10 opens the bottom of aircraft nose 1, load and unload the group spare in to commodity circulation cabin 12, closed aircraft nose 1, master control MCU control unmanned aerial vehicle navigates along appointed route, when arriving appointed place, four rotor 5 of master control MCU control make unmanned aerial vehicle hover or low latitude descend in the air, master control MCU control throws in the hatch door and opens, master control MCU control suspension type hoist 13 picks up appointed group spare and throws in it with fixed point, close and throw in the hatch door, control unmanned aerial vehicle through computer monitoring master control MCU and continue to carry the group spare or return to navigate.
The utility model provides a design fuses mutually for wing and fuselage, conventional fuselage storing cabin, the unmanned aerial vehicle that has V-arrangement fin structural style, and still be equipped with the rotor in the below of wing, two types of commodity circulation unmanned aerial vehicle's advantage has fully been combined, unmanned aerial vehicle's storing space and the stability of organism have been increased, can also carry out the accurate piece of throwing when guaranteeing high-speed transportation, the transport speed of commodity circulation has been improved, unmanned aerial vehicle's duration has been promoted, the degree of accuracy that the article was put in is improved.
It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (9)
1. A novel unmanned aerial vehicle for aerial delivery logistics transportation is characterized by comprising a body, a nose, wings and a plurality of rotors; the top of aircraft nose with the front end of fuselage is articulated, the front end both sides of fuselage respectively are equipped with an electronic hydraulic press, electronic hydraulic press's hydraulic stem with the aircraft nose is articulated, the end of fuselage is equipped with the V-arrangement fin, the wing symmetry sets up the both sides of fuselage, the wing with the fuselage is integrated into one piece, the fixed double-generator turboprop engine that is equipped with of lower extreme of wing, the lower extreme of wing still is equipped with two straight-bars, the both ends of straight-bar respectively are equipped with a rotor, still be equipped with a plurality of oil tank in the wing, the end of fuselage still is equipped with the propelling generator and with propelling generator electric connection's propulsion screw, the lower extreme of fuselage is equipped with the undercarriage, the commodity circulation cabin has been seted up in the fuselage, be equipped with hoisting apparatus in the commodity circulation cabin, be equipped with control system in the aircraft nose, control system, The electric hydraulic press comprises a wireless communication device and a plurality of displays, wherein an infrared imaging device and 4 high-definition cameras are arranged on the outer wall of a machine head, the electric hydraulic press is provided with a double-engine turboprop engine, a push generator, a rotor, the infrared imaging device, the high-definition cameras, the displays and a hoisting device, the hoisting device is respectively electrically connected with a controller, and the controller is in communication connection with a user terminal through the wireless communication device.
2. The unmanned aerial vehicle for air drop logistics transportation of claim 1, wherein the controller is a master MCU and the wireless communication device is OFDM.
3. The unmanned aerial vehicle for air-drop logistics transportation of claim 1, wherein the user terminal is a computer.
4. The unmanned aerial vehicle for air-drop logistics transportation of claim 1, wherein a drop door is opened on the logistics cabin, and the drop door is electrically connected with the controller.
5. The unmanned aerial vehicle for air drop logistics transportation of claim 1, wherein the display comprises an upper screen, a middle screen and a lower screen which are connected with the controller, and the upper screen is a HUD screen.
6. The unmanned aerial vehicle for air-drop logistics transportation of claim 1, wherein an inner supporting beam is arranged in the wing.
7. The unmanned aerial vehicle for air-drop logistics transportation of claim 1, wherein the landing gear is a rear three-point landing gear.
8. The novel unmanned aerial vehicle for air-drop logistics transportation of claim 1, wherein the crane is a suspension crane.
9. The unmanned aerial vehicle for air-drop logistics transportation of claim 1, wherein the infrared imaging device is a thermal infrared imager.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921780214.XU CN210942265U (en) | 2019-10-22 | 2019-10-22 | Novel aerial commodity circulation of puting in transports unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921780214.XU CN210942265U (en) | 2019-10-22 | 2019-10-22 | Novel aerial commodity circulation of puting in transports unmanned aerial vehicle |
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| CN210942265U true CN210942265U (en) | 2020-07-07 |
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| CN201921780214.XU Expired - Fee Related CN210942265U (en) | 2019-10-22 | 2019-10-22 | Novel aerial commodity circulation of puting in transports unmanned aerial vehicle |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111824411A (en) * | 2020-07-30 | 2020-10-27 | 南方科技大学 | Fixed-wing VTOL UAV |
| CN114537065A (en) * | 2022-02-28 | 2022-05-27 | 重庆交通大学 | Air-ground dual-purpose multifunctional unmanned aerial vehicle |
| CN116062205A (en) * | 2023-03-07 | 2023-05-05 | 四川腾盾科技有限公司 | Unmanned aerial vehicle with integral fuselage cargo hold throwing and recycling device and throwing method |
-
2019
- 2019-10-22 CN CN201921780214.XU patent/CN210942265U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111824411A (en) * | 2020-07-30 | 2020-10-27 | 南方科技大学 | Fixed-wing VTOL UAV |
| CN114537065A (en) * | 2022-02-28 | 2022-05-27 | 重庆交通大学 | Air-ground dual-purpose multifunctional unmanned aerial vehicle |
| CN116062205A (en) * | 2023-03-07 | 2023-05-05 | 四川腾盾科技有限公司 | Unmanned aerial vehicle with integral fuselage cargo hold throwing and recycling device and throwing method |
| CN116062205B (en) * | 2023-03-07 | 2023-06-30 | 四川腾盾科技有限公司 | Unmanned aerial vehicle with integral fuselage cargo hold throwing and recycling device and throwing method |
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