CN202414153U - Multi-purpose unmanned aerial vehicle airframe - Google Patents
Multi-purpose unmanned aerial vehicle airframe Download PDFInfo
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- CN202414153U CN202414153U CN2011205391380U CN201120539138U CN202414153U CN 202414153 U CN202414153 U CN 202414153U CN 2011205391380 U CN2011205391380 U CN 2011205391380U CN 201120539138 U CN201120539138 U CN 201120539138U CN 202414153 U CN202414153 U CN 202414153U
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- aerial vehicle
- unmanned aerial
- purpose unmanned
- airframe
- aircraft
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Abstract
The utility model provides a multi-purpose unmanned aerial vehicle airframe. The multi-purpose unmanned aerial vehicle airframe comprises an airframe main body, an equipment compartment, a parachuting equipment compartment, an engine diversion cover, a tail supporting beam, a vertical tail wing, a landing gear set and aircraft main wings, wherein the front part of the airframe main body is sequentially provided with the equipment compartment and the parachuting equipment compartment; the fixing positions of the tail supporting beam and the aircraft main wings are fixed by using metal connecting and fast disassembly and assembly components; and the aircraft main wings are connected with the airframe main body, a metal fast disassembly and assembly and connecting component and a bolt are used for fixation, and the whole of the multi-purpose unmanned aerial vehicle airframe is of pneumatic appearance design. The multi-purpose unmanned aerial vehicle airframe disclosed by the utility model has the advantages and the positive effects that the appearance layout design uses a twin-tailboom back pushing type engine, so that the mounting and using space of equipment is expanded and the multi-purpose unmanned aerial vehicle airframe is further conductive to performing a monitoring task; and in the aspect of assembly of the whole machine, the metal connecting and fast disassembly and assembly components are applied, the disassembly and the assembly are convenient and fast, the whole machine is convenient to carry after decomposition, and the trivial operation of using a high-strength insertion pipe for connection of an existing product in the two assembly links and the potential flight hidden troubles can be further eliminated.
Description
Technical field
The utility model belongs to the unmanned plane technical field.
Background technology
According to the needs that society uses, regional among a small circle to some, the especially geologic hazard of particular surroundings or high-risk environment, the aerial image and the monitoring requirements of preventing and reducing natural disasters are all the more extensively with urgent.Image is monitored and collected in these zones in the air, and using has people's aircraft cost high, relates to the restriction problem of personal safety and flying condition, and the SUAV that arises at the historic moment has thus progressively had momentum of development.In recent years; Domestic more existing be used for the SUAV in these fields; Owing to be the early stage of development; Majority is to be processed by former large-scale model aircraft conversion, and all still there is a lot of problem and shortage its reliability, standardization level, the specialization of flying platform and aspect such as proprietary performance of corresponding task in practical application.
Summary of the invention
To the deficiency of prior art, the problem that the utility model will solve provides a kind of multi-purpose unmanned aerial vehicle body, the middle lowsteaming of especially corresponding common mission requirements and the requirement of flight stability.
For solving the problems of the technologies described above, the technical scheme that the utility model adopts is:
A kind of multi-purpose unmanned aerial vehicle body comprises fuselage main body, equipment compartment, parachuting equipment compartment, engine flow guiding cover, shoe beam, vertical tail, tailplane, alighting gear group, aircraft main wing, aircraft aileron; Said fuselage body front part is provided with equipment compartment and parachuting equipment compartment successively, and its rear portion is provided with Power Drive Unit, and the engine flow guiding cover is set above the said Power Drive Unit; Be provided with the device for image fixed mount in the said equipment compartment, be provided with the equipment hatchcover above it; Said airframe main body interposition is equipped with wing body fusion wing platform and is connected with both sides aircraft main wing, and the aircraft main wing is provided with the aircraft aileron in the outer panel position; Said shoe beam is arranged at aircraft main wing lower surface and captives joint with the aircraft main wing; Said shoe beam is provided with vertical tail at the back, and said vertical tail inboard is provided with tailplane.
Further, the full machine of said multi-purpose unmanned aerial vehicle body adopts the high strength composite material.
Further, said alighting gear group is connected with the fuselage main body, uses the regular bolt locking, is convenient to the exchange of two kinds of landing modes.
Further, said aircraft main wing is connected with the fuselage main body, uses metal fast assembling-disassembling coupling assembling and bolt.
Further, the fixed position of said shoe beam and aircraft main wing is used metal to connect the fast assembling-disassembling assembly and is fixed.
Further, said alighting gear group is wheeled sliding alighting gear group of running, and its fuselage main body belly also is provided with and launches the skid device.
Further, the integral body of said multi-purpose unmanned aerial vehicle body designs for aerodynamic configuration.
Advantage and the good effect that the utlity model has are:
This multi-purpose unmanned aerial vehicle body can be realized the flexible rapid reaction of little spatial domain scope, the operation of high-risk environment low-risk;
Pusher engine behind the two shoes of profile topological design use; The installation of equipment and the expansion that usage space more helps the task of monitoring have been expanded; The specialized equipment dimensional weight commonly used that is provided with the tasks such as monitoring of can corresponding existing implementing to take photo by plane requires the device designed cabin; Wheeled sliding alighting gear group of running, reservation launch sled and parachute compartment, take off and land in the zone that is used for inorganic field condition;
Aspect the complete machine assembling; The aircraft main wing is connected with the wing main body with fuselage main body, shoe beam; What the connection at this two place was used is to connect the fast assembling-disassembling assembly by the metal that high-strength aluminium alloyage CNC is processed into; Convenient to disassembly, it is easy to carry to decompose the back complete machine, and eliminates more existing model of an airplane repacking products and use the loaded down with trivial details and potential flight hidden danger of high strength intubate bonded assembly these two assembling links.
Description of drawings
Fig. 1 is the lateral plan of the utility model;
Fig. 2 is the birds-eye view of the utility model;
Fig. 3 is the front elevation of the utility model.
Among the figure:
1, fuselage main body 2, equipment hatchcover 3, parachuting equipment compartment
4, engine flow guiding cover 5, shoe beam 6, vertical tail
7, tailplane 8, alighting gear group 9, launch sled
10, aircraft main wing 11 aircraft ailerons
The specific embodiment
Shown in Fig. 1 to 3:
A kind of multi-purpose unmanned aerial vehicle body of the utility model comprises fuselage main body 1, equipment hatchcover 2, parachuting equipment compartment 3, engine flow guiding cover 4, shoe beam 5, vertical tail 6, tailplane 7, alighting gear group 8, launches sled 9, aircraft main wing 10, aircraft aileron 11; Said fuselage main body 1 front portion is provided with equipment compartment and parachuting equipment compartment 3 successively, and its rear portion is provided with Power Drive Unit, and engine flow guiding cover 4 is set above the said Power Drive Unit; Be provided with the device for image fixed mount in the said equipment compartment, be provided with equipment hatchcover 2 above it; Said airframe main body 1 interposition is equipped with wing body fusion wing platform and uses metal fast assembling-disassembling coupling assemblings to be connected with bolt with both sides aircraft main wing 10; Aircraft main wing 10 is provided with aircraft aileron 11 in the outer panel position, and said shoe beam 5 is arranged at aircraft main wing 10 lower surface positions and uses metal to be connected fast assembling-disassembling assembly captive joint with aircraft main wing 10; Said shoe beam 5 back are provided with vertical tail 6, and said vertical tail 6 inboards are provided with tailplane 7; The full machine of said multi-purpose unmanned aerial vehicle body adopts the high strength composite material; Said alighting gear group 8 is wheeled sliding alighting gear groups of running, and it is connected with fuselage main body 1, uses regular bolt to lock, and is convenient to the quick exchange of two kinds of landing modes, and its front fuselage main body belly also is provided with and launches sled 9; The integral body of said multi-purpose unmanned aerial vehicle body designs for aerodynamic configuration.
The working process of this instance: at first; Input contemplated route and RTE DATA in the automatic flight control unit in this multi-purpose unmanned aerial vehicle body; Again with its startup; Accomplish driverless operation state automated closed-loop flight and aerial reflection on the way down and take, can be applied to aerial monitoring, take photo by plane, geology archaeology and providing of collection of images and data in the air such as prevent and reduce natural disasters.
More than the embodiment of the utility model is specified, but said content is merely the preferred embodiment of the utility model, can not be considered to be used to limit the practical range of the utility model.All equalizations of doing according to the utility model application range change and improve etc., all should still belong within the patent covering scope of the utility model.
Claims (7)
1. multi-purpose unmanned aerial vehicle body; Comprise fuselage main body, aircraft main wing, shoe beam, vertical tail and alighting gear group; It is characterized in that: said fuselage body front part is provided with equipment compartment and parachuting equipment compartment successively; Its rear portion is provided with Power Drive Unit, and the engine flow guiding cover is set above the said Power Drive Unit; Be provided with the device for image fixed mount in the said equipment compartment, be provided with the equipment hatchcover above it; Said airframe main body interposition is equipped with wing body fusion wing platform and is connected with both sides aircraft main wing, and the aircraft main wing is provided with the aircraft aileron in the outer panel position; Said shoe beam is arranged at aircraft main wing lower surface and captives joint with the aircraft main wing; Said shoe beam is provided with vertical tail at the back, and said vertical tail inboard is provided with tailplane.
2. multi-purpose unmanned aerial vehicle body according to claim 1 is characterized in that: the body that its full machine adopts the high strength composite material to process.
3. multi-purpose unmanned aerial vehicle body according to claim 1 is characterized in that: said alighting gear group is used the regular bolt locking with being connected of fuselage main body.
4. multi-purpose unmanned aerial vehicle body according to claim 1 is characterized in that: said aircraft main wing is connected with the fuselage main body, uses metal fast assembling-disassembling coupling assembling and bolt.
5. multi-purpose unmanned aerial vehicle body according to claim 1 is characterized in that: the fixed position of said shoe beam and aircraft main wing, and use metal to connect the fast assembling-disassembling assembly and fix.
6. multi-purpose unmanned aerial vehicle body according to claim 1 is characterized in that: said alighting gear group is wheeled sliding alighting gear group of running, and its fuselage main body belly also is provided with and launches the sled device.
7. multi-purpose unmanned aerial vehicle body according to claim 1 is characterized in that: its integral body designs for aerodynamic configuration.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205391380U CN202414153U (en) | 2011-12-21 | 2011-12-21 | Multi-purpose unmanned aerial vehicle airframe |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205391380U CN202414153U (en) | 2011-12-21 | 2011-12-21 | Multi-purpose unmanned aerial vehicle airframe |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202414153U true CN202414153U (en) | 2012-09-05 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205391380U Expired - Fee Related CN202414153U (en) | 2011-12-21 | 2011-12-21 | Multi-purpose unmanned aerial vehicle airframe |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202414153U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103523215A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Landing assisting wheel of unmanned aerial vehicle |
| CN103523203A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Front camera cabin of unmanned aerial vehicle |
| CN106741823A (en) * | 2016-12-30 | 2017-05-31 | 易瓦特科技股份公司 | Unmanned plane body prepared by composite and preparation method thereof |
| CN110228581A (en) * | 2019-06-06 | 2019-09-13 | 天峋创新（北京）科技有限公司 | A kind of high speed Bi-Tail-Boom Layout unmanned plane |
| CN111824388A (en) * | 2019-04-18 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Fixed wing unmanned aerial vehicle tail boom hangs |
| CN115258190A (en) * | 2022-08-04 | 2022-11-01 | 杨熙 | Design method and system for modifying unmanned aerial vehicle system by upper single-wing aircraft |
-
2011
- 2011-12-21 CN CN2011205391380U patent/CN202414153U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103523215A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Landing assisting wheel of unmanned aerial vehicle |
| CN103523203A (en) * | 2013-10-15 | 2014-01-22 | 江苏艾锐泰克无人飞行器科技有限公司 | Front camera cabin of unmanned aerial vehicle |
| CN106741823A (en) * | 2016-12-30 | 2017-05-31 | 易瓦特科技股份公司 | Unmanned plane body prepared by composite and preparation method thereof |
| CN106741823B (en) * | 2016-12-30 | 2019-11-15 | 易瓦特科技股份公司 | By the unmanned plane body and preparation method thereof of composite material preparation |
| CN111824388A (en) * | 2019-04-18 | 2020-10-27 | 成都飞机工业（集团）有限责任公司 | Fixed wing unmanned aerial vehicle tail boom hangs |
| CN110228581A (en) * | 2019-06-06 | 2019-09-13 | 天峋创新（北京）科技有限公司 | A kind of high speed Bi-Tail-Boom Layout unmanned plane |
| CN115258190A (en) * | 2022-08-04 | 2022-11-01 | 杨熙 | Design method and system for modifying unmanned aerial vehicle system by upper single-wing aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: ZHONGHENG TIANXIN (TIANJIN) AEROSPACE TECHNOLOGY C Free format text: FORMER OWNER: TIANJIN FENGZHIYING TECHNOLOGY CO., LTD. Effective date: 20150617 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150617 Address after: 300000, building 10, Zhonglian Industrial Park, Xiqing automotive industry zone, Tianjin, 101 Patentee after: Heng Tianxin (Tianjin) Aviation Technology Co. Ltd. Address before: 300412, Tianjin Beichen District East Road (King Wang Food Co., Ltd.) Patentee before: Tianjin Fengzhiying Technology Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120905 Termination date: 20181221 |