CN205239913U - Top load unmanned aerial vehicle convenient to take off and land fast - Google Patents
Top load unmanned aerial vehicle convenient to take off and land fast Download PDFInfo
- Publication number
- CN205239913U CN205239913U CN201520886790.8U CN201520886790U CN205239913U CN 205239913 U CN205239913 U CN 205239913U CN 201520886790 U CN201520886790 U CN 201520886790U CN 205239913 U CN205239913 U CN 205239913U
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- unmanned plane
- landing
- aerial vehicle
- unmanned aerial
- top load
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Abstract
The utility model discloses a top load unmanned aerial vehicle convenient to take off and land fast, carry thing cabin including this internal being provided with of unmanned aerial vehicle body and unmanned aerial vehicle, the both sides of mounting bracket all are provided with and all are provided with the descending support frame in pivot and the pivot, and the both sides of descending support frame all are provided with the bracing piece in being provided with backup pad and backup pad, and the one end of bracing piece is provided with the descending supporting seat, and be provided with supporting spring between backup pad and the descending supporting seat and supporting spring cup joints on the bracing piece, the one side of carrying the thing cabin is provided with the controller. The utility model discloses the load of high power capacity can be carried out, unmanned aerial vehicle's delivery efficiency has been improved, when carrying out the top load descending, supporting spring can provide certain cushion effect, has avoided the damage to unmanned aerial vehicle, quick the stretching out of descending support frame meeting behind the ground that is about to to reach, it descends to provide supports, has improved unmanned aerial vehicle's speed of taking off and land and efficiency, can not receive the damage by effectual protection unmanned aerial vehicle.
Description
Technical field
The utility model relates to a kind of unmanned plane, particularly a kind of top load unmanned plane of being convenient to quick landing.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is the journey of utilizing radio robot and providing for oneselfThe not manned aircraft that order control device is handled. Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, nothingPeople's multi-rotor aerocraft, unmanned airship, unmanned parasol etc.; Unmanned plane, by application, can be divided into military and civilian. MilitaryAspect, unmanned plane is divided into reconnaissance plane and target drone; Unmanned plane+sector application is the real firm need of unmanned plane. At present taking photo by plane,The application in the field such as agricultural plant protection, mapping, has expanded the purposes of unmanned plane itself greatly. Unmanned plane is as far back as 20th century 20Age occurs, is at that time to use as the target drone of training use. That for describing, latest generation is unmanned to fly in many countriesThe term of machine. From literal, this term can be described from kite, and drone comes from developing to V-1 fly bombCruise missile, but in the term of the military, only limit to reusable heavier-than-air aircraft.
What unmanned plane was applied aspect agricultural production, mapping and national defence at present is very extensive, does to expanding economy and national defenceLoad exceedance gone out very large contribution, but the load of current unmanned plane is lower, because can cause damage to the undercarriage of unmanned planeWound, and load exceedance can damage the structural stability of unmanned plane; Current unmanned plane is in landing, owing to risingThe bracing frame that falls is fixed, and in landing, must reduce sinking speed, otherwise can cause damage to undercarriage, causesSinking speed slower, affected the landing speed of unmanned plane.
Utility model content
The technical problems to be solved in the utility model is to overcome existing defect, provides a kind of top load of being convenient to quick landing unmannedMachine can carry out quick landing in the situation that carrying out top load.
In order to solve the problems of the technologies described above, the utility model provides following technical scheme:
A kind of top load unmanned plane of being convenient to quick landing of the utility model, comprises in unmanned plane body and described unmanned plane body and establishingBe equipped with loading cabin, a side in described loading cabin is provided with cover plate, and a side of described unmanned plane body is provided with installing rack and described peaceShelve and be provided with laser range finder, the both sides of described installing rack are provided with and in rotating shaft and described rotating shaft, are provided with landing and supportFrame, the both sides of described landing bracing frame are provided with in gripper shoe and described gripper shoe and are provided with support bar, one of described support barEnd is provided with landing supporting seat, is provided with support spring and described support spring cover between described gripper shoe and described landing supporting seatBe connected on support bar; One side in described loading cabin is provided with controller.
As the preferred a kind of technical scheme of the utility model, a side of described landing bracing frame be provided with the first back-up block and described inOn the first back-up block, be provided with hydraulic stem, one end that the both sides of described unmanned plane body are provided with installing plate and described installing plate arrangesHave the second back-up block, one end of described hydraulic stem is connected to described the second back-up block.
As the preferred a kind of technical scheme of the utility model, the both sides of described unmanned plane body are provided with mounting rod and described peaceOne end of dress bar is provided with motor, and one end of described motor is provided with on rotating shaft and described rotating shaft and is all provided with and revolvesThe wing.
As the preferred a kind of technical scheme of the utility model, described laser range finder is electrically connected described controller and described controlDevice is electrically connected described hydraulic stem.
The beneficial effects of the utility model are: can carry out the load of high power capacity, improve the delivery efficiency of unmanned plane; Carry outWhen top load landing, support spring can provide certain cushion effect, has avoided the damage to unmanned plane; The ground that is being about to reachRear landing bracing frame can stretch out fast, provides landing to support, and has improved landing speed and the efficiency of unmanned plane; Can be effectiveProtection unmanned plane is not damaged.
Brief description of the drawings
Accompanying drawing is used to provide further understanding of the present utility model, and forms a part for description, with of the present utility modelEmbodiment mono-is used from explanation the utility model, does not form restriction of the present utility model. In the accompanying drawings:
Fig. 1 is the structural representation of a kind of top load unmanned plane of being convenient to quick landing described in the utility model embodiment;
Fig. 2 is the module map of a kind of top load unmanned plane of being convenient to quick landing described in the utility model embodiment;
In figure: 1, unmanned plane body; 2, loading cabin; 3, cover plate; 4, mounting rod; 5, motor; 6, rotating shaft; 7,Rotor; 8, installing rack; 9, laser range finder; 10, controller; 11, rotating shaft; 12, landing bracing frame; 13, landingSupport seat; 14, gripper shoe; 15, support bar; 16, support spring; 17, the first back-up block; 18, hydraulic stem; 19, installPlate; 20, the second back-up block.
Detailed description of the invention
Below in conjunction with accompanying drawing, preferred embodiment of the present utility model is described, should be appreciated that preferred enforcement described hereinExample is only for description and interpretation the utility model, and is not used in restriction the utility model.
Embodiment:
As shown in Figure 1 to Figure 2, a kind of top load unmanned plane of being convenient to quick landing of the utility model, comprises unmanned plane body 1And in unmanned plane body 1, be provided with loading cabin 2, a side in loading cabin 2 is provided with cover plate 3, and a side of unmanned plane body 1 is establishedBe equipped with on installing rack 8 and installing rack 8 and be provided with laser range finder 9, the both sides of installing rack 8 are provided with rotating shaft 11 and rotating shaftOn 11, be provided with landing bracing frame 12, the both sides of landing bracing frame 12 are provided with gripper shoe 14 and the interior all settings of gripper shoe 14Have support bar 15, one end of support bar 15 is provided with landing supporting seat 13, between gripper shoe 14 and landing supporting seat 13, arrangesThere are support spring 16 and support spring 16 to be socketed on support bar 15; One side in loading cabin 2 is provided with controller 10.
One side of landing bracing frame 12 is provided with on the first back-up block 17 and the first back-up block 17 and is provided with hydraulic stem 18, unmannedOne end that the both sides of machine body 1 are provided with installing plate 19 and installing plate 19 is provided with the second back-up block 20, one of hydraulic stem 18End is connected to the second back-up block 20, can be fast by hydraulic stem 18 flexible landing bracing frame 12 is folded and underPut.
One end that the both sides of unmanned plane body 1 are provided with mounting rod 4 and mounting rod 4 is provided with motor 5, motor 5One end be provided with on rotating shaft 6 and rotating shaft 6 rotor 7 be all installed, provide enough moving can to taking off of unmanned planePower.
Laser range finder 9 is electrically connected controller 10 and controller 10 is electrically connected hydraulic stem 18, can pass through laser range finder9 detect and approach behind ground, then stretch out by controlling 10 control hydraulic stems, and landing bracing frame 12 is transferred, and completeThe landing of unmanned plane.
The utility model can use loading cabin 2 to carry out top load, and then take off and carry out loading flight, in landing,On installing rack 8, laser range finder 9 can detect the distance apart from ground in real time, in the time being about to reach ground, can pass through controller 10Control hydraulic stem 18 stretch out, the bracing frame 12 that then lands can stretch out, because the load in loading cabin 2 is larger, therefore withoutThe man-machine impulsive force for ground is very large, but support spring 16 can provide certain cushion effect by gripper shoe 14, avoids fallingThe bracing frame 12 that falls is damaged, and has also reduced the impulsive force that unmanned plane body 1 is subject to simultaneously.
The utility model can carry out the load of high power capacity, has improved the delivery efficiency of unmanned plane; In the time carrying out top load landing,Support spring 16 can provide certain cushion effect, has avoided the damage to unmanned plane; Behind the ground that is about to reach, landing is supportedFrame 12 can stretch out fast, provides landing to support, and has improved landing speed and the efficiency of unmanned plane: can effectively protect nothingMan-machinely be not damaged.
Finally it should be noted that: the foregoing is only preferred embodiment of the present utility model, be not limited to this practicality newType, although the utility model is had been described in detail with reference to previous embodiment, for a person skilled in the art, itsThe technical scheme that still can record aforementioned each embodiment is modified, or part technical characterictic is wherein equal to and is replacedChange. All within spirit of the present utility model and principle, any amendment of doing, be equal to replacement, improvement etc., all should be included inWithin protection domain of the present utility model.
Claims (4)
1. be convenient to a top load unmanned plane for quick landing, comprise in unmanned plane body and described unmanned plane body and be provided with loadingCabin, a side in described loading cabin is provided with cover plate, it is characterized in that, and a side of described unmanned plane body is provided with installing rack and instituteState on installing rack and be provided with laser range finder, the both sides of described installing rack are provided with in rotating shaft and described rotating shaft and are provided with landingBracing frame, the both sides of described landing bracing frame are provided with in gripper shoe and described gripper shoe and are provided with support bar, described support barOne end be provided with landing supporting seat, between described gripper shoe and described landing supporting seat, be provided with support spring and described support bulletSpring is socketed on support bar; One side in described loading cabin is provided with controller.
2. a kind of top load unmanned plane of being convenient to quick landing according to claim 1, is characterized in that, described landing is propped upOne side of support is provided with on the first back-up block and described the first back-up block and is provided with hydraulic stem, and establish the both sides of described unmanned plane bodyThe one end that is equipped with installing plate and described installing plate is provided with the second back-up block, and one end of described hydraulic stem is connected to described second and supportsPiece.
3. a kind of top load unmanned plane of being convenient to quick landing according to claim 1, is characterized in that described unmanned planeOne end that the both sides of body are provided with mounting rod and described mounting rod is provided with motor, and one end of described motor all arrangesHave on rotating shaft and described rotating shaft rotor is all installed.
4. a kind of top load unmanned plane of being convenient to quick landing according to claim 2, is characterized in that described Laser MeasuringBe electrically connected described controller and described controller is electrically connected described hydraulic stem apart from instrument.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520886790.8U CN205239913U (en) | 2015-11-10 | 2015-11-10 | Top load unmanned aerial vehicle convenient to take off and land fast |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520886790.8U CN205239913U (en) | 2015-11-10 | 2015-11-10 | Top load unmanned aerial vehicle convenient to take off and land fast |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205239913U true CN205239913U (en) | 2016-05-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520886790.8U Expired - Fee Related CN205239913U (en) | 2015-11-10 | 2015-11-10 | Top load unmanned aerial vehicle convenient to take off and land fast |
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|---|---|
| CN (1) | CN205239913U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005375A (en) * | 2016-06-03 | 2016-10-12 | 全蕊 | Unmanned gyroplane landing gear and unmanned gyroplane |
| CN106043701A (en) * | 2016-06-15 | 2016-10-26 | 张萍 | Novel agricultural irrigation unmanned aerial vehicle based on Internet of Things |
| CN107719674A (en) * | 2017-10-23 | 2018-02-23 | 于青池 | A kind of student for possessing VTOL function is with Intelligent unattended machine |
| CN107878735A (en) * | 2017-11-14 | 2018-04-06 | 冯志强 | A kind of foldable unmanned plane undercarriage |
| CN108408032A (en) * | 2018-01-31 | 2018-08-17 | 芜湖市海联机械设备有限公司 | A kind of unmanned plane equipped with foldable unmanned plane supporting member |
| CN110884644A (en) * | 2019-12-09 | 2020-03-17 | 湖南浩天翼航空技术有限公司 | Prevent violently rocking unmanned aerial vehicle with descending structure |
| CN113371213A (en) * | 2021-06-25 | 2021-09-10 | 上海海事大学 | Unmanned aerial vehicle structure with take-off and landing protection device |
| CN115416844A (en) * | 2022-09-28 | 2022-12-02 | 张春宝 | Unmanned aerial vehicle undercarriage based on agricultural monitoring automatic cleaning landing site |
-
2015
- 2015-11-10 CN CN201520886790.8U patent/CN205239913U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106005375A (en) * | 2016-06-03 | 2016-10-12 | 全蕊 | Unmanned gyroplane landing gear and unmanned gyroplane |
| CN106043701A (en) * | 2016-06-15 | 2016-10-26 | 张萍 | Novel agricultural irrigation unmanned aerial vehicle based on Internet of Things |
| CN106043701B (en) * | 2016-06-15 | 2018-01-23 | 湖南莲花百川电子科技有限公司 | A kind of new unmanned plane for being used for agricultural and pouring based on Internet of Things |
| CN107719674A (en) * | 2017-10-23 | 2018-02-23 | 于青池 | A kind of student for possessing VTOL function is with Intelligent unattended machine |
| CN107878735A (en) * | 2017-11-14 | 2018-04-06 | 冯志强 | A kind of foldable unmanned plane undercarriage |
| CN108408032A (en) * | 2018-01-31 | 2018-08-17 | 芜湖市海联机械设备有限公司 | A kind of unmanned plane equipped with foldable unmanned plane supporting member |
| CN110884644A (en) * | 2019-12-09 | 2020-03-17 | 湖南浩天翼航空技术有限公司 | Prevent violently rocking unmanned aerial vehicle with descending structure |
| CN113371213A (en) * | 2021-06-25 | 2021-09-10 | 上海海事大学 | Unmanned aerial vehicle structure with take-off and landing protection device |
| CN115416844A (en) * | 2022-09-28 | 2022-12-02 | 张春宝 | Unmanned aerial vehicle undercarriage based on agricultural monitoring automatic cleaning landing site |
| CN115416844B (en) * | 2022-09-28 | 2023-09-26 | 张春宝 | Unmanned aerial vehicle undercarriage based on agricultural monitoring automatically cleans landing site |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: XI'AN DERUN AVIATION TECHNOLOGY CO., LTD. Document name: Notification to Pay the Fees |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160518 Termination date: 20171110 |
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| CF01 | Termination of patent right due to non-payment of annual fee |