CN217515368U - Land is unmanned aerial vehicle clamping device for prequalification - Google Patents
Land is unmanned aerial vehicle clamping device for prequalification Download PDFInfo
- Publication number
- CN217515368U CN217515368U CN202221088012.0U CN202221088012U CN217515368U CN 217515368 U CN217515368 U CN 217515368U CN 202221088012 U CN202221088012 U CN 202221088012U CN 217515368 U CN217515368 U CN 217515368U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- mainboard
- centre gripping
- subplate
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
Images
Landscapes
- Manipulator (AREA)
Abstract
The utility model relates to the technical field of aircrafts, and discloses an unmanned aerial vehicle clamping device for land pre-examination, which comprises a clamping main board, the two sides of the clamping main board are provided with main board grooves, the inner parts of the main board grooves are movably connected with telescopic auxiliary boards, the size of the telescopic auxiliary plate is matched with that of the main plate groove, an auxiliary plate groove is arranged inside the telescopic auxiliary plate, the inside of the auxiliary plate groove is provided with a telescopic spring, the size of the telescopic spring is matched with the size of the auxiliary plate groove, one end of the expansion spring penetrates through the groove of the main board and is fixedly connected with the middle part of the clamping main board, the other end of the expansion spring is fixedly connected with one side of the expansion auxiliary board, the size of the unmanned aerial vehicle body is generally not fixed by arranging the expansion auxiliary board, the width of the telescopic auxiliary plate is adjusted according to the width of the unmanned aerial vehicle body through the telescopic auxiliary plate, so that the unmanned aerial vehicle body is fixed and does not shake.
Description
Technical Field
The utility model relates to an aircraft technical field, more specifically relate to an land used is unmanned aerial vehicle clamping device for pretrial.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can provide a wide range of basic geographic information for city planning, construction and management, as well as law enforcement forensics, such as urban road bridge construction, traffic patrols, police surveillance, city law enforcement, and the like. When urban planning is carried out, more detailed urban land utilization information is needed, if manual exploration is carried out, the workload is huge, and information about urban residential land, road traffic, public buildings and the like can be clearly interpreted and extracted from aerial images of unmanned aerial vehicles.
In the prior art, the unmanned aerial vehicle is provided with no cockpit, is provided with an automatic pilot, a program control device and other equipment, and is tracked, positioned, remotely controlled, telemetered and digitally transmitted by the personnel on the ground, a naval vessel or a mother aircraft remote control station through radar and other equipment.
SUMMERY OF THE UTILITY MODEL
In order to overcome prior art's above-mentioned defect, the utility model provides an land is unmanned aerial vehicle clamping device for prequalification to solve the problem that exists among the above-mentioned background art.
The utility model provides a following technical scheme: the utility model provides an land is unmanned aerial vehicle clamping device for prequalification, includes the centre gripping mainboard, the mainboard recess has been seted up to the both sides of centre gripping mainboard, the inside swing joint of mainboard recess has flexible subplate, the size of flexible subplate and the big or small looks adaptation of mainboard recess, the subplate recess has been seted up to the inside of flexible subplate, expanding spring has been placed to the inside of subplate recess, expanding spring's size and the big or small looks adaptation of subplate recess, expanding spring's one end runs through mainboard recess fixed connection at centre gripping mainboard middle part, expanding spring's other end fixed connection is in one side of flexible subplate, is favorable to making the fuselage fixed and not rock according to the width of the flexible subplate of width adjustment of unmanned fuselage.
Further, the bottom fixedly connected with centre gripping bottom plate of centre gripping mainboard, the centre gripping mainboard is the same with the length and width of centre gripping bottom plate, the bottom both sides fixedly connected with support frame of centre gripping bottom plate, two the bottom fixedly connected with U type undercarriage of support frame, the frame groove that has fallen has been seted up to the top surface of U type undercarriage, the inside in frame groove that falls is fixed to the bottom of support frame, the big or small looks adaptation in support frame and the frame groove that falls, the wear-resisting soft rubber pad of bottom fixedly connected with of U type undercarriage is favorable to unmanned aerial vehicle big impact force when descending, plays the cushioning effect when fast, and protection fuselage bottom camera equipment does not receive easy damage.
Further, the top swing joint of centre gripping mainboard has the unmanned aerial vehicle fuselage, the both sides fixedly connected with fixed wing of unmanned aerial vehicle fuselage, four the one end swing joint of fixed wing has folding wing, four the one end top swing joint of folding wing has the screw, unmanned aerial vehicle fuselage bottom front end swing joint has high definition digtal camera, is favorable to unmanned aerial vehicle when flight, shoots the picture and saves according to operator's demand high definition digtal camera.
Further, the outer wall fixedly connected with fixed bump of flexible subplate, the outer end swing joint of fixed bump has flexible resilience rope, is favorable to further making the fuselage fixed and not rocking according to the length of the flexible resilience rope of size adjustment of unmanned fuselage.
Further, flexible resilience rope is five millimeters to a centimetre for the diameter and is the elastic material, is favorable to fixed unmanned aerial vehicle.
Further, the material of wear-resisting rubber cushion is high-elastic wear-resisting material, and it is big to be favorable to unmanned aerial vehicle impact force when descending, plays the cushioning effect when fast, protects fuselage bottom camera equipment not receive easy damage.
The utility model discloses a technological effect and advantage:
1. the utility model discloses a be equipped with flexible subplate, unmanned aerial vehicle's fuselage size is generally all unfixed, makes the fuselage fixed and do not rock through the width that is equipped with flexible subplate according to the flexible subplate of width adjustment of unmanned aerial vehicle fuselage.
2. The utility model discloses a be equipped with wear-resisting rubber cushion, it is big to be favorable to unmanned aerial vehicle impact force when descending, plays the cushioning effect when fast, and protection fuselage bottom camera equipment does not receive easy damage.
3. The utility model discloses a be equipped with flexible resilience rope, be favorable to further making the fuselage fixed and not rocking according to the length of the flexible resilience rope of size adjustment of unmanned fuselage.
Drawings
Fig. 1 is the utility model discloses an unmanned aerial vehicle clamping device overall structure schematic diagram.
Fig. 2 is a schematic structural view of the clamping device of the present invention.
Fig. 3 is an explosion diagram of the structure of the holding device of the present invention.
Fig. 4 is a schematic view of the top structure of the clamping device of the present invention.
The reference signs are: 1. clamping the main board; 101. clamping the bottom plate; 102. a U-shaped landing gear; 103. a wear-resistant soft rubber pad; 104. a telescopic auxiliary plate; 105. fixing the salient points; 106. a retractable rebound rope; 107. a support frame; 108. a landing gear slot; 109. a main board groove; 110. a secondary plate groove; 111. a tension spring; 2. an unmanned aerial vehicle body; 201. fixing the wing; 202. folding the wing; 203. a propeller; 204. high-definition camera.
Detailed Description
The technical solution of the present invention will be clearly and completely described below with reference to the drawings of the present invention, and in addition, the forms of the structures described in the following embodiments are merely examples, and the present invention relates to an unmanned aerial vehicle clamping device for land pre-examination is not limited to the structures described in the following embodiments, and all other embodiments obtained by a person having ordinary skill in the art without creative labor belong to the scope of the present invention.
Referring to fig. 1-4, the utility model provides an unmanned aerial vehicle clamping device is used in land pre-examination, including centre gripping mainboard 1, mainboard recess 109 has been seted up to centre gripping mainboard 1's both sides, the inside swing joint of mainboard recess 109 has flexible subplate 104, the size of flexible subplate 104 and the big or small looks adaptation of mainboard recess 109, subplate recess 110 has been seted up to the inside of flexible subplate 104, expanding spring 111 has been placed to the inside of subplate recess 110, expanding spring 111's size and subplate recess 110's big or small looks adaptation, mainboard recess 109 fixed connection is run through to expanding spring 111's one end at centre gripping mainboard 1 middle part, expanding spring 111's other end fixed connection is in one side of flexible subplate 104, be favorable to making the fuselage fixed and not rock according to the width of the flexible subplate 104 of width adjustment of unmanned fuselage.
Wherein, the bottom fixedly connected with centre gripping bottom plate 101 of centre gripping mainboard 1, centre gripping mainboard 1 is the same with the length and width of centre gripping bottom plate 101, the bottom both sides fixedly connected with support frame 107 of centre gripping bottom plate 101, the bottom fixedly connected with U type undercarriage 102 of two support frames 107, undercarriage groove 108 has been seted up to the top surface of U type undercarriage 102, the inside at undercarriage groove 108 is fixed to the bottom of support frame 107, the big or small looks adaptation in support frame 107 and undercarriage groove 108, the wear-resisting soft rubber pad 103 of bottom fixedly connected with of U type undercarriage 102, it is big to be favorable to unmanned aerial vehicle impact force when descending, play the cushioning effect when fast, protection fuselage bottom camera equipment does not receive easy damage.
Wherein, the top swing joint of centre gripping mainboard 1 has unmanned aerial vehicle fuselage 2, the both sides fixedly connected with fixed wing 201 of unmanned aerial vehicle fuselage 2, the one end swing joint of four fixed wing 201 has folding wing 202, the one end top swing joint of four folding wing 202 has screw 203, 2 bottom front end swing joints of unmanned aerial vehicle fuselage have high definition digtal camera 204, be favorable to unmanned aerial vehicle when flying, according to operator's demand high definition digtal camera 204 with the picture shoot and save.
Wherein, the outer wall fixedly connected with fixed bump 105 of flexible subplate 104, the outer end swing joint of fixed bump 105 has flexible resilience rope 106, is favorable to further making the fuselage fixed and not rocking according to the length of the flexible resilience rope 106 of size adjustment of unmanned aerial vehicle body.
Wherein, flexible rope 106 of kick-backing is five millimeters to a centimetre of diameter and is the elastic material, is favorable to fixed unmanned aerial vehicle.
Wherein, the material of wear-resisting rubber cushion pad 103 is high-elastic wear-resisting material, and it is big to be favorable to unmanned aerial vehicle impact force when descending, plays the cushioning effect when fast, and protection fuselage bottom camera equipment does not receive easy damage.
The utility model discloses a theory of operation:
the method comprises the following steps: when using unmanned aerial vehicle clamping device, take out the one end of expanding spring 111 from centre gripping mainboard 1's mainboard recess 109 earlier and fix the inboard fixed connection at flexible subplate 104 and place in subplate recess 110, insert the one end of flexible subplate 104 in mainboard recess 109, make flexible subplate 104 can be according to unmanned aerial vehicle's fuselage size adjustment width at mainboard recess 109, fix the top surface at centre gripping bottom plate 101 with centre gripping mainboard 1 bottom surface after that, the bottom at centre gripping bottom plate 101 is fixed at support frame 107 top, the bottom of support frame 107 is inserted and is made support frame 107 and U type undercarriage 102 fixed connection in the undercarriage groove 108, the bottom at U type undercarriage 102 is fixed at the top of wear-resisting soft rubber pad 103.
Step two: when using unmanned aerial vehicle clamping device, place unmanned aerial vehicle fuselage 2 in centre gripping mainboard 1, folding wing 202 stretches out from fixed wing 201, the starting power supply, screw 203 begins to hover and makes unmanned aerial vehicle fuselage 2 begin to take off, reach and shoot a little after, high definition digtal camera 204 begins to shoot required picture, after the shooting task is accomplished, unmanned aerial vehicle navigates back, slowly whereabouts, wear-resisting soft rubber pad 103 contacts ground and makes whole unmanned aerial vehicle obtain the cushioning effect, be favorable to fuselage bottom camera equipment not to damage.
The points to be finally explained are: first, in the description of the present application, it should be noted that, unless otherwise specified and limited, the terms "mounted," "connected," and "connected" should be understood broadly, and may be a mechanical connection or an electrical connection, or a communication between two elements, and may be a direct connection, and "upper," "lower," "left," and "right" are only used to indicate a relative positional relationship, and when the absolute position of the object to be described is changed, the relative positional relationship may be changed;
secondly, the method comprises the following steps: in the drawings of the disclosed embodiments of the present invention, only the structures related to the disclosed embodiments are referred to, and other structures can refer to the common design, and under the condition of no conflict, the same embodiment and different embodiments of the present invention can be combined with each other;
and finally: the foregoing is illustrative of the preferred embodiments of the present invention, and is not to be construed as limiting the invention, and any modifications, equivalent alterations, improvements and the like made within the spirit and principle of the invention are intended to be included within the scope of the invention.
Claims (6)
1. The utility model provides an land is unmanned aerial vehicle clamping device for prequalification, includes centre gripping mainboard (1), its characterized in that: mainboard recess (109) have been seted up to the both sides of centre gripping mainboard (1), the inside swing joint of mainboard recess (109) has flexible subplate (104), the size of flexible subplate (104) and the big or small looks adaptation of mainboard recess (109), subplate recess (110) have been seted up to the inside of flexible subplate (104), expanding spring (111) have been placed to the inside of subplate recess (110), the size of expanding spring (111) and the big or small looks adaptation of subplate recess (110), mainboard recess (109) fixed connection is run through to the one end of expanding spring (111) at centre gripping mainboard (1) middle part, the other end fixed connection of expanding spring (111) is in one side of flexible subplate (104).
2. The unmanned aerial vehicle clamping device for land pre-trial use of claim 1, characterized in that: the bottom fixedly connected with centre gripping bottom plate (101) of centre gripping mainboard (1), centre gripping mainboard (1) is the same with the length and width of centre gripping bottom plate (101), bottom both sides fixedly connected with support frame (107) of centre gripping bottom plate (101), two the bottom fixedly connected with U type undercarriage (102) of support frame (107), undercarriage groove (108) have been seted up to the top surface of U type undercarriage (102), the inside in undercarriage groove (108) is fixed in the bottom of support frame (107), the big or small looks adaptation in support frame (107) and undercarriage groove (108), the wear-resisting soft rubber pad (103) of bottom fixedly connected with of U type undercarriage (102).
3. The unmanned aerial vehicle clamping device is used to land utilization pretrial according to claim 2, characterized in that: the top swing joint of centre gripping mainboard (1) has unmanned aerial vehicle fuselage (2), both sides fixedly connected with fixed wing (201) of unmanned aerial vehicle fuselage (2), four the one end swing joint of fixed wing (201) has folding wing (202), four the one end top swing joint of folding wing (202) has screw (203), unmanned aerial vehicle fuselage (2) bottom front end swing joint has high definition digtal camera (204).
4. The unmanned aerial vehicle clamping device for land pre-trial use of claim 1, characterized in that: the outer wall of the telescopic auxiliary plate (104) is fixedly connected with a fixed salient point (105), and the outer end of the fixed salient point (105) is movably connected with a telescopic rebound rope (106).
5. The unmanned aerial vehicle clamping device for land pre-trial use of claim 4, characterized in that: the telescopic rebound rope (106) is five millimeters to one centimeter in diameter and made of elastic materials.
6. The unmanned aerial vehicle clamping device is used to land utilization pretrial according to claim 2, characterized in that: the material of the wear-resistant soft rubber pad (103) is high-elastic wear-resistant material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221088012.0U CN217515368U (en) | 2022-05-09 | 2022-05-09 | Land is unmanned aerial vehicle clamping device for prequalification |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221088012.0U CN217515368U (en) | 2022-05-09 | 2022-05-09 | Land is unmanned aerial vehicle clamping device for prequalification |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217515368U true CN217515368U (en) | 2022-09-30 |
Family
ID=83373465
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221088012.0U Active CN217515368U (en) | 2022-05-09 | 2022-05-09 | Land is unmanned aerial vehicle clamping device for prequalification |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217515368U (en) |
-
2022
- 2022-05-09 CN CN202221088012.0U patent/CN217515368U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US10967960B2 (en) | Ground movement system plugin for VTOL UAVs | |
| CN106081098A (en) | A kind of unmanned plane | |
| Hovstein et al. | Experiences with coastal and maritime UAS BLOS operation with phased-array antenna digital payload data link | |
| CN206012982U (en) | A kind of small-sized electric fixed-wing unmanned plane for oblique photograph | |
| CN217515368U (en) | Land is unmanned aerial vehicle clamping device for prequalification | |
| CN109760830B (en) | Environment surveying is with three leg module combination formula rotor unmanned aerial vehicle that prop | |
| WO2020079935A1 (en) | Flying body and system | |
| CN213535092U (en) | Unmanned aerial vehicle that geographic information survey and drawing was used | |
| CN205022916U (en) | Portable flight equipment | |
| CN212980523U (en) | Undercarriage with buffering function for unmanned aerial vehicle | |
| US11018755B2 (en) | Network for enabling beyond visual line of sight aircraft command and control communications | |
| CN206031776U (en) | Unmanned aerial vehicle | |
| CN209719908U (en) | A kind of mapping geography information mapping unmanned plane damping undercarriage | |
| WO2020079934A1 (en) | Control apparatus, program, system, and control method | |
| CN206031763U (en) | Unmanned aerial vehicle plug -in type undercarriage | |
| KR102336741B1 (en) | Unmanned aerial vehicle having apparatus for control take off | |
| CN206031796U (en) | Unmanned aerial vehicle's parachute structure | |
| CN212709948U (en) | Six rotor unmanned aerial vehicle frames that stability can be good | |
| JP2007260374A (en) | Radio-controlled small plane | |
| CN210681169U (en) | A built-up components for unmanned aerial vehicle | |
| CN106240812A (en) | One lifts unmanned plane easily | |
| CN107284684A (en) | One kind is shot without dead angle Intelligent unattended machine | |
| KR102053889B1 (en) | Unmanned aerial vehicle for easily landing | |
| CN215944877U (en) | Floor stand for unmanned aerial vehicle | |
| CN206050071U (en) | It is a kind of to lift easily unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 450000 room 1303, 13th floor, unit 2, building 2, No.22 Chenzhuang street, Zhengdong New District, Zhengzhou City, Henan Province Patentee after: Henan Runtai Digital Technology Group Co.,Ltd. Address before: 450000 room 1303, 13th floor, unit 2, building 2, No.22 Chenzhuang street, Zhengdong New District, Zhengzhou City, Henan Province Patentee before: Henan Runtai Engineering Management Co.,Ltd. |
|
| CP01 | Change in the name or title of a patent holder |