CN113665801A - Unmanned aerial vehicle shock attenuation collection device - Google Patents
Unmanned aerial vehicle shock attenuation collection device Download PDFInfo
- Publication number
- CN113665801A CN113665801A CN202110959369.5A CN202110959369A CN113665801A CN 113665801 A CN113665801 A CN 113665801A CN 202110959369 A CN202110959369 A CN 202110959369A CN 113665801 A CN113665801 A CN 113665801A
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- China
- Prior art keywords
- storage box
- groove
- unmanned aerial
- rod
- aerial vehicle
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- 230000035939 shock Effects 0.000 title claims abstract description 15
- 230000000149 penetrating effect Effects 0.000 claims description 4
- 238000013016 damping Methods 0.000 description 7
- 238000010521 absorption reaction Methods 0.000 description 4
- 230000004888 barrier function Effects 0.000 description 2
- 230000000116 mitigating effect Effects 0.000 description 2
- 239000006096 absorbing agent Substances 0.000 description 1
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention discloses an unmanned aerial vehicle shock attenuation collection device, which is provided with a collection device for collecting a cushioning column, wherein the cushioning column is positioned below an unmanned aerial vehicle arm, and the collection device is characterized by comprising: receiver, movable plate, connecting rod and first recess. The collecting device is arranged, the movable piece is pulled to drive the connecting rod and the movable block to move towards the direction of withdrawing from the storage box, when the movable block completely withdraws from the storage box through the first groove, the telescopic rod is pulled out of the cushioning column, the telescopic rod and the cushioning column are transferred into the storage box, when the telescopic rod and the cushioning column are placed into the storage box, the movable piece is loosened, the spring drives the movable piece to reset, the movable piece drives the connecting rod and the movable block to re-enter the storage box through the first groove, and then the movable piece is in contact with the telescopic rod and the cushioning column in the storage box, so that the telescopic rod and the cushioning column are prevented from being separated from the storage box, and the problems that the conventional cushioning column cannot be folded when not used and is inconvenient to carry are solved.
Description
Technical Field
The invention relates to an unmanned aerial vehicle damping and collecting device.
Background
An unmanned plane is an unmanned plane which is operated by radio remote control equipment and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and can be divided into military, civil and civil aspects according to the application field.
Unmanned aerial vehicle all can have barriers such as trees all around when flying, and unmanned aerial vehicle's paddle can cause the fuselage vibration too big and lead to the problem of crash when bumping over these barriers, consequently need install damping shock mitigation system in the horn below usually, and current damping shock mitigation system does not use at ordinary times and still installs in the horn below, can't accomodate, is unfavorable for carrying of unmanned aerial vehicle.
Disclosure of Invention
The invention aims to provide a device capable of accommodating a damping device below an unmanned aerial vehicle arm.
In order to solve the problems, the invention provides an unmanned aerial vehicle damping and collecting device, which is provided with a collecting device for collecting a damping column, wherein the damping column is positioned below an unmanned aerial vehicle arm, and the collecting device is characterized by comprising:
the storage box is fixed below the unmanned aerial vehicle arm and is horizontally arranged, the storage box is of a hollow structure, the bottom of the storage box is open, at least one side wall of the storage box is provided with a first groove penetrating through the side wall, the cushioning column is rotatably connected to the inner wall of the storage box, and the storage box is stored in the storage box when the cushioning column rotates to the horizontal position;
the movable sheet is arranged beside the first groove and parallel to the first groove, the size of the first groove can limit the passage of the movable sheet, and two ends of the movable sheet are connected to the storage box through springs;
one end of the connecting rod is fixed on the movable sheet and penetrates through the first groove;
and the movable block is fixed at the other end of the connecting rod and can penetrate through the first groove.
As a further improvement of the present invention, a second groove is provided on the other side wall of the storage box, the second groove is parallel to the first groove, and the movable block can be inserted into the second groove.
As a further improvement of the invention, an inner side wall of the storage box is also rotatably connected with an axially telescopic rod, and the other end of the telescopic rod is installed in a clamping groove of the shock absorption column in a pluggable mode.
As a further improvement of the present invention, the telescopic rod is provided with a first rod body and a second rod body, the outer diameter of the first rod body is larger than the outer diameter of the second rod body, one end of the first rod body is rotatably connected to the side wall of the storage box, one end of the second rod body is installed in the clamping groove of the cushioning column, and the other end of the second rod body is inserted into the other end of the first rod body and can slide therein along the axial direction thereof.
As a further improvement of the present invention, the first groove, the second groove and the movable block are all in a strip structure.
The collecting device has the advantages that the collecting device is arranged, the movable piece is pulled to drive the connecting rod and the movable block to move towards the direction of withdrawing from the storage box, when the movable block completely withdraws from the storage box through the first groove, the telescopic rod is pulled out of the cushioning column, the telescopic rod and the cushioning column are transferred into the storage box, after the telescopic rod and the cushioning column are placed into the storage box, the movable piece is loosened, the spring can drive the movable piece to reset at the moment, the movable piece drives the connecting rod and the movable block to re-enter the storage box through the first groove, the telescopic rod and the cushioning column are contacted in the storage box, the telescopic rod and the cushioning column are prevented from being separated from the storage box, and the problems that the conventional cushioning column cannot be folded when not used and is inconvenient to carry are solved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic view of the shock absorber and the collecting device shown in FIG. 1.
In the figure: 3-a machine arm; 4-a shock absorption column; 7-a collecting device; 71-a storage box; 72-a telescopic rod; 73-connecting rod; 74-a movable plate; 75-a spring; 76-moving block.
Detailed Description
The technical scheme of the invention is further explained by the specific implementation mode in combination with the attached drawings.
As shown in fig. 1, the present invention is provided with a collecting device 7 for collecting the cushioning columns 4, wherein the cushioning columns 4 are located below the unmanned aerial vehicle arm 3, and the collecting device 7 comprises:
the storage box 71 is fixed below the unmanned aerial vehicle arm 3 and horizontally arranged, the storage box 71 is of a hollow structure, the bottom of the storage box 71 is open, at least one side wall of the storage box 71 is provided with a first groove penetrating through the side wall, the cushioning column 4 is rotatably connected to the inner wall of the storage box 71, and the storage box 71 is stored in the storage box 71 when the cushioning column rotates to the horizontal position;
a movable piece 74 disposed beside the first groove and parallel to the first groove, wherein the size of the first groove can limit the passage of the movable piece 74, and two ends of the movable piece 74 are connected to the storage box 71 through springs 75;
a connecting rod 73 having one end fixed to the movable piece 74 and passing through the first groove;
a movable block 76 fixed to the other end of the connecting rod 73, wherein the movable block 76 can pass through the first groove.
The collecting device 7 is arranged, the movable piece 74 is pulled to drive the connecting rod 73 and the movable block 76 to move towards the direction of withdrawing from the storage box 71, when the movable block 76 passes through the first groove and completely withdraws from the storage box 71, the telescopic rod 72 is pulled out of the cushioning column 4, the telescopic rod 72 and the cushioning column 4 are transferred into the storage box 71, after the telescopic rod 72 and the cushioning column 4 are placed into the storage box 71, the movable piece 74 is loosened, at the moment, the spring 75 can drive the movable piece 74 to reset, so that the movable piece 74 drives the connecting rod 73 and the movable block 76 to re-enter the storage box 71 through the first groove, and further contact with the telescopic rod 72 and the cushioning column 4 in the storage box 71, the telescopic rod 72 and the cushioning column 4 are prevented from being separated from the storage box 71, and the problems that the existing cushioning column 4 cannot be retracted when not used and is inconvenient to carry are solved.
As a further improvement of the present invention, a second groove is provided on the other side wall of the storage box 71, the second groove is arranged in parallel with the first groove, and the movable block 76 can be inserted into the second groove.
The invention is provided with a second groove, and the movable block 76 is positioned in the second groove under the action of the spring 75, so that the movable block 76 is limited and fixed.
As a further improvement of the present invention, an inner side wall of the storage box 71 is further rotatably connected with an axially retractable telescopic rod 72, and the other end of the telescopic rod 72 is installed in the slot of the shock absorption post 4 in a pluggable manner.
The telescopic rod 72 is arranged for providing supporting force when the shock absorption column 4 is vertically arranged.
As a further improvement of the present invention, the telescopic rod 72 is provided with a first rod body and a second rod body, the outer diameter of the first rod body is larger than the outer diameter of the second rod body, one end of the first rod body is rotatably connected to the side wall of the storage box 71, one end of the second rod body is installed in the slot of the cushioning column 4, and the other end of the second rod body is inserted into the other end of the first rod body and can slide therein along the axial direction thereof.
The first rod body and the second rod body are arranged, and the telescopic rod 72 can be stretched and retracted by the second rod body moving in the first rod body.
As a further improvement of the present invention, the first groove, the second groove, and the movable block 76 are all of an elongated structure.
The first groove, the second groove and the movable block 76 are all long strip structures, play a role in fool proofing, and prevent the movable block 76 from being separated from the first groove or the second groove when not pulled manually.
The technical principle of the present invention is described above in connection with specific embodiments. The description is made for the purpose of illustrating the principles of the invention and should not be construed in any way as limiting the scope of the invention. Based on the explanations herein, those skilled in the art will be able to conceive of other embodiments of the present invention without inventive effort, which would fall within the scope of the present invention.
Claims (5)
1. The utility model provides an unmanned aerial vehicle shock attenuation collection device, its is equipped with collection device (7) that are used for bradyseism post (4) to collect, bradyseism post (4) are located unmanned aerial vehicle horn (3) below, its characterized in that, collection device (7) include:
the storage box (71) is fixed below the unmanned aerial vehicle arm (3) and horizontally arranged, the storage box (71) is of a hollow structure, the bottom of the storage box is open, at least one side wall of the storage box is provided with a first groove penetrating through the side wall, the cushioning column (4) is rotatably connected to the inner wall of the storage box (71), and the storage box (71) is stored when the cushioning column rotates to the horizontal position;
the movable sheet (74) is arranged beside the first groove and is parallel to the first groove, the size of the first groove can limit the passage of the movable sheet (74), and two ends of the movable sheet (74) are connected to the storage box (71) through springs (75);
a connecting rod (73) with one end fixed on the movable sheet (74) and penetrating through the first groove;
and the movable block (76) is fixed at the other end of the connecting rod (73), and the movable block (76) can penetrate through the first groove.
2. The unmanned aerial vehicle shock attenuation collection device of claim 1, characterized in that, be equipped with the second recess on the other lateral wall of receiver (71), the second recess sets up with first recess is parallel, movable block (76) can insert in the second recess.
3. The unmanned aerial vehicle shock attenuation collection device of claim 2, characterized in that, an axial telescopic link (72) is still connected on an inside wall of receiver (71) in a rotating way, the other end of telescopic link (72) is installed in the draw-in groove of bradyseism post (4) with the mode of can inserting and pull out.
4. The unmanned aerial vehicle shock attenuation collection device of claim 3, characterized in that, telescopic link (72) are equipped with the first body of rod and the second body of rod, the external diameter of the first body of rod is greater than the external diameter of the second body of rod, first body of rod one end is rotated and is connected on the lateral wall of receiver (71), the one end of the second body of rod is installed in the draw-in groove of bradyseism post (4), and the other end inserts another tip of the first body of rod to can follow its axial slip wherein.
5. The shock absorbing and collecting device for unmanned aerial vehicles according to claim 4, wherein the first groove, the second groove and the movable block (76) are all long strip-shaped structures.
Priority Applications (1)
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CN202110959369.5A CN113665801A (en) | 2021-08-20 | 2021-08-20 | Unmanned aerial vehicle shock attenuation collection device |
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CN202110959369.5A CN113665801A (en) | 2021-08-20 | 2021-08-20 | Unmanned aerial vehicle shock attenuation collection device |
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CN202110959369.5A Pending CN113665801A (en) | 2021-08-20 | 2021-08-20 | Unmanned aerial vehicle shock attenuation collection device |
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Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000002034A (en) * | 1999-06-01 | 2000-01-07 | Okuda Seisakusho:Kk | Locking method of wing and housing box using the same |
CN205891217U (en) * | 2016-08-22 | 2017-01-18 | 四川建筑职业技术学院 | Built -in folding horn of multiaxis rotorcraft aircraft shock attenuation undercarriage |
CN206803874U (en) * | 2017-05-03 | 2017-12-26 | 天合富奥汽车安全系统(长春)有限公司 | Size detection cubing between a kind of hinge of control arm two |
CN109398689A (en) * | 2018-11-16 | 2019-03-01 | 东莞理工学院 | A kind of aerial soft robot of wind drive |
CN111824389A (en) * | 2020-07-24 | 2020-10-27 | 浙江点辰航空科技有限公司 | Unmanned aerial vehicle horn subassembly |
CN212125511U (en) * | 2020-01-15 | 2020-12-11 | 广州幽晟科技有限公司 | Unmanned aerial vehicle is with frame shock-absorbing structure that plays |
CN112193428A (en) * | 2020-10-23 | 2021-01-08 | 湖南睿谷电子科技有限公司 | Protection device for unmanned aerial vehicle during flight |
CN212354394U (en) * | 2020-04-13 | 2021-01-15 | 汤方其 | Unmanned aerial vehicle is patrolled and examined to undercarriage folded cascade |
CN213036330U (en) * | 2020-08-24 | 2021-04-23 | 代开磊 | Water sample storage device for environmental monitoring field sampling |
CN213863538U (en) * | 2020-11-10 | 2021-08-03 | 南安市恒发鑫彩印包装有限公司 | Anti-falling gift box |
-
2021
- 2021-08-20 CN CN202110959369.5A patent/CN113665801A/en active Pending
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2000002034A (en) * | 1999-06-01 | 2000-01-07 | Okuda Seisakusho:Kk | Locking method of wing and housing box using the same |
CN205891217U (en) * | 2016-08-22 | 2017-01-18 | 四川建筑职业技术学院 | Built -in folding horn of multiaxis rotorcraft aircraft shock attenuation undercarriage |
CN206803874U (en) * | 2017-05-03 | 2017-12-26 | 天合富奥汽车安全系统(长春)有限公司 | Size detection cubing between a kind of hinge of control arm two |
CN109398689A (en) * | 2018-11-16 | 2019-03-01 | 东莞理工学院 | A kind of aerial soft robot of wind drive |
CN212125511U (en) * | 2020-01-15 | 2020-12-11 | 广州幽晟科技有限公司 | Unmanned aerial vehicle is with frame shock-absorbing structure that plays |
CN212354394U (en) * | 2020-04-13 | 2021-01-15 | 汤方其 | Unmanned aerial vehicle is patrolled and examined to undercarriage folded cascade |
CN111824389A (en) * | 2020-07-24 | 2020-10-27 | 浙江点辰航空科技有限公司 | Unmanned aerial vehicle horn subassembly |
CN213036330U (en) * | 2020-08-24 | 2021-04-23 | 代开磊 | Water sample storage device for environmental monitoring field sampling |
CN112193428A (en) * | 2020-10-23 | 2021-01-08 | 湖南睿谷电子科技有限公司 | Protection device for unmanned aerial vehicle during flight |
CN213863538U (en) * | 2020-11-10 | 2021-08-03 | 南安市恒发鑫彩印包装有限公司 | Anti-falling gift box |
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Application publication date: 20211119 |