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CN-117657489-B - Inspection device for unmanned aerial vehicle and unmanned aerial vehicle thereof

CN117657489BCN 117657489 BCN117657489 BCN 117657489BCN-117657489-B

Abstract

The application relates to the technical field of unmanned aerial vehicle parts, and provides an inspection device for an unmanned aerial vehicle, which comprises a mounting seat, a cover plate and a connecting assembly, wherein the mounting seat is arranged on the mounting seat; the cover plate is rotatably connected to the mounting seat, the connecting assembly comprises a connecting seat, two rotating arms, a torsion spring and a buckle, the connecting seat is arranged in the mounting seat, one ends of the two rotating arms are rotatably connected to the connecting seat, the torsion spring is arranged on the two rotating arms to drive the other ends of the two rotating arms to rotate towards one sides close to each other, a clamping groove is formed between the two rotating arms, and the buckle is arranged on one side, close to the mounting seat, of the cover plate and is clamped in the clamping groove. Based on this, the cover plate can be easily fixed. In addition, an unmanned aerial vehicle is also provided.

Inventors

  • DONG JINZHONG

Assignees

  • 厦门市嘉能科技有限公司

Dates

Publication Date
20260505
Application Date
20231212

Claims (8)

  1. 1. The inspection device for the unmanned aerial vehicle is characterized by comprising a mounting seat (1), a cover plate (2) and a connecting assembly (3), wherein the cover plate (2) is rotatably connected to the mounting seat (1), the connecting assembly (3) comprises a connecting seat (31), two rotating arms (32), a torsion spring (33) and a buckle (34), the connecting seat (31) is arranged in the mounting seat (1), one ends of the two rotating arms (32) are rotatably connected to the connecting seat (31), the torsion spring (33) is arranged on the two rotating arms (32) so as to drive the other ends of the two rotating arms (32) to rotate towards the side close to each other, a clamping groove (35) is formed between the two rotating arms (32), and the buckle (34) is arranged on one side of the cover plate (2) close to the mounting seat (1) and is clamped in the clamping groove (35); The inspection device further comprises a limiting assembly (5) and a pressing assembly (6), wherein the limiting assembly (5) comprises a limiting rod (51) and a first elastic piece (52), the limiting rod (51) is connected to one rotating arm (32) in a sliding mode and is far away from the other rotating arm (32) under the driving of the first elastic piece (52), the clamping buckle (34) is provided with a limiting hole (341), and the pressing assembly (6) is used for pressing the limiting rod (51) so that the limiting rod (51) is inserted into the limiting hole (341); The compression assembly (6) comprises a mounting cylinder (61), a compression rod (62) and a second elastic piece (63), wherein the mounting cylinder (61) is arranged on one side, close to the mounting seat (1), of the cover plate (2), a sliding groove (611) is formed in the inner side of the mounting cylinder (61) along the length direction of the mounting cylinder, a rotating groove (612) is formed in the circumferential direction of the mounting cylinder, the rotating groove (612) is formed in one end, far away from the cover plate (2), of the sliding groove (611), a connecting hole (22) communicated with the inside of the mounting cylinder (61) is formed in the cover plate (2), the compression rod (62) comprises a compression part (621), a limiting part (622) and a rotating part (623), the compression part (621) is movably arranged on the mounting cylinder (61), one end of the compression part (621) is in contact with the limiting rod (51), the limiting part (622) is arranged on one end of the compression part (621) and is limited on the rotating groove (612), the rotating part (623) is arranged on one end, far away from the first elastic piece (63) is arranged between the first end (22) and the limiting piece (63), so as to drive the pressing part (621) away from the limit rod (51).
  2. 2. An inspection apparatus for an unmanned aerial vehicle according to claim 1, wherein the connecting assembly (3) further comprises two rollers (36), the two rollers (36) are respectively provided on the two rotating arms (32), and each of the rollers (36) is rotatably connected to an end of each of the rotating arms (32) which is far away from the rotation of the corresponding one.
  3. 3. The inspection device for the unmanned aerial vehicle according to claim 1, wherein the inspection device further comprises two rotating assemblies (4), the two rotating assemblies (4) are respectively arranged at two ends of the cover plate (2), the rotating assemblies (4) comprise rotating sleeves (41), rotating pieces (42) and fastening pieces (43), the rotating sleeves (41) are arranged on the mounting seat (1), the rotating pieces (42) are rotatably connected with the rotating sleeves (41) and are attached to one side, close to the mounting seat (1), of the cover plate (2), and one end of each fastening piece (43) is movably arranged on the cover plate (2) in a penetrating mode and is threaded on the corresponding rotating piece (42).
  4. 4. The inspection device for an unmanned aerial vehicle according to claim 3, wherein a counter bore (21) is formed in the side, away from the mounting base (1), of the cover plate (2), and one end, away from the rotating plate (42), of the fastening piece (43) is embedded in the counter bore (21).
  5. 5. The inspection apparatus for an unmanned aerial vehicle according to claim 1, wherein a guide groove (512) is provided at an end of the stopper rod (51) near the pressing portion (621).
  6. 6. The inspection device for an unmanned aerial vehicle according to claim 1, wherein the mounting cylinder (61) is provided with a limit groove (613) at one end of the rotation groove (612) away from the sliding groove (611) toward the other end of the sliding groove (611).
  7. 7. An inspection apparatus for an unmanned aerial vehicle according to claim 6, wherein the pressing member (6) further comprises an elastic pad (64), and the elastic pad (64) is provided at one end of the mounting cylinder (61) near the cover plate (2) and abuts against the rotating portion (623).
  8. 8. An unmanned aerial vehicle comprising an inspection apparatus as claimed in any one of claims 1 to 7.

Description

Inspection device for unmanned aerial vehicle and unmanned aerial vehicle thereof Technical Field The application relates to the field of unmanned aerial vehicle components, in particular to an inspection device for an unmanned aerial vehicle and the unmanned aerial vehicle. Background The drone is a drone that is maneuvered with a radio remote control device and a self-contained programming device. Wherein, be equipped with the inspection port on unmanned aerial vehicle's the fuselage, inspection port department is equipped with inspection device to the unmanned aerial vehicle is inspected. In the related art, inspection device includes mount pad and apron, and mount pad fixed connection is in the inspection mouth department of fuselage, and the mount pad offer with the inside inspection hole of intercommunication of fuselage, the apron passes through bolt fixed connection in the mount pad, through dismantling the bolt, opens the apron again and operates, can realize checking unmanned aerial vehicle. However, after the inspection of the unmanned aerial vehicle is completed, the cover plate needs to be locked and fastened again by the bolts so as to fix the cover plate, and the operation is troublesome, so that improvement is needed. Disclosure of Invention In order to facilitate fixing of the cover plate, in a first aspect, the application provides an inspection device for a unmanned aerial vehicle. The application provides an inspection device for an unmanned aerial vehicle, which adopts the following technical scheme: The inspection device for the unmanned aerial vehicle comprises an installation seat, a cover plate and a connecting assembly, wherein the cover plate is rotationally connected to the installation seat, the connecting assembly comprises a connecting seat, two rotating arms, a torsion spring and a buckle, the connecting seat is arranged in the installation seat, one ends of the two rotating arms are rotationally connected to the connecting seat, the torsion spring is arranged on the two rotating arms so as to drive the other ends of the two rotating arms to rotate towards one sides close to each other, a clamping groove is formed between the two rotating arms, and the buckle is arranged on one side, close to the installation seat, of the cover plate and is clamped in the clamping groove. Through adopting above-mentioned technical scheme, after the unmanned aerial vehicle inspection is accomplished, through rotating the apron, so that the buckle passes from between two rotating arms, under the extrusion effect of buckle, two rotating arms rotate and make torsional spring elastic deformation towards one side that keeps away from each other, after two rotating arms were worn to locate to the buckle, the torsional spring resets, so that two rotating arms rotate towards one side that is close to each other in order to order about, be formed with the draw-in groove between two rotating arms, buckle joint is in the draw-in groove this moment, in order to realize fixing to the apron, easy operation is convenient. Preferably, the connecting assembly further comprises two rollers, the two rollers are respectively arranged on the two rotating arms, and each roller is rotatably connected to one end, far away from the rotating arm, of each rotating arm. Through adopting above-mentioned technical scheme, through setting up two gyro wheels, when the buckle passes from between two rotating arms, buckle and two gyro wheels contact for two gyro wheels rotate, with the frictional force that reduces the buckle and pass between two rotating arms, thereby be convenient for buckle joint in the draw-in groove. Preferably, the inspection device further comprises two rotating assemblies, the two rotating assemblies are respectively arranged at two ends of the cover plate, each rotating assembly comprises a rotating sleeve, a rotating sheet and a fastening piece, the rotating sleeve is arranged on the mounting seat, the rotating sheet is rotationally connected with the rotating sleeve and is attached to one side, close to the mounting seat, of the cover plate, and one end of each fastening piece is movably arranged on the cover plate in a penetrating mode and is threaded on the rotating sheet. Through adopting above-mentioned technical scheme, through setting up rotating assembly to realize that the apron rotates to be connected in the mount pad, and be convenient for the installation between apron and the mount pad. Preferably, a countersink is formed in one side, away from the mounting seat, of the cover plate, and one end, away from the rotating piece, of the fastener is embedded into the countersink. Through adopting above-mentioned technical scheme, through setting up the counter bore, avoid the fastener protrusion in the apron as far as possible to reduce the resistance when unmanned aerial vehicle flies. The inspection device comprises a rotating arm, a clamping buckle, a limiting assembly, a limiting hole and