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CN-122009578-A - Aircraft, aircraft assembly and vehicle

CN122009578ACN 122009578 ACN122009578 ACN 122009578ACN-122009578-A

Abstract

The application discloses an aircraft, an aircraft assembly and a vehicle, relates to the technical field of vehicles, and aims to solve the problem of how to reduce the volume of the aircraft assembly. The aircraft is suitable for landing on the air park, the air park comprises an air park body and a limiting part arranged on the air park body, the aircraft comprises an aircraft body, a foot rest and a driving assembly, the foot rest is movably connected with the aircraft body, the driving assembly is connected between the foot rest and the aircraft body in a transmission mode, and the driving assembly can drive at least part of the foot rest to move relative to the aircraft body so as to enable the foot rest and the limiting part of the air park to be matched with each other to adjust the stop position of the aircraft.

Inventors

  • LI JIALIAN
  • ZHAO SHENGLEI
  • CHEN JINGE

Assignees

  • 比亚迪股份有限公司

Dates

Publication Date
20260512
Application Date
20260320

Claims (10)

  1. 1. An aircraft suitable for landing on a parking apron (20), wherein the parking apron (20) comprises a parking apron body (5) and a limiting part (52) arranged on the parking apron body (5), and the aircraft is characterized by comprising an aircraft body (1), a foot rest (2) and a driving component (3), the foot rest (2) is movably connected with the aircraft body (1), and the driving component (3) is in transmission connection between the foot rest (2) and the aircraft body (1); The driving assembly (3) can drive at least part of the foot rest (2) to move relative to the aircraft body (1) so as to enable the foot rest (2) and the limit part (52) of the apron (20) to be matched and adjust the stop position of the aircraft (10).
  2. 2. The aircraft according to claim 1, wherein the foot rest (2) comprises a first foot rest (2 a) and a second foot rest (2 b), the first foot rest (2 a) and the second foot rest (2 b) being both connected to the aircraft body (1); The driving component (3) is in transmission connection with at least one of the first foot rest (2 a) and the second foot rest (2 b) and is used for driving the first foot rest (2 a) and the second foot rest (2 b) to relatively move along opposite directions; And/or said at least one of said first and second footrests (2 a, 2 b) is rotatably connected to said aircraft body (1); The drive assembly (3) is capable of driving the at least one of the first foot rest (2 a) and the second foot rest (2 b) to rotate so as to cause the first foot rest (2 a) and the second foot rest (2 b) to rotate relatively in opposite directions.
  3. 3. The aircraft according to any one of claims 1-2, characterized in that the drive assembly (3) comprises a drive element (31) and a transmission assembly, the drive element (31) being connected with the aircraft body (1), the drive element (31) being in transmission connection with the foot rest (2) by means of the transmission assembly.
  4. 4. An aircraft according to claim 3, wherein the transmission assembly comprises a first transmission member (32) and a second transmission member (33), the foot rest (2) comprising a first foot rest (2 a) and a second foot rest (2 b), the first transmission member (32) being drivingly connected between the driving member (31) and the first foot rest (2 a), the second transmission member (33) being drivingly connected between the driving member (31) and the second foot rest (2 b).
  5. 5. The aircraft according to any one of claims 1-2, wherein the foot rest (2) comprises a mating portion (21) and a guiding portion (22), the mating portion (21) being connected to the aircraft body (1) for contact mating with the limiting portion (52) for pushing the aircraft body (1) to move in a first direction, the guiding portion (22) being connected to the mating portion (21) for contact mating with the limiting portion (52) for pushing the aircraft body (1) to move in a second direction, both the first direction and the second direction being parallel to the bearing surface (51) of the apron (20), and the first direction and the second direction being perpendicular.
  6. 6. The aircraft according to claim 5, characterized in that the mating part (21) is located on the underside of the aircraft body (1), the guide part (22) being connected to the end of the mating part (21) in the second direction, the guide part (22) being located on the side of the mating part (21) that is close to the aircraft body (1).
  7. 7. An aircraft assembly, characterized by comprising an aircraft (10) according to any one of claims 1-6.
  8. 8. The aircraft assembly according to claim 7, further comprising a tarmac (20), the tarmac (20) comprising a tarmac body (5) and a limit stop (52) provided to the tarmac body (5); The parking apron (20) comprises a bearing surface (51) for bearing an aircraft and a parking mark (53) arranged on the bearing surface (51), the limiting part (52) comprises a first limiting part (521) and a second limiting part (522) arranged on the bearing surface (51), the first limiting part (521) and the second limiting part (522) are arranged on the periphery side of the parking mark (53), the second limiting part (522) is arranged on one side, close to the parking mark (53), of the first limiting part (521) and is connected with the first limiting part (521), the first limiting part (521) can be in contact fit with a matching part (21) of the aircraft, and the second limiting part (522) can be in contact fit with a guiding part (22) of the aircraft.
  9. 9. The aircraft assembly of claim 7, wherein the aircraft assembly (300) comprises a plurality of the aircraft (10).
  10. 10. A vehicle characterized by comprising an aircraft (10) according to any one of claims 1-6 and/or an aircraft assembly (300) according to any one of claims 7-9.

Description

Aircraft, aircraft assembly and vehicle Technical Field The application relates to the technical field of vehicles, in particular to an aircraft, an aircraft assembly and a vehicle. Background The aircraft can be used for detecting road conditions, taking photo by plane and the like, for example, a camera is carried on the aircraft, and the road conditions, scenery and the like are shot at high altitude through the camera. In the prior art, an aircraft can be carried on a vehicle, road conditions in front of the vehicle are detected through the aircraft, and road conditions are fed back in real time through a vehicle-to-machine system, so that the running safety of the vehicle is improved. But the structural defects of the existing aircraft assembly result in a bulky aircraft assembly. Disclosure of Invention The application aims to provide an aircraft, an aircraft assembly and a vehicle, and aims to solve the problem of how to reduce the volume of the aircraft assembly. According to the first aspect, the aircraft is suitable for being landed on the parking apron, the parking apron comprises an parking apron body and a limiting part arranged on the parking apron body, the aircraft comprises an aircraft body, a foot rest and a driving assembly, the foot rest is movably connected with the aircraft body, the driving assembly is in transmission connection between the foot rest and the aircraft body, and the driving assembly can drive at least part of the foot rest to move relative to the aircraft body so as to enable the foot rest and the limiting part of the parking apron to be matched with each other to adjust the parking position of the aircraft. In the scheme, the driving assembly can drive at least part of the foot rest of the aircraft to move relative to the aircraft body so as to adjust the stop position of the aircraft through the cooperation of the foot rest and the limiting part of the air park. Compared with the arrangement of the homing structure on the parking apron in the related art, the homing structure on the parking apron pushes the aircraft to be at the preset position, and the homing device realizes homing of the aircraft by moving the foot rest of the aircraft body, so that the volume of the parking apron is effectively reduced, and further the volume of the aircraft component is reduced. Optionally, the foot rest comprises a first foot rest and a second foot rest, wherein the first foot rest and the second foot rest are both connected with the aircraft body, and the driving assembly is in transmission connection with at least one of the first foot rest and the second foot rest and used for driving the first foot rest and the second foot rest to relatively move along opposite directions. Optionally, the at least one of the first foot rest and the second foot rest is rotatably connected with the aircraft body, and the driving assembly can drive the at least one of the first foot rest and the second foot rest to rotate so as to enable the first foot rest and the second foot rest to rotate relatively in opposite directions. Optionally, the driving assembly comprises a driving piece and a transmission assembly, the driving piece is connected with the aircraft body, and the driving piece is in transmission connection with the foot rest by means of the transmission assembly. Optionally, the transmission assembly includes first driving piece and second driving piece, the foot rest includes first foot rest and second foot rest, first driving piece transmission connect in between the driving piece with first foot rest, the second driving piece transmission connect in between the driving piece with the second foot rest. Optionally, the foot rest includes cooperation portion and guide part, cooperation portion connect in the aircraft body, be used for with spacing portion contact cooperation is in order to promote the aircraft body moves along first direction, guide portion connect in cooperation portion is used for with spacing portion contact cooperation is in order to promote the aircraft body moves along the second direction, first direction with the second direction is all parallel to the loading surface of apron, just first direction with the second direction is perpendicular. Optionally, the mating portion is located at a lower side of the aircraft body, the guiding portion is connected to an end portion of the mating portion in the second direction, and the guiding portion is located at a side, close to the aircraft body, of the mating portion. In a second aspect, the present application provides an aircraft assembly, comprising an aircraft. Optionally, the aircraft assembly further comprises an apron, wherein the apron comprises an apron body and a limiting part arranged on the apron body. The parking apron comprises a bearing surface for bearing an aircraft and a parking mark arranged on the bearing surface, wherein the limiting parts comprise a first limiting part and a second limiting part