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CN-224225329-U - Foldable unmanned aerial vehicle

CN224225329UCN 224225329 UCN224225329 UCN 224225329UCN-224225329-U

Abstract

The utility model relates to an unmanned aerial vehicle technical field, an embodiment of the disclosure provides a collapsible unmanned aerial vehicle, it includes fuselage and installation arm, install a plurality of installation arms on the fuselage, still include the transfer line, collapsible wing, the retainer plate, butt positioning mechanism, installation cover and joint mechanism, the transfer line rotates and installs on the installation arm, collapsible wing has been cup jointed on the transfer line, collapsible wing follows the synchronous rotation of transfer line, a plurality of retainer plates are installed through the mounting panel to the downside of fuselage, butt positioning mechanism cup joints on the transfer line, and can follow the vertical movement of transfer line, butt positioning mechanism is used for the butt to the retainer plate to the transfer line location, the installation cover cup joints on the transfer line, the installation cover follows the synchronous rotation of transfer line. Through above-mentioned technical scheme for solve among the prior art unmanned aerial vehicle wing and be difficult to fold, lead to unmanned aerial vehicle whole volume great, be inconvenient for accomodate the technical problem who carries.

Inventors

  • TAN LEI
  • FENG YUHUI
  • LIU LEI
  • TIAN YANG
  • ZHAO LIQIANG

Assignees

  • 河北凯为航空科技有限公司

Dates

Publication Date
20260512
Application Date
20250624

Claims (10)

  1. 1. The utility model provides a collapsible unmanned aerial vehicle, includes fuselage (1) and installation arm (2), install a plurality of on fuselage (1) installation arm (2), its characterized in that still includes: The transmission rod (3) is rotatably arranged on the mounting arm (2), the transmission rod (3) is sleeved with the foldable wing (4), and the foldable wing (4) synchronously rotates along with the transmission rod (3); The positioning rings (5) are arranged on the lower side of the machine body (1) through mounting plates, and a plurality of positioning rings (5) are arranged on the lower side of the machine body; The abutting positioning mechanism is sleeved on the transmission rod (3) and can vertically move along the transmission rod (3), and the abutting positioning mechanism is used for abutting on the positioning ring (5) to position the transmission rod (3); The installation cover (6), install cover (6) cup joint on transfer line (3) install cover (6) follow transfer line (3) synchronous rotation, the outside of install cover (6) is provided with joint mechanism, joint mechanism is used for right butt positioning mechanism is in the position location on transfer line (3).
  2. 2. The foldable drone of claim 1, wherein the abutment positioning mechanism comprises: The mounting bracket (101) is sleeved on the transmission rod (3) and can vertically move along the transmission rod (3); The abutting positioning seat (102) is arranged on the upper side of the mounting bracket (101) through a vertical rod, and can synchronously move along with the transmission rod (3); And a clamping plate (103), wherein the clamping plate (103) is mounted on the mounting bracket (101) and can synchronously move along with the mounting bracket (101).
  3. 3. The foldable drone of claim 2, wherein the clamping mechanism comprises: A housing (201), the housing (201) being mounted outside the mounting cover (6); The adjusting rod (202) is horizontally movably inserted into the outer side of the shell (201); A sliding plate (203), wherein the sliding plate (203) is mounted on the adjusting rod (202) and can synchronously move along with the adjusting rod (202); A clamping block (204), wherein the clamping block (204) is arranged on the sliding plate (203) and can synchronously move along with the sliding plate (203); The spring (205), the spring (205) cup joints on adjusting lever (202), both ends of spring (205) respectively with casing (201) with sliding plate (203).
  4. 4. A foldable unmanned aerial vehicle according to claim 3, wherein the transmission rod (3) is provided with square bars, and the inner side of the mounting bracket (101) is provided with square grooves.
  5. 5. The foldable drone of claim 4, wherein the upper side of the abutment seat (102) is provided with a non-slip pad.
  6. 6. A foldable unmanned aerial vehicle according to claim 2, wherein the outer side of the mounting cover (6) is provided with a movement opening, the outer side of the mounting bracket (101) is provided with an adjusting member, and the width of the movement opening is adapted to the width of the adjusting member.
  7. 7. A foldable unmanned aerial vehicle according to claim 3, wherein the clamping plate (103) is provided with a clamping groove, and the width of the clamping groove is adapted to the width of the clamping block (204).
  8. 8. A foldable drone according to claim 1, characterized in that the exterior of the mounting arm (2) is provided with a receiving slot, the height of which is adapted to the height of the foldable wing (4).
  9. 9. A foldable drone according to claim 3, characterized in that the interior of the housing (201) is fitted with a sliding rail on which the sliding plate (203) is slidingly connected.
  10. 10. The foldable unmanned aerial vehicle of claim 9, wherein a limit baffle is mounted on the inner side of the sliding rail, and a buffer layer is arranged inside the limit baffle.

Description

Foldable unmanned aerial vehicle Technical Field The embodiment of the disclosure relates to the technical field of unmanned aerial vehicles, in particular to a foldable unmanned aerial vehicle. Background Unmanned aircraft, for short, "unmanned aircraft", is unmanned aircraft that is maneuvered using radio remote control devices and self-contained programming devices, or is operated autonomously, either entirely or intermittently, by an onboard computer, and is often more suited to tasks that are too "fool, messy, or dangerous" than unmanned aircraft; Unmanned aerial vehicle wing among the prior art is difficult to fold, leads to unmanned aerial vehicle whole volume great, is inconvenient for accomodating it when not using unmanned aerial vehicle, leads to comparatively troublesome when carrying unmanned aerial vehicle, though have wing foldable unmanned aerial vehicle, but the wing after its folding takes place not hard up phenomenon easily, influences the carrying to unmanned aerial vehicle easily. Disclosure of utility model In order to overcome the above-mentioned defect, the embodiment of the present disclosure provides a foldable unmanned aerial vehicle for solve the technical problems that unmanned aerial vehicle wings in related art/prior art are difficult to fold, resulting in the overall size of the unmanned aerial vehicle being larger, and being inconvenient to store and carry. According to one aspect, at least one embodiment of the present disclosure provides a foldable unmanned aerial vehicle, including a fuselage and a mounting arm, the fuselage having a plurality of the mounting arms mounted thereon, further comprising: The transmission rod is rotatably arranged on the mounting arm, a foldable wing is sleeved on the transmission rod, and the foldable wing synchronously rotates along with the transmission rod; The lower side of the machine body is provided with a plurality of positioning rings through a mounting plate; The abutting positioning mechanism is sleeved on the transmission rod and can vertically move along the transmission rod, and is used for abutting on the positioning ring to position the transmission rod; The installation cover is sleeved on the transmission rod and synchronously rotates along with the transmission rod, and a clamping mechanism is arranged on the outer side of the installation cover and used for positioning the position of the abutting positioning mechanism on the transmission rod. In order to achieve positioning of the position of the foldable wing on the mounting arm, the abutment positioning mechanism comprises: the mounting bracket is sleeved on the transmission rod and can vertically move along the transmission rod; The abutting positioning seat is arranged on the upper side of the mounting bracket through a vertical rod and can synchronously move along with the transmission rod; The clamping plate is installed on the mounting bracket and can synchronously move along with the mounting bracket. In order to realize the location to butt positioning mechanism on the transfer line, joint mechanism includes: A housing mounted on an outer side of the mounting cover; The adjusting rod is horizontally movably inserted into the outer side of the shell; the sliding plate is arranged on the adjusting rod and can synchronously move along with the adjusting rod; the clamping block is arranged on the sliding plate and can synchronously move along with the sliding plate; The spring is sleeved on the adjusting rod, and two ends of the spring are respectively connected with the shell and the sliding plate. In order to ensure the stability of the mounting bracket during movement, the square bar is arranged on the transmission rod, and a square groove is formed in the inner side of the mounting bracket. In order to enhance the positioning effect of the abutting positioning seat, an anti-slip pad is arranged on the upper side of the abutting positioning seat. In order to realize the adjustment to butt positioning mechanism to transfer line locate mode, the removal opening has been seted up to the outside of installing the cover, the regulating part is installed to the outside of installing the bracket, remove the open-ended width with the width looks adaptation of regulating part. In order to realize the joint between joint board and the joint piece, offered the joint groove on the joint board, the width in joint groove with the width looks adaptation of joint piece. In order to accommodate the folded part of the foldable wing, an accommodating groove is formed in the outer portion of the mounting arm, and the height of the accommodating groove is matched with the height of the foldable wing. In order to ensure the stability of the sliding plate during movement, a sliding rail is arranged in the shell, and the sliding plate is connected to the sliding rail in a sliding manner. In order to realize the stop limit to the sliding plate, a limit baffle is installed on the inner sid