CN210455180U - Arm folding mechanism for unmanned aerial vehicle - Google Patents

Arm folding mechanism for unmanned aerial vehicle Download PDF

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Publication number
CN210455180U
CN210455180U CN201921500686.5U CN201921500686U CN210455180U CN 210455180 U CN210455180 U CN 210455180U CN 201921500686 U CN201921500686 U CN 201921500686U CN 210455180 U CN210455180 U CN 210455180U
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CN
China
Prior art keywords
locking piece
pipe clamp
connecting rod
hinged
folding mechanism
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CN201921500686.5U
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Chinese (zh)
Inventor
李勇
李一鸣
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Zhongshan Huaao Yihang Technology Co ltd
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Zhongshan Huaao Yihang Technology Co ltd
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Priority to CN201921500686.5U priority Critical patent/CN210455180U/en
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Abstract

The utility model provides an unmanned vehicles is with horn folding mechanism, belong to unmanned vehicles technical field, the utility model discloses a well beam slab, moving part and pipe clamp, well beam slab is articulated with moving part one end, the other end and the pipe clamp of moving part are articulated, the pipe clamp is articulated to be installed on well beam slab, be provided with the bracing piece on the well beam slab, the one end and the bracing piece of connecting rod are articulated, the other end of connecting rod is articulated with the other end of locking piece, the other end of locking piece is articulated to be installed on the pipe clamp, be provided with on the locking piece and be used for the spacing trip of connecting rod, connecting seat fixed mounting is on the connecting pipe, the cartridge has the pivot on the connecting seat, the rotatable suit of locking piece is in the pivot, still be provided with round bar and circular arc trip on the connecting seat, the cover is equipped with the horn spring on the round bar. The utility model discloses a folding mechanism adopts the integration setting, not only saves space, convenient transportation and carrying, simple structure moreover, convenient operation.

Description

Arm folding mechanism for unmanned aerial vehicle
Technical Field
The utility model relates to a horn folding mechanism for unmanned vehicles belongs to unmanned vehicles technical field.
Background
The Chinese unmanned aerial vehicle attracts attention not only in forming a complete series with complete varieties and various functions, but also in improving performance indexes thereof continuously. Make its horn have foldability through designing unmanned vehicles, consequently can reduce unmanned aerial vehicle's parking space, but current unmanned aerial vehicle horn beta structure adopts the bolt fastening more, the dismouting is inconvenient, or adopt buckle or round pin hub fixation, there is the space between the back and the frame to expand by structure restriction horn, perhaps round pin axle strength is limited, especially to the great unmanned aerial vehicle of some loads, round pin axle deformation produces the space after folding horn uses a period, just so caused the life weak point of horn, and the maintenance difficulty, very big waste has been caused. Different folding mechanisms therefore face the same technical difficulties, namely that the folding mechanism is not sufficiently tight, the unfolding operation is cumbersome and the working efficiency is low.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the technical problem and further providing an unmanned aerial vehicle is with horn folding mechanism.
The technical scheme of the utility model:
a machine arm folding mechanism for an unmanned aerial vehicle comprises a middle beam plate, a moving part and a pipe clamp, wherein the middle beam plate is hinged with one end of the moving part, the other end of the moving part is hinged with the pipe clamp, and the pipe clamp is hinged on the middle beam plate;
the middle beam plate is provided with a supporting rod, the moving part comprises a connecting rod and a locking piece, one end of the connecting rod is hinged with the supporting rod, the other end of the connecting rod is hinged with one end of the locking piece, the other end of the locking piece is hinged to the pipe clamp, and the locking piece is provided with a clamping tenon for limiting the connecting rod;
the pipe clamp comprises a connecting pipe and a connecting seat, the connecting seat is fixedly mounted on the connecting pipe, a rotating shaft is arranged on the connecting seat in an inserted mode, a locking piece is rotatably sleeved on the rotating shaft, a round rod and an arc clamping tenon are further arranged on the connecting seat, an arm spring is sleeved on the round rod, one end of a spring arm of the arm spring is attached to the locking piece, and the other end of the spring arm is attached to the arc clamping tenon.
Furthermore, a spring cover is arranged at the end part of the rotating shaft and covers the machine arm spring and the arc clamping tenon.
Furthermore, an included angle between the connecting rod and an inner angle A formed when the locking piece is in the unfolding state is an obtuse angle.
The utility model discloses following beneficial effect has: the utility model realizes the folding action of the machine arm by the moving part arranged between the support rod and the pipe clamp, and the tenon arranged on the locking piece directly limits the rotation of the connecting rod, so that the connecting rod forms a rigid structure when being unfolded and can be automatically locked when being folded; the utility model discloses a folding mechanism adopts the integration setting, not only saves space, convenient transportation and carrying, simple structure moreover, convenient operation.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of a center sill panel;
FIG. 3 is a schematic view of the latch member;
FIG. 4 is a schematic view of the construction of the pipe clamp;
FIG. 5 is a schematic view of the overall structure of the installation site of the present invention;
fig. 6 is a schematic structural view of the movable member of the present invention in a folded state;
in the figure, 1-a middle beam plate, 2-a movable piece, 3-a pipe clamp, 11-a support rod, 21-a connecting rod, 22-a locking piece, 221-a clamping tenon, 31-a connecting pipe, 32-a connecting seat, 321-a round rod, 322-an arc clamping tenon, 33-an arm spring, 34-a rotating shaft and 35-a spring cover.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings.
The embodiment is described with reference to fig. 1 to 5, and the arm folding mechanism for the unmanned aerial vehicle comprises a middle beam plate 1, a movable member 2 and a pipe clamp 3, wherein the middle beam plate 1 is hinged to one end of the movable member 2, the other end of the movable member 2 is hinged to the pipe clamp 3, and the pipe clamp 3 is hinged to the middle beam plate 1; according to the arrangement, the pipe clamp can be driven to swing through the movement of the movable piece, the support rod 11 is arranged on the middle beam plate 1, the movable piece 2 comprises the connecting rod 21 and the locking piece 22, one end of the connecting rod 21 is hinged to the support rod 11, the other end of the connecting rod 21 is hinged to one end of the locking piece 22, the other end of the locking piece 22 is hinged to the pipe clamp 3, and the locking piece 22 is provided with the tenon 221 for limiting the connecting rod 21; the locking piece is provided with the clamping tenon, when the connecting rod and the locking piece move relatively, the connecting rod stops moving when being tightly propped against the clamping tenon, and the limiting effect on the connecting rod is achieved; the pipe clamp 3 comprises a connecting pipe 31 and a connecting seat 32, the connecting seat 32 is fixedly installed on the connecting pipe 31, a rotating shaft 34 is inserted on the connecting seat 32, a locking piece 22 is rotatably sleeved on the rotating shaft 34, a round rod 321 and an arc-shaped tenon 322 are further arranged on the connecting seat 32, an arm spring 33 is sleeved on the round rod 321, one end of a spring arm of the arm spring 33 is attached to the locking piece 22, and the other end of the spring arm is attached to the arc-shaped tenon 322; the arc clamping tenon and the rotating shaft are used for extruding the machine arm spring, and when the locking piece arranged on the rotating shaft rotates, the machine arm spring is released; preferably, four groups of folding mechanisms are arranged and distributed at four end corners of the middle beam plate; further optimizing, an included angle of an inner angle A formed when the connecting rod 21 and the locking piece 22 are in the unfolding state is an obtuse angle; so set up, increased the swing range of pipe clamp on the one hand, on the other hand conveniently carries out spacing messenger's structure more stable.
The utility model realizes the unfolding and folding actions of the pipe clamp 3 relative to the support rod 11 by the hinge connection of the moving part 2 with the support rod 11 and the pipe clamp 3 respectively, the moving part 2 consists of the connecting rod 21 and the locking part 22, the locking part 22 is also provided with the tenon 221, when the pipe clamp 3 is in the unfolding state, the connecting rod 21 and the locking part 22 are both in the stretching state, the connecting seat 32 of the pipe clamp 3 is also provided with the arm spring 33, under the releasing force action of the arm spring 33 and the manual assistance, the tenon 221 on the locking part 22 is contacted with the end part of the connecting rod 21, namely, the limit value of the stretching state is reached, the tenon 221 performs the limit action on the connecting rod 21, when the folding is needed, the connecting rod 21 and the locking part 22 are released to limit for folding action by applying force to the connecting point of the connecting rod 21 and the locking part 22, the connecting rod 21 and the locking part 22 are continuously close to each other, and finally, the folding mechanism is automatically locked when the pipe clamp 3 is reset by applying force.
This embodiment is only illustrative of the patent and does not limit the scope of protection thereof, and those skilled in the art can make modifications to its part without departing from the spirit of the patent.

Claims (3)

1. The horn folding mechanism for the unmanned aerial vehicle is characterized by comprising a middle beam plate (1), a moving part (2) and a pipe clamp (3), wherein the middle beam plate (1) is hinged with one end of the moving part (2), the other end of the moving part (2) is hinged with the pipe clamp (3), and the pipe clamp (3) is hinged to the middle beam plate (1);
a support rod (11) is arranged on the middle beam plate (1), the movable part (2) comprises a connecting rod (21) and a locking piece (22), one end of the connecting rod (21) is hinged to the support rod (11), the other end of the connecting rod (21) is hinged to one end of the locking piece (22), the other end of the locking piece (22) is hinged to the pipe clamp (3), and a clamping tenon (221) used for limiting the connecting rod (21) is arranged on the locking piece (22);
pipe clamp (3) are including connecting pipe (31) and connecting seat (32), connecting seat (32) fixed mounting is in on connecting pipe (31), the cartridge has pivot (34) on connecting seat (32), the rotatable suit of locking piece (22) is in on pivot (34), still be provided with round bar (321) and circular arc trip (322) on connecting seat (32), the cover is equipped with horn spring (33) on round bar (321), the spring arm one end and the laminating of locking piece (22) of horn spring (33), the other end and the laminating of circular arc trip (322).
2. The folding mechanism of the unmanned aerial vehicle arm is characterized in that a spring cover (35) is installed at the end of the rotating shaft (34), and the spring cover (35) covers the arm spring (33) and the arc tenon (322).
3. The folding mechanism of unmanned aerial vehicle arm according to claim 1, wherein an included angle a formed by the link (21) and the lock member (22) in the unfolded state is an obtuse angle.
CN201921500686.5U 2019-09-10 2019-09-10 Arm folding mechanism for unmanned aerial vehicle Active CN210455180U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921500686.5U CN210455180U (en) 2019-09-10 2019-09-10 Arm folding mechanism for unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921500686.5U CN210455180U (en) 2019-09-10 2019-09-10 Arm folding mechanism for unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN210455180U true CN210455180U (en) 2020-05-05

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921500686.5U Active CN210455180U (en) 2019-09-10 2019-09-10 Arm folding mechanism for unmanned aerial vehicle

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CN (1) CN210455180U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111731466A (en) * 2020-06-10 2020-10-02 中山福昆航空科技有限公司 Aircraft with automatic folding wings
CN111959771A (en) * 2020-08-18 2020-11-20 北京京东乾石科技有限公司 Frame and unmanned aerial vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111731466A (en) * 2020-06-10 2020-10-02 中山福昆航空科技有限公司 Aircraft with automatic folding wings
CN111959771A (en) * 2020-08-18 2020-11-20 北京京东乾石科技有限公司 Frame and unmanned aerial vehicle
CN111959771B (en) * 2020-08-18 2021-11-30 北京京东乾石科技有限公司 Frame and unmanned aerial vehicle

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