CN213832090U

CN213832090U - Multi-rotor unmanned aerial vehicle wing tip lock catch

Info

Publication number: CN213832090U
Application number: CN202022906229.5U
Authority: CN
Inventors: 鄂云翔
Original assignee: Wuhan Yuli Mechanical Equipment Co ltd
Current assignee: Wuhan Yuli Mechanical Equipment Co ltd
Priority date: 2020-12-07
Filing date: 2020-12-07
Publication date: 2021-07-30
Anticipated expiration: 2030-12-07

Abstract

The utility model discloses a many rotor unmanned aerial vehicle wingtip hasp, including two bases, first diaphragm, second diaphragm, connecting plate, buckle and regulation post, two through the fixed joint of detaining, below between the base the inner wall bottom fixedly connected with installation piece of base, the top fixed connection and the first diaphragm of installation piece, above-mentioned the inside sliding connection of base has the second diaphragm, the positive fixedly connected with slide of second diaphragm, and the positive sliding connection of slide has quantity to be two connecting plates. The utility model discloses a use of base and buckle can make the better aggregate erection of base, and fixed form is nimble more, uses the fixed spacing that can adjust between the wing tip through the cooperation of first diaphragm, ball and slide, guarantees fixed regulation convenience more, and fixed effect is better, can hand the pull rod through the use of kelly and carry out the regulation of position to the buckle to make the removal of buckle become convenience more.

Description

Multi-rotor unmanned aerial vehicle wing tip lock catch

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to a many rotor unmanned aerial vehicle wingtip hasp.

Background

The unmanned plane is called 'unmanned plane' for short, and is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and the unmanned plane is a general name of the unmanned plane in fact, and can be defined as follows from the technical point of view: compared with manned aircraft, the unmanned fixed wing aircraft has the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.

The unmanned aerial vehicle correlation technique rapid development at home and abroad, unmanned aerial vehicle system is of a great variety, the wide characteristics of usage are bright, cause it at the size, the quality, the voyage, the time of flight, flight height, flying speed, many-sided difference such as task all have, and current unmanned aerial vehicle is not stable enough when parking, and traditional mechanical fixed mode or plug-in type fixed mode, it is fixed with the mode that unmanned aerial vehicle fuselage and unmanned aerial vehicle wing adopted screw and nut, and this kind of structure is complicated, fixed regulation is inconvenient, therefore we have proposed a many rotor unmanned aerial vehicle wing tip hasp and have solved above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

For overcoming the problem that exists among the correlation technique, the embodiment of the utility model provides a many rotor unmanned aerial vehicle wingtip hasp has solved the inconvenient problem of present unmanned aerial vehicle wing fixed regulation.

The embodiment of the utility model provides a wing tip lock catch of multi-rotor unmanned aerial vehicle, which comprises two bases, a first transverse plate, a second transverse plate, a connecting plate, a retaining ring and an adjusting column, wherein the two bases are clamped through a fixing buckle, the lower part of the base is fixedly connected with an installation block at the bottom of the inner wall of the base, the top of the installation block is fixedly connected with the first transverse plate, the aforesaid the inside sliding connection of base has the second diaphragm, and the front fixedly connected with slide of second diaphragm, the front sliding connection of slide have quantity be two connecting plates, fixedly connected with have the buckle of elasticity limit on the connecting plate, the top fixedly connected with ball of connecting plate, ball and slide sliding connection, the bottom of connecting plate is rotated and is connected with the rotation post, rotates post and first diaphragm sliding connection, top the inner wall top fixedly connected with quantity of base is two spring posts, two spring posts and second diaphragm fixed connection.

Further, the left side and the right side of the second transverse plate are provided with balls, and the two balls are connected with the base in a sliding mode.

Furthermore, a soft pad is fixedly connected to the inner ring of the retaining ring, and the thickness of the soft pad is not less than two centimeters.

Furthermore, the side face of the retaining ring is fixedly connected with a connecting block, and the side face of the connecting block is rotatably connected with a pull rod.

Furthermore, the inner wall of base is located fixedly connected with stopper between two spring posts, the maximum elastic limit of the height of stopper and spring post.

The embodiment of the utility model provides a technical scheme has following beneficial effect: through the use of base and buckle, can make the better aggregate erection of base, fixed form is more nimble, uses the fixed spacing that can adjust between the wing tip through the cooperation of first diaphragm, ball and slide, guarantees that fixed regulation is more convenient, and fixed effect is better, can hand the pull rod through the use of kelly and carry out the regulation of position to the buckle to the removal that makes the buckle becomes more convenient.

It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention as claimed.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the invention and together with the description, serve to explain the principles of the invention.

Fig. 1 is the embodiment of the utility model provides an in the embodiment structure schematic diagram of many rotor unmanned aerial vehicle wingtip hasp.

Fig. 2 is the embodiment of the utility model provides an in the embodiment buckle structure schematic diagram of many rotor unmanned aerial vehicle wingtip hasp.

Detailed Description

Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, like numbers in different drawings represent the same or similar elements unless otherwise indicated. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with the present invention. Rather, they are merely examples of apparatus, and associated applications, methods, consistent with certain aspects of the invention, as detailed in the following claims.

FIG. 1 is a schematic view of a multi-rotor unmanned aerial vehicle wing tip lock in an embodiment of the present invention, FIG. 2 is a schematic view of a buckle ring structure of the multi-rotor unmanned aerial vehicle wing tip lock in an embodiment of the present invention, as shown in FIGS. 1 and 2, the multi-rotor unmanned aerial vehicle wing tip lock comprises two bases 1, a first transverse plate 3, a second transverse plate 4, a connecting plate 7, a buckle ring 8 and an adjusting post 11, the two bases are connected by a fixing buckle 15, the bases can be assembled better, the fixing form is more flexible, the bottom of the inner wall of the base below is fixedly connected with an installing block 2, the top of the installing block is fixedly connected with the first transverse plate, the inside of the base is slidably connected with the second transverse plate, the left and right sides of the second transverse plate are both provided with balls 5, the distance between the fixing clamps can be adjusted according to the width of the wing, the two balls are slidably connected with the bases, the front of the second transverse plate is fixedly connected with a sliding plate 6, the front sliding connection of slide has the connecting plate that quantity is two, and fixedly connected with has the buckle of elasticity limit on the connecting plate, pulling the buckle in the time of can assisting second diaphragm to adjust the fixed spacing, and the inner ring department fixedly connected with cushion 9 of buckle, the thickness of cushion is not less than two centimeters, can prevent that the buckle from wearing the wing tip, and the integrality of assurance wing tip is better.

The side surface of the retaining ring is fixedly connected with a connecting block, the side surface of the connecting block is rotatably connected with a pull rod 12, the pull rod can be held by hand to adjust the position of the retaining ring, thereby the movement of the retaining ring becomes more convenient, the top of the connecting plate is fixedly connected with a ball 10 which is connected with the sliding plate in a sliding way, the movement of the connecting plate is ensured to be smoother and smoother, the bottom of the connecting plate is rotatably connected with a rotating column which is connected with the first transverse plate in a sliding way, the use angle of the retaining ring can be adjusted while the movement adjustment is assisted, the top of the inner wall of the upper base is fixedly connected with two spring columns 13, the two spring columns are fixedly connected with the second transverse plate, make to remove more stable and safety of adjusting, the inner wall of base is located fixedly connected with stopper 14 between two spring posts, and the limit of regulation can be guaranteed to the high maximum elasticity limit with the spring post of stopper to prevent that the spring post from adjusting excessively and causing the damage of spring post.

Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. This application is intended to cover any variations, uses, or adaptations of the invention following, in general, the principles of the invention and including such departures from the present disclosure as come within known or customary practice within the art to which the invention pertains.

It will be understood that the invention is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the present invention is limited only by the appended claims.

Claims

1. A wing tip lock catch of a multi-rotor unmanned aerial vehicle is characterized by comprising two bases, a first transverse plate, a second transverse plate, a connecting plate, a retaining ring and an adjusting column, wherein the two bases are clamped through a fixing buckle, the bottom of the inner wall of the lower base is fixedly connected with an installation block, the top of the installation block is fixedly connected with the first transverse plate, the aforesaid the inside sliding connection of base has the second diaphragm, and the front fixedly connected with slide of second diaphragm, the front sliding connection of slide have quantity be two connecting plates, fixedly connected with have the buckle of elasticity limit on the connecting plate, the top fixedly connected with ball of connecting plate, ball and slide sliding connection, the bottom of connecting plate is rotated and is connected with the rotation post, rotates post and first diaphragm sliding connection, top the inner wall top fixedly connected with quantity of base is two spring posts, two spring posts and second diaphragm fixed connection.

2. The multi-rotor unmanned aerial vehicle wingtip latch of claim 1, wherein the second cross plate is provided with balls on both sides, both balls being slidably connected to the base.

3. The multi-rotor unmanned wingtip latch of claim 1, wherein a soft pad is fixedly attached to the inner ring of the grommet, the soft pad having a thickness of no less than two centimeters.

4. The multi-rotor unmanned wing tip latch of claim 1, wherein a connection block is fixedly attached to a side of the retaining ring, and a pull rod is rotatably attached to a side of the connection block.

5. The multi-rotor unmanned aerial vehicle wingtip lock according to claim 1, wherein the inner wall of the base is located between two spring posts and is fixedly connected with a limiting block, and the height of the limiting block and the maximum elastic limit of the spring posts are limited.