CN214690230U

CN214690230U - A equipment fixing frame for unmanned aerial vehicle

Info

Publication number: CN214690230U
Application number: CN202023344056.9U
Authority: CN
Inventors: 谭钰峰; 生文强; 吕芳; 刘发; 李庚泽; 秦玮键; 董盛博; 毛喆恺
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-12-31
Filing date: 2020-12-31
Publication date: 2021-11-12
Anticipated expiration: 2030-12-31

Abstract

The utility model belongs to the technical field of unmanned aerial vehicle's equipment fixing rack, especially, be an equipment fixing rack for unmanned aerial vehicle, including the mount pad, the bilateral symmetry of mount pad is provided with a set of connecting block, the top symmetry of mount pad has seted up a set of installation cavity, two connect through the top cap between the installation cavity, the bottom of top cap just is located be provided with the mounting panel in the installation cavity, the bottom of mounting panel through spring one with the installation cavity is connected, just be located one side of mounting panel in the installation cavity is provided with the release assembly that cooperatees with the top cap, the intermediate position of connecting block has seted up the connection chamber, be provided with coupling assembling in the connection chamber, the bilateral symmetry of top cap has seted up a set of movable chamber; when needs are changed the motor or when the motor breaks down out of work, can be quick dismantle convenient to use between mount pad and the unmanned aerial vehicle.

Description

A equipment fixing frame for unmanned aerial vehicle

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle's equipment fixing rack, concretely relates to an equipment fixing rack for unmanned aerial vehicle.

Background

Drones are often more suited to tasks that are too fool, dirty, or dangerous than manned aircraft. Unmanned aerial vehicles can be classified into military and civil according to application fields. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the application of the unmanned aerial vehicle industry is really just needed by the unmanned aerial vehicle, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the application of the industry and developing the unmanned aerial vehicle technology.

The existing unmanned aerial vehicle provides power through the motor when in operation, so that the unmanned aerial vehicle can adapt to mounting frames of different motors, great convenience can be provided for workers when assembling the unmanned aerial vehicle, the mounting frame of the motor of the existing unmanned aerial vehicle is matched through the arrangement of the mounting plate, the mainboard, the supporting plate and the like, although the mounting frame can be adjusted according to the type of the motor to be installed, in the specific use process, on one hand, the mounting seat is connected with the unmanned aerial vehicle through bolts, the connection mode can ensure that the mounting seat is more stable in the working process, but the mounting seat can be disassembled under the condition of using tools when the motor needs to be replaced, so that the unmanned aerial vehicle is inconvenient to use, and on the other hand, the sealing cover is installed between the sealing cover and the mounting seat through screws, so that when the motor does not work, the sealing cover needs to be disassembled by using tools first by the workers, after the motor is overhauled, the sealing cover is installed through tools, so that workers are not convenient to use, meanwhile, the time for detaching and installing the motor is prolonged, and the working efficiency is greatly reduced.

For solving the above problem, the utility model provides an equipment fixing frame for unmanned aerial vehicle in this application.

SUMMERY OF THE UTILITY MODEL

To solve the problems set forth in the background art described above. The utility model provides an equipment fixing frame for unmanned aerial vehicle has the characteristics that have improved work efficiency and convenient to use.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an equipment fixing frame for unmanned aerial vehicle, includes the mount pad, the bilateral symmetry of mount pad is provided with a set of connecting block, a set of installation cavity, two have been seted up to the top symmetry of mount pad connect through the top cap between the installation cavity, the bottom of top cap just is located be provided with the mounting panel in the installation cavity, the bottom of mounting panel pass through spring one with the installation cavity is connected, just be located in the installation cavity one side of mounting panel be provided with top cap matched with release assembly, the connection chamber has been seted up to the intermediate position of connecting block, be provided with coupling assembling in the connection chamber, a set of movable chamber has been seted up to the bilateral symmetry of top cap, be provided with in the movable chamber with release assembly matched with drive assembly.

As the utility model relates to an equipment mounting bracket is preferred for unmanned aerial vehicle, the release subassembly is including setting up the gear in the installation cavity, one side of gear is provided with the rack, the top of rack be provided with drive assembly matched with scarf.

As the utility model relates to an equipment mounting bracket is preferred for unmanned aerial vehicle, the release subassembly alternates to set up the release axle of gear intermediate position, the release axle is kept away from the one end of gear extends to the outside and the release button of mount pad are connected.

As the utility model relates to an equipment fixing frame for unmanned aerial vehicle is preferred, coupling assembling is including setting up connect the connecting axle of intracavity, the bottom of connecting axle extends to the one end of connecting block is connected with the connection button, the connecting axle is kept away from the one end of connecting the button is provided with the connecting rod.

As the utility model relates to an equipment mounting bracket is preferred for unmanned aerial vehicle, coupling assembling is still including setting up just be located on the connecting axle the connecting rod with connection pad between the connection button, just be located on the connecting axle the connection pad is close to one side of connecting rod is provided with spring two.

As the utility model relates to an equipment fixing frame for unmanned aerial vehicle is preferred, drive assembly is including setting up spring three in the activity intracavity, spring three is kept away from the one end of activity intracavity chamber be provided with scarf matched with drive block.

Compared with the prior art, the beneficial effects of the utility model are that: cooperate through setting up devices such as release subassembly, coupling assembling and drive assembly to in concrete use, under the prerequisite of not using tools, just can dismantle mount pad and top cap and install, and then when needs are changed the motor or when the motor breaks down out of work, can be quick dismantle between mount pad and the unmanned aerial vehicle, and then convenient to use.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a schematic structural view of the present invention;

FIG. 2 is an enlarged view of a portion A of FIG. 1;

FIG. 3 is a partially enlarged view of the structure at B in FIG. 1;

in the figure: 1. a mounting seat; 2. connecting blocks; 3. a mounting cavity; 4. a top cover; 5. mounting a plate; 6. a release assembly; 601. a gear; 602. a rack; 603. a wedge surface; 604. releasing the shaft; 605. a release button; 7. a connecting cavity; 8. a connecting assembly; 801. a connecting shaft; 802. a connecting button; 803. a connecting rod; 804. a connecting disc; 805. a second spring; 9. a movable cavity; 10. a drive assembly; 1001. a third spring; 1002. a drive block; 11. and a first spring.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Example 1

Referring to fig. 1-3, the present invention provides a technical solution: the utility model provides an equipment fixing frame for unmanned aerial vehicle, including mount pad 1, the bilateral symmetry of mount pad 1 is provided with a set of connecting block 2, a set of installation cavity 3 has been seted up to the top symmetry of mount pad 1, connect through top cap 4 between two installation cavities 3, the bottom of top cap 4 just is located the installation cavity and is provided with mounting panel 5, one 11 and installation cavity 3 are connected through spring to the bottom of mounting panel 5, the one side that just is located mounting panel 5 in the installation cavity 3 is provided with and top cap 4 matched with release assembly 6, connection chamber 7 has been seted up to the intermediate position of connecting block 2, be provided with coupling assembling 8 in the connection chamber 7, a set of movable chamber 9 has been seted up to the bilateral symmetry of top cap 4, be provided with in the movable chamber 9 with release assembly 6 matched with drive assembly 10.

In this embodiment: the utility model has the advantages that: cooperate through setting up devices such as release assembly 6, coupling assembling 8 and drive assembly 10 to in concrete use, under the prerequisite of not using tools, just can dismantle and install mount pad 1 and top cap 4, and then when needs are changed the motor or when the motor breaks down out of work, can be quick dismantle between mount pad 1 and the unmanned aerial vehicle, and then convenient to use.

In an alternative embodiment, the releasing assembly 6 includes a gear 601 disposed in the mounting cavity 3, a rack 602 is disposed on one side of the gear 601, a wedge surface 603 engaged with the driving assembly 10 is disposed at a top end of the rack 602, the releasing assembly 6 is inserted into a releasing shaft 604 disposed at a middle position of the gear 601, and an end of the releasing shaft 604 far away from the gear 601 extends to an outer side of the mounting seat 1 to be connected with a releasing button 605.

In this embodiment: through setting up release assembly 6 to in specific use, can dismantle and install top cap 4 under the condition of not using tools, and then the staff's of being convenient for use, simultaneously, also can save a large amount of time, improve work efficiency.

In an alternative embodiment, the connecting assembly 8 includes a connecting shaft 801 disposed in the connecting cavity 7, one end of the connecting shaft 801 extending to the connecting block 2 is connected to the connecting button 802, one end of the connecting shaft 801 far away from the connecting button 802 is provided with a connecting rod 803, the connecting assembly 8 further includes a connecting disc 804 disposed on the connecting shaft 801 and located between the connecting rod 803 and the connecting button 802, and a second spring 805 is disposed on the connecting shaft 801 and located on one side of the connecting disc 804 close to the connecting rod 803.

In this embodiment: through setting up coupling assembling 8 to in specific use, can be under the condition of not using tools, install and dismantle between quick mount pad 1 and the unmanned aerial vehicle, and then the staff's of being convenient for use.

In an alternative embodiment, the driving assembly 10 includes a spring tri 1001 disposed in the movable chamber 9, and an end of the spring tri 1001 away from the inner cavity of the movable chamber 9 is provided with a driving block 1002 engaged with the wedge 603.

In this embodiment: through setting up drive assembly 10 to in specific use, can install top cap 4 through pressing down top cap 4, and then be convenient for staff's use.

The utility model discloses a theory of operation and use flow: after the motor is installed in the inner cavity of the installation seat 1, the top cover 4 is pressed downwards, the driving block 1002 is matched with the installation cavity 3 under the action of the spring three 1001, the installation of the top cover 4 is further completed, the installation seat 1 is placed in the area where the motor is installed on the unmanned aerial vehicle, a cavity matched with the connecting assembly 8 is formed in the unmanned aerial vehicle (the bottom of the cavity is cuboid-shaped, the top of the cavity is cylindrical, the diameter of the inner cavity of the cylindrical shape is the same as the width of the inner cavity of the cuboid-shaped cavity), the top end of the inner cavity of the connection cavity 7 is connected with the cavity formed in the unmanned aerial vehicle, the connection button 802 is pushed towards the unmanned aerial vehicle, the connection rod 803 enters the cylinder through the inner cavity of the cuboid-shaped cavity in the unmanned aerial vehicle, the connection button 802 is rotated towards the right side and released, and the installation of the installation seat 1 is further completed; when the mount pad 1 needs to be disassembled, the connecting button 802 is rotated by ninety degrees in any direction, under the action of the second spring 805, the connecting rod 803 and the unmanned aerial vehicle are released, after the mount pad 1 is disassembled, the releasing button 605 is rotated, the releasing button 605 drives the releasing shaft 604 and the gear 601 to rotate, the gear 601 is meshed with the rack 602, the rack 602 moves upwards to be matched with the driving block 1002, the driving block 1002 moves towards the movable cavity 9 under the action of the third spring 1001, after the driving block 1002 moves out of the mount cavity 3, under the action of the first mounting plate 5 and the first spring 11, the top cover 4 pops out of the mount cavity 3, and then the separation between the top cover 4 and the mount pad 1 is completed.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. An equipment mounting bracket for unmanned aerial vehicle, includes mount pad (1), its characterized in that: a group of connecting blocks (2) are symmetrically arranged on two sides of the mounting seat (1), a group of mounting cavities (3) are symmetrically arranged at the top end of the mounting seat (1), the two mounting cavities (3) are connected through a top cover (4), a mounting plate (5) is arranged at the bottom end of the top cover (4) and in the mounting cavity (3), the bottom end of the mounting plate (5) is connected with the mounting cavity (3) through a first spring (11), a release component (6) matched with the top cover (4) is arranged in the mounting cavity (3) and on one side of the mounting plate (5), a connecting cavity (7) is arranged in the middle of the connecting block (2), a connecting component (8) is arranged in the connecting cavity (7), a group of movable cavities (9) are symmetrically formed in two sides of the top cover (4), and driving components (10) matched with the release components (6) are arranged in the movable cavities (9).

2. The equipment mounting bracket for unmanned aerial vehicle of claim 1, wherein: the release assembly (6) comprises a gear (601) arranged in the installation cavity (3), a rack (602) is arranged on one side of the gear (601), and a wedge surface (603) matched with the driving assembly (10) is arranged at the top end of the rack (602).

3. The equipment mounting bracket for unmanned aerial vehicle of claim 2, wherein: the releasing component (6) is inserted into a releasing shaft (604) arranged in the middle of the gear (601), and one end, far away from the gear (601), of the releasing shaft (604) extends to the outer side of the mounting base (1) to be connected with a releasing button (605).

4. The equipment mounting bracket for unmanned aerial vehicle of claim 1, wherein: coupling assembling (8) are including setting up connecting axle (801) in connecting chamber (7), the bottom of connecting axle (801) extends to the one end and the connection button (802) of connecting block (2) are connected, connecting axle (801) are kept away from the one end of connecting button (802) is provided with connecting rod (803).

5. The equipment mounting rack for unmanned aerial vehicle of claim 4, wherein: the connecting assembly (8) further comprises a connecting disc (804) which is arranged on the connecting shaft (801) and located between the connecting rod (803) and the connecting button (802), and a second spring (805) is arranged on one side, close to the connecting rod (803), of the connecting disc (804) on the connecting shaft (801).

6. The equipment mounting bracket for unmanned aerial vehicle of claim 2, wherein: the driving assembly (10) comprises a spring III (1001) arranged in the movable cavity (9), and a driving block (1002) matched with the wedge surface (603) is arranged at one end, far away from the inner cavity of the movable cavity (9), of the spring III (1001).