CN213262943U

CN213262943U - Unmanned aerial vehicle integrated equipment mounting bracket

Info

Publication number: CN213262943U
Application number: CN202022074835.5U
Authority: CN
Inventors: 徐庆华; 贺集乐; 孟令赛; 许灯顺; 禹志刚
Original assignee: Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
Current assignee: Shenyang Aircraft Design and Research Institute Aviation Industry of China AVIC
Priority date: 2020-09-21
Filing date: 2020-09-21
Publication date: 2021-05-25
Anticipated expiration: 2030-09-21

Abstract

This application belongs to mounting bracket technical field, in particular to unmanned aerial vehicle integration equipment mounting bracket. The method comprises the following steps: the first support, second support and third support. The cross section of the first support is L-shaped, a plurality of first supports are arranged along the vertical direction respectively, and two ends of each first support are connected with the frame beam of the machine body structure respectively; the cross section of the second support is U-shaped, two second supports arranged in parallel form a group, a plurality of groups are arranged along the horizontal direction respectively, two ends of each second support are connected with the first support or the frame beam of the machine body structure respectively, the middle part of each second support is connected with the first support, and the outer side of a web plate of each second support is provided with an installation lug; the cross section of each third support is T-shaped, the three third supports form an H-shaped equipment frame, the H-shaped equipment frame comprises a plurality of third supports, and two ends of each third support are respectively connected with the two second supports in the same group. This application can guarantee that equipment fixing fastening is reliable, and the guarantee is maintained to the convenience, effectively reduces weight and cost, and simple structure has commonality and integrativeness to most finished product equipment simultaneously.

Description

Unmanned aerial vehicle integrated equipment mounting bracket

Technical Field

This application belongs to mounting bracket technical field, in particular to unmanned aerial vehicle integration equipment mounting bracket.

Background

Unmanned aerial vehicle integrated equipment mounting bracket's main effect: firstly, equipment is ensured to be installed and fastened reliably; secondly, the maintenance is convenient; thirdly, the weight and the cost are reduced.

The existing aircraft finished product installation in China mostly adopts the finished product to be connected, installed and fixed with the installation frame built by the equipment installation frame and the aircraft structure, lacks the comprehensive design from the angle of the whole aircraft, and is not enough in the aspects of weight, safety, maintenance, cost and the like.

Accordingly, a technical solution is desired to overcome or at least alleviate at least one of the above-mentioned drawbacks of the prior art.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing an unmanned aerial vehicle integration equipment mounting bracket to solve at least one problem that prior art exists.

The technical scheme of the application is as follows:

an unmanned aerial vehicle integration equipment mounting bracket, comprising:

the cross section of the first support is L-shaped, the first support comprises a plurality of supports which are arranged along the vertical direction respectively, and two ends of the first support are connected with the frame beam of the machine body structure respectively;

the cross section of the second support is U-shaped, the two second supports arranged in parallel form a group, the second supports comprise a plurality of groups and are respectively arranged along the horizontal direction, two ends of each second support are respectively connected with the first support or the machine body structure frame beam, the middle part of each second support is connected with the first support, and the outer side of a web plate of each second support is provided with an installation lug;

the cross section of each third support is T-shaped, the number of the third supports is three, the third supports form an H-shaped equipment frame, the H-shaped equipment frame comprises a plurality of third supports, and two ends of the H-shaped equipment frame are connected with the second supports in the same group respectively.

Optionally, the second support is arranged in two layers along the up-down direction of the first support.

Optionally, the first bracket and the second bracket are both provided with ribs.

Optionally, two of the mounting lugs are symmetrically arranged on the second bracket corresponding to each of the H-shaped device frames.

Optionally, the H-shaped equipment frame comprises two first frame units arranged in parallel and a second frame unit perpendicular to the first frame units, and the second frame unit is provided with a tapered pin.

Optionally, two tapered pins are symmetrically arranged on the second frame unit.

Optionally, the method further comprises:

the chassis is arranged on the H-shaped equipment frame, and a tapered hole matched with the tapered pin is formed in the rear end face of the chassis;

a front locking assembly, the front locking assembly comprising: an L-shaped latch hook, a pin shaft and a front locking mechanism, wherein,

the L-shaped lock hook is arranged on the front end surface of the case;

the pin shaft is arranged in the mounting lug plate;

the front locking mechanism is matched with the L-shaped locking hook and the pin shaft to fasten the case.

Optionally, each chassis is configured with two sets of the front locking assemblies.

Optionally, a fuse is mounted on the pin.

Utility model has the following beneficial technical effects:

the utility model provides an unmanned aerial vehicle integration equipment mounting bracket can guarantee that the equipment fixing fastening is reliable, and the guarantee is maintained to the convenience, effectively reduces weight and cost, and simple structure has commonality and integration to most finished product equipment simultaneously.

Drawings

Fig. 1 is a schematic view of an integrated equipment mount for a drone according to an embodiment of the present application;

fig. 2 is a schematic illustration of a taper pin mounting of a drone integrated device mount of one embodiment of the present application;

fig. 3 is an equipment installation schematic diagram of the integrated equipment mounting rack of the unmanned aerial vehicle according to an embodiment of the present application.

Wherein:

1-a first scaffold; 2-a second scaffold; 21-mounting a tab; 3-a third scaffold; 31-a tapered dowel; 4-a case; 5-L-shaped latch hook; 6-a pin shaft; 7-front locking mechanism.

Detailed Description

In order to make the implementation objects, technical solutions and advantages of the present application clearer, the technical solutions in the embodiments of the present application will be described in more detail below with reference to the drawings in the embodiments of the present application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are a subset of the embodiments in the present application and not all embodiments in the present application. The embodiments described below with reference to the drawings are exemplary and intended to be used for explaining the present application and should not be construed as limiting the present application. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present application. Embodiments of the present application will be described in detail below with reference to the accompanying drawings.

In the description of the present application, it is to be understood that the terms "center", "longitudinal", "lateral", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are used merely for convenience in describing the present application and for simplifying the description, and do not indicate or imply that the referenced device or element must have a particular orientation, be constructed in a particular orientation, and be operated, and therefore should not be construed as limiting the scope of the present application.

The present application is described in further detail below with reference to fig. 1 to 3.

The application provides an unmanned aerial vehicle integrated equipment mounting bracket, include: a first bracket 1, a second bracket 2 and a third bracket 3.

Specifically, as shown in fig. 1, the cross section of the first support 1 is L-shaped, the first support 1 includes a plurality of supports, the supports are respectively arranged along the vertical direction, and two ends of the first support 1 are respectively connected with the frame beam of the machine body structure in a detachable manner; the cross section of the second bracket 2 is U-shaped, two second brackets 2 arranged in parallel form a group, the second brackets 2 are provided with a plurality of groups and are respectively arranged along the horizontal direction, two ends of the second brackets 2 are respectively welded or bolted with the first bracket 1 or detachably connected with a frame beam of the machine body structure, the middle part of the second bracket 2 is connected with the first bracket 1 in a welding or bolting mode, and the outer side of a web plate of the second bracket 2 is provided with an installation lug 21; the cross section of the third support 3 is T-shaped, three third supports 3 form an H-shaped equipment frame, the H-shaped equipment frame comprises a plurality of the third supports, and two ends of the H-shaped equipment frame are respectively connected with the two second supports 2 in the same group in a welding or bolt connection mode. Form holistic frame beam structure through first support 1, second support 2 and third support 3 in this application, as unmanned aerial vehicle integrated equipment's mounting bracket.

The utility model provides an unmanned aerial vehicle integration equipment mounting bracket, second support 2 can follow the upper and lower direction of first support 1 and arrange the multilayer. In this embodiment, two layers are preferably arranged, each layer is provided with a plurality of groups of second brackets 2, and two second brackets 2 in each group are arranged on the corresponding first brackets 1 in parallel along the same horizontal direction.

In one embodiment of the present application, the ribs are provided on both the first bracket 1 and the second bracket 2, which can improve the overall stability of the mounting bracket.

In one embodiment of the present application, two mounting tabs 21 are symmetrically disposed on the second bracket 2 corresponding to each H-shaped equipment frame for installation of equipment.

In one embodiment of the application, the H-shaped equipment frame comprises two first frame units arranged in parallel and a second frame unit perpendicular to the first frame units, the length of the second frame unit can be set according to the equipment to be installed, and H-shaped equipment frames with multiple specifications are configured to meet installation requirements of multiple kinds of equipment. Advantageously, as shown in fig. 2, a tapered pin 31 is provided on the second frame unit for cooperating with a tapered hole provided on the apparatus to effect mounting and positioning of the apparatus. In this embodiment, two tapered pins 31 are symmetrically arranged on the second frame unit of each H-shaped equipment frame.

As shown in fig. 3, the integrated equipment mounting bracket of unmanned aerial vehicle of this application still includes: case 4 and preceding locking Assembly, wherein, case 4 sets up on H type equipment frame, all has two symmetrical installation positions on every H type equipment frame, and 4 laps of case are in the installation position, offer the bell mouth that matches with toper pin 31 on the rear end face of case 4, realize 4 rear end of case location. In this embodiment, the case 4 may be a square device such as a flying pipe computer and a power supply box. The front locking assembly includes: the locking mechanism comprises an L-shaped locking hook 5, a pin shaft 6 and a front locking mechanism 7, wherein the L-shaped locking hook 5 is arranged on the front end face of the case 4, and the L-shaped locking hook 5 can be installed through bolts; the pin 6 is arranged in the mounting lug 21, and a fuse is preferably mounted on the pin 6. The front locking mechanism 7 is matched with the L-shaped locking hook 5 and the pin 6 to fasten the front end of the case 4. In this embodiment, each chassis 4 is installed by matching two mounting tabs 21 with two sets of front locking assemblies.

According to the unmanned aerial vehicle integrated equipment mounting frame, the integral mounting frame is built through the L-shaped first support 1, the U-shaped second support 2 and the T-shaped third support 3, and loads are transmitted; the rear end of the equipment is fixed through the tapered pin 31 and the tapered hole on the rear end face of the equipment, and the front end of the equipment is fixed through the L-shaped lock hook 5, the pin shaft 6 and the front locking mechanism 7, so that the installation of the fastening equipment is finally achieved. This application is through locking mechanism 7 before opening, makes preceding locking mechanism 7 and latch hook 6 separation, can directly take equipment out convenient and fast. The mounting lugs 21 connected to the front locking mechanism 7 are arranged directly on the second bracket 2, saving the cross members of the mounting bracket.

The utility model provides an unmanned aerial vehicle integration equipment mounting bracket can guarantee that the equipment fixing fastening is reliable, and the guarantee is maintained to the convenience, effectively reduces weight and cost. The device is simple in structure and has universality and integration for most finished equipment.

The above description is only for the specific embodiments of the present application, but the scope of the present application is not limited thereto, and any changes or substitutions that can be easily conceived by those skilled in the art within the technical scope of the present application should be covered within the scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.

Claims

1. An unmanned aerial vehicle integration equipment mounting bracket, its characterized in that includes:

the cross section of the first support (1) is L-shaped, the first support (1) comprises a plurality of supports which are arranged along the vertical direction respectively, and two ends of the first support (1) are connected with the frame beam of the machine body structure respectively;

the cross section of the second support (2) is U-shaped, the two second supports (2) which are arranged in parallel form a group, the second supports (2) comprise a plurality of groups which are respectively arranged along the horizontal direction, two ends of each second support (2) are respectively connected with the first support (1) or the frame beam of the machine body structure, the middle part of each second support is connected with the first support (1), and the outer side of a web plate of each second support (2) is provided with an installation lug (21);

and the cross section of each third support (3) is T-shaped, the number of the third supports (3) is three, each H-shaped equipment frame comprises a plurality of H-shaped equipment frames, and two ends of each H-shaped equipment frame are respectively connected with the two second supports (2) in the same group.

2. The unmanned aerial vehicle integration equipment mounting bracket of claim 1, wherein the second support (2) is arranged in two layers along the up-down direction of the first support (1).

3. The unmanned aerial vehicle integration equipment mounting bracket of claim 1, wherein the first bracket (1) and the second bracket (2) are each provided with a rib.

4. The unmanned aerial vehicle integrated equipment mounting bracket of claim 1, wherein two mounting lugs (21) are symmetrically arranged on the second bracket (2) corresponding to each H-shaped equipment frame.

5. The unmanned aerial vehicle integrated equipment mounting frame of claim 1, wherein the H-shaped equipment frame comprises two first frame units arranged in parallel and a second frame unit perpendicular to the first frame units, and tapered pins (31) are arranged on the second frame unit.

6. The UAV integration equipment mount of claim 5, wherein the second frame unit is symmetrically provided with two tapered pins (31).

7. The unmanned aerial vehicle integrated equipment mount of claim 5, further comprising:

the chassis (4) is arranged on the H-shaped equipment frame, and a tapered hole matched with the tapered pin (31) is formed in the rear end face of the chassis (4);

a front locking assembly, the front locking assembly comprising: an L-shaped latch hook (5), a pin shaft (6) and a front locking mechanism (7), wherein,

the L-shaped lock hook (5) is arranged on the front end face of the case (4);

the pin shaft (6) is arranged in the mounting lug (21);

the front locking mechanism (7) is matched with the L-shaped locking hook (5) and the pin shaft (6) to fasten the case (4).

8. The unmanned aerial vehicle integrated equipment mount of claim 7, wherein each of the chassis (4) is configured with two sets of the front locking assemblies.

9. The unmanned aerial vehicle integration equipment mounting bracket of claim 7, wherein the pin (6) is provided with a fuse.