CN219154747U

CN219154747U - Hanging bracket for airplane

Info

Publication number: CN219154747U
Application number: CN202223505031.1U
Authority: CN
Inventors: 余涛
Original assignee: Weizhen Aviation Technology Haifeng Co ltd
Current assignee: Weizhen Aviation Technology Haifeng Co ltd
Priority date: 2022-12-27
Filing date: 2022-12-27
Publication date: 2023-06-09
Anticipated expiration: 2032-12-27

Abstract

The utility model relates to the technical field of suspension brackets, in particular to an aircraft suspension bracket. The front support is fixedly arranged at the top of the first support, the rear support is fixedly arranged on the second support, a third support is arranged between the first support and the second support, a plurality of sleeve frames are fixedly arranged between the first support and the third support, adjusting frames are movably inserted in the sleeve frames, one ends of the adjusting frames penetrate through one ends of the sleeve frames and one side of the third support fixedly connected with the second support, two adjacent adjusting frames are connected through a folding assembly, the occurrence of leakage can be reduced by the folding assembly, articles are prevented from falling, limiting assemblies which are clamped with the two adjusting frames are arranged on two sides of the third support, the adjusting frames can be stably limited, and the limiting assemblies are prevented from falling out of the third support; the utility model provides an aircraft suspension bracket which can reduce the occurrence of larger leakage when adjusting the bracket, can stably limit the adjusting bracket and prevent a limiting component from falling off.

Description

Hanging bracket for airplane

Technical Field

The utility model relates to the technical field of suspension brackets, in particular to an aircraft suspension bracket.

Background

At present, the hanging species of an airplane are various, and different hanging objects have large supporting distance difference, so that the supporting requirements of different hanging objects in disassembly and assembly are met, and the airplane is divided into a fixed bracket and a telescopic bracket.

Common telescopic bracket is great in the middle of the leak when carrying out the flexible, and very likely article drops from the leak when placing article, and simultaneously when the position of spacing alignment jig, not stable enough leads to spacing subassembly still more easily coming off to can not spacing alignment jig's position effectively, therefore has proposed an aircraft and has used the thing bracket of hanging.

Disclosure of Invention

The utility model aims to solve the technical problem of providing the aircraft suspension bracket which can reduce the generation of larger leakage when adjusting the bracket, stably limit the adjusting bracket and prevent the limiting component from falling off.

The technical scheme adopted by the utility model is as follows: the utility model provides an aircraft is with suspension bracket, includes support one, support two, preceding support, back support, its characterized in that: the front support is fixedly arranged at the top of the first support, the rear support is fixedly arranged on the second support, a third support is arranged between the first support and the second support, a plurality of sleeve frames are fixedly arranged between the first support and the third support, adjusting frames are movably inserted in the sleeve frames, one ends of the adjusting frames penetrate through one ends of the sleeve frames and one side of the third support fixedly connected with the second support, two adjacent adjusting frames are connected through a folding assembly, the occurrence of leakage can be reduced by the folding assembly, articles are prevented from falling, limiting assemblies which are clamped with the two adjusting frames are arranged on two sides of the third support, the adjusting frames can be stably limited, and the limiting assemblies are prevented from falling out of the third support;

the folding assembly comprises a plurality of diamond frames which are connected in a rotating way, one end of one diamond frame close to the third bracket is fixedly connected with the third bracket through a connecting clamp I, one end of the other diamond frame close to the second bracket is fixedly connected with the second bracket through a connecting clamp II, one end of the diamond frame close to the adjusting bracket is connected with a sliding block through a spring I, and the sliding block is connected with the adjusting bracket in a sliding way;

the limiting component comprises a penetrating rod which penetrates through the third support, one end of the penetrating rod is clamped in the adjusting frame, clamping blocks which are clamped in the adjusting frame are fixedly arranged on two sides of the adjusting frame, a handle is fixedly arranged on the other end of the penetrating rod, and a second spring and a sleeve plate are sleeved on the penetrating rod.

As a further scheme of the utility model: a plurality of hack levers are fixedly arranged between two adjacent sleeve frames.

As a further scheme of the utility model: one end of the sleeve frame is provided with a through hole for the adjusting frame to penetrate through, and the third bracket is provided with a through hole for the adjusting frame to penetrate through.

As a further scheme of the utility model: one end of the diamond-shaped frame is rotationally connected with the first connecting clamp, and the other end of the diamond-shaped frame is rotationally connected with the second connecting clamp.

As a further scheme of the utility model: the adjusting frame is provided with a chute for sliding connection of the sliding block.

As a further scheme of the utility model: the adjusting frame is provided with a plurality of penetrating grooves for penetrating and clamping the penetrating rod and the clamping block.

As a further scheme of the utility model: one end of the second spring is fixedly connected with the inner side of the third support, the other end of the second spring is fixedly connected with a sleeve plate, and the sleeve plate is movably attached to the adjusting frame.

Compared with the prior art, the utility model has the beneficial effects that:

according to the utility model, through the arrangement of the folding assembly, the occurrence of leakage can be reduced, and the articles are prevented from falling off, so that the articles with different sizes can be placed in an increased manner.

According to the utility model, the adjusting frame can be stably limited by the limiting component, and the limiting component is prevented from falling out of the third bracket.

Drawings

The accompanying drawings are included to provide a further understanding of the utility model and are incorporated in and constitute a part of this specification, illustrate the utility model and together with the embodiments of the utility model, serve to explain the utility model. In the drawings:

fig. 1 is a schematic view showing the overall structure of a hanger bracket for an aircraft according to the present utility model.

Fig. 2 is a schematic view of a portion a of an aircraft suspension bracket according to the present utility model.

Fig. 3 is a schematic view of a B-section structure of an aircraft suspension bracket according to the present utility model.

In the accompanying drawings:

1. a first bracket; 2. a second bracket; 3. a front support; 4. a rear bracket; 5. a third bracket; 6. a sleeve frame; 7. an adjusting frame; 8. a folding assembly; 9. a limit component; 8.1, a diamond frame; 8.2, a first spring; 8.3, sliding blocks; 9.1, threading a rod; 9.2, clamping blocks; 9.3, a handle; 9.4, a second spring; 9.5, sleeve plate.

Detailed Description

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

Referring to fig. 1-3, the present utility model provides a technical solution: the utility model provides an aircraft is with suspension bracket, includes support 1, support 2, preceding support 3, back support 4, its characterized in that: the front support 3 is fixedly arranged at the top of the first support 1, the rear support 4 is fixedly arranged on the second support 2, a third support 5 is arranged between the first support 1 and the second support 2, a plurality of sleeve frames 6 are fixedly arranged between the first support 1 and the third support 5, a plurality of frame rods 6.1 are fixedly arranged between two adjacent sleeve frames 6, an adjusting frame 7 is movably inserted into the sleeve frames 6, one end of the adjusting frame 7 penetrates through one end of the sleeve frame 6 and one side of the third support 5 to be fixedly connected with the second support 2, one end of the sleeve frame 6 is provided with a through hole for the adjusting frame 7 to penetrate through, the third support 5 is provided with a movable through hole for the adjusting frame 7 to penetrate through, the two adjacent adjusting frames 7 are connected through a folding assembly 8, the folding assembly 8 can reduce leakage, the article is prevented from falling, limiting assemblies 9 which are clamped with the two adjusting frames 7 are arranged at two sides of the third support 5, the adjusting frames 7 can be stably limited, and the limiting assemblies 9 are prevented from falling out of the third support 5; when the hanger bracket needs to be adjusted, the limiting component 9 is pulled in a rotating mode, so that the limiting component 9 is separated from the adjusting frame 7, then the adjusting frame 7 can be adjusted in a sliding mode, the folding component 8 can be changed at the moment, leakage is prevented from being enlarged, when the hanger bracket is adjusted to a proper position, the limiting component 9 can be loosened in a rotating mode, and the position of the limiting adjusting frame 7 is fixed through the limiting component 9.

The folding assembly 8 comprises a plurality of rhombus frames 8.1 which are connected with each other in a rotating way, one end of one rhombus frame 8.1 close to the third bracket 5 is fixedly connected with the third bracket 5 through a first connecting clamp, one end of the other rhombus frame 8.1 close to the second bracket 2 is fixedly connected with the second bracket 2 through a second connecting clamp, one end of one rhombus frame 8.1 is connected with the first connecting clamp in a rotating way, one end of the other rhombus frame 8.1 is connected with the second connecting clamp in a rotating way, one end of the rhombus frame 8.1 close to the adjusting frame 7 is connected with a sliding block 8.3 through a first spring 8.2, the sliding block 8.3 is connected with the adjusting frame 7 in a sliding way, and a sliding groove for the sliding connection of the sliding block 8.3 is arranged on the adjusting frame 7; when the second bracket 2 moves, the diamond-shaped frame 8.1 can be pulled, so that the folding angle of the diamond-shaped frame 8.1 is changed, the first spring 8.2 is deformed, and the sliding block 8.3 also slides on the adjusting frames 7, so that gaps between two adjacent adjusting frames 7 are reduced.

Limiting component 9 is including running through the pole 9.1 that wears to set up on the third 5 of support, wear the one end joint of pole 9.1 in alignment jig 7, the fixture block 9.2 of joint in alignment jig 7 is all fixed to the both sides of alignment jig 7, be equipped with the wearing groove that a plurality of confession worn pole 9.1 and fixture block 9.2 run through the joint on the alignment jig 7, wear the other end of pole 9.1 and fixedly be equipped with handle 9.3, wear the pole 9.1 on the cover be equipped with spring two 9.4 and bushing 9.5, the one end fixed connection third 5 inboard of spring two 9.4, the other end fixed connection bushing 9.5 of spring two 9.4, bushing 9.5 movable paste even alignment jig 7. When the position of the adjusting frame 7 needs to be controlled through the limiting component 9, the handle 9.3 can be rotated, the threading rod 9.1 is driven to rotate, the clamping block 9.2 is enabled to rotate, then the threading rod 9.1 can be pulled outwards, the threading rod 9.1 and the clamping block 9.2 are enabled to move out of the threading groove, the sleeve plate 9.5 is pushed, the springs II 9.4 are extruded, at the moment, the position of the adjusting frame 7 can be adjusted in a sliding mode, when the adjusting frame is adjusted to a proper position, the handle 9.3 can be rotated, the clamping block 9.2 is driven to rotate, then the handle 9.3 is loosened, the sleeve plate 9.5 can be pushed through the elastic force of the springs II 9.4, the clamping block 9.2 and the threading rod 9.1 are spliced in the threading groove, then the handle 9.3 is rotated, the clamping block 9.2 is driven to rotate, and the clamping block 9.2 is enabled to be clamped with the threading groove.

The working principle of the utility model is as follows:

when the hanger bracket needs to be adjusted, the handle 9.3 can be rotated firstly, so that the penetrating rod 9.1 is driven to rotate, the clamping blocks 9.2 are also rotated, then the penetrating rod 9.1 can be pulled outwards, the penetrating rod 9.1 and the clamping blocks 9.2 are moved out of the penetrating grooves, the sleeve plate 9.5 is pushed, the springs II 9.4 are extruded, at the moment, the positions of the adjusting frames 7 can be adjusted in a sliding mode, the diamond frames 8.1 on the folding assembly 8 are pulled, the folding angle of the diamond frames 8.1 is changed, meanwhile, the springs I8.2 are deformed, meanwhile, the sliding blocks also 8.3 slide on the adjusting frames 7, so that gaps between the two adjacent adjusting frames 7 are reduced, leakage gaps are prevented from becoming large, when the hanger bracket is adjusted to a proper position, the handles 9.3 can be rotated, so that the clamping blocks 9.2 are driven to rotate, then the elastic force of the handles 9.3 can be released, the sleeve plate 9.5 is pushed, the clamping blocks 9.2 and the penetrating rods 9.1 are spliced in the penetrating grooves, and then the handles 9.3 are rotated, so that the clamping blocks 9.2 are driven to rotate, and the clamping blocks are driven to rotate, so that the clamping blocks 9.2 are connected with the clamping blocks.

The utility model and its embodiments have been described above with no limitation, and the actual construction is not limited to the embodiments of the utility model as shown in the drawings. In summary, if one of ordinary skill in the art is informed by this disclosure, a structural manner and an embodiment similar to the technical solution should not be creatively devised without departing from the gist of the present utility model.

Claims

1. The utility model provides an aircraft is with suspension bracket, includes support one (1), support two (2), preceding support (3), back support (4), its characterized in that: the front support bracket (3) is fixedly arranged at the top of the first support bracket (1), the rear support bracket (4) is fixedly arranged on the second support bracket (2), a third support bracket (5) is arranged between the first support bracket (1) and the second support bracket (2), a plurality of sleeve brackets (6) are fixedly arranged between the first support bracket (1) and the third support bracket (5), an adjusting bracket (7) is movably inserted in the sleeve brackets (6), one end of the adjusting bracket (7) penetrates through one end of the sleeve brackets (6) and one side of the third support bracket (5) to be fixedly connected with the second support bracket (2), two adjacent adjusting brackets (7) are connected through a folding assembly (8), and limiting assemblies (9) for clamping two adjusting brackets (7) are arranged on two sides of the third support bracket (5);

the folding assembly (8) comprises a plurality of diamond frames (8.1) which are connected in a rotating way, one end of one diamond frame (8.1) close to the third bracket (5) is fixedly connected with the third bracket (5) through a connecting clamp I, one end of the other diamond frame (8.1) close to the second bracket (2) is fixedly connected with the second bracket (2) through a connecting clamp II, one end of the diamond frame (8.1) close to the first adjusting bracket (7) is connected with a sliding block (8.3) through a spring I (8.2), and the sliding block (8.3) is connected with the adjusting bracket (7) in a sliding way;

limiting component (9) are including running through pole (9.1) of wearing that sets up on support three (5), the one end joint of pole (9.1) is worn in alignment jig (7), fixture block (9.2) of joint in alignment jig (7) are all fixed to both sides of alignment jig (7), the other end of pole (9.1) is fixed and is equipped with handle (9.3), the cover is equipped with spring two (9.4) and bushing (9.5) on pole (9.1).

2. An aircraft suspension bracket according to claim 1, wherein: a plurality of hack levers (6.1) are fixedly arranged between two adjacent sleeve frames (6).

3. An aircraft suspension bracket according to claim 1, wherein: one end of the sleeve frame (6) is provided with a perforation for the penetration and movement of the adjusting frame (7), and the third bracket (5) is provided with a through hole for the penetration and movement of the adjusting frame (7).

4. An aircraft suspension bracket according to claim 1, wherein: one end of one diamond-shaped frame (8.1) is rotationally connected with the first connecting clamp, and one end of the other diamond-shaped frame (8.1) is rotationally connected with the second connecting clamp.

5. An aircraft suspension bracket according to claim 1, wherein: the adjusting frame (7) is provided with a chute for sliding connection of the sliding block (8.3).

6. An aircraft suspension bracket according to claim 1, wherein: the adjusting frame (7) is provided with a plurality of penetrating grooves for penetrating and clamping the penetrating rod (9.1) and the clamping block (9.2).

7. An aircraft suspension bracket according to claim 1, wherein: one end of the second spring (9.4) is fixedly connected with the inner side of the third support (5), the other end of the second spring (9.4) is fixedly connected with the sleeve plate (9.5), and the sleeve plate (9.5) is movably attached to the adjusting frame (7).