CN209912664U

CN209912664U - Assembled general transformer mounting bracket for aircraft

Info

Publication number: CN209912664U
Application number: CN201920878005.2U
Authority: CN
Inventors: 李宁康; 梁飞; 曾辉; 刘韬; 熊超林; 韩晋平; 李峰
Original assignee: Jiangxi Crown General Aviation Co Ltd
Current assignee: Jiangxi Crown General Aviation Co Ltd
Priority date: 2019-06-12
Filing date: 2019-06-12
Publication date: 2020-01-07
Anticipated expiration: 2029-06-12

Abstract

The utility model discloses an assembled general transformer mounting bracket for aircraft, which is formed by assembling a base, a sliding plate, a stabilizing plate and a transformer main body, shortens the assembling and disassembling time of the mounting bracket, improves the working efficiency, and once an element is damaged, only the damaged element needs to be replaced, and other elements are kept to be continuously used; the stabilizing plate and the spring form an element for assembling the transformer mounting frame, the fixing base and the transformer main body, and when the transformer main body works and vibrates, the stabilizing plate plays a role in damping, and influences on the transformer are reduced. The utility model discloses simple structure, the equipment is quick, and it is convenient to change, can extensively promote and utilize.

Description

Assembled general transformer mounting bracket for aircraft

[ technical field ] A method for producing a semiconductor device

The utility model relates to a technical field of transformer mounting bracket, especially the technical field of transformer mounting bracket for the general aircraft of assembled.

[ background of the invention ]

The transformer is a device for changing alternating voltage, most of transformers for the general airplane are fixed in the airplane, and if the transformers break down, the transformers are extremely inconvenient to disassemble during maintenance; the transformer can vibrate during working, and the service life of the device can be influenced when the transformer is used for a long time under a fixed structure; in order to solve the problems, an assembled general-purpose aircraft transformer mounting frame with a damping function is needed to be designed, so that the transformer is convenient to mount and dismount, and the service life of the device is prolonged.

[ Utility model ] content

The utility model aims at solving the problem among the prior art, provide a transformer mounting bracket for assembled general aircraft, can make the installation convenient with the dismantlement, reduce the influence of transformer vibrations, increase of service life.

In order to achieve the purpose, the utility model provides a transformer mounting bracket for assembled general aircraft, including base, sliding plate, steadying plate and transformer main part, transformer main part both sides respectively are provided with a support and two spouts, the support surface is provided with two bolts, the bolt top is provided with the nut.

Preferably, the number of the sliding plates is two, the sliding plates are provided with a first screw hole, a second screw hole, a first sliding block and a second sliding block, the first screw hole and the second screw hole are matched with the bolt, and the first sliding block and the second sliding block are matched with the sliding groove.

Preferably, the base surface is provided with a first fixing groove and a second fixing groove.

Preferably, the number of the stabilizing plates is two, six springs are arranged on the surfaces of the stabilizing plates, the stabilizing plates are matched with the transformer main body, and the stabilizing plates are matched with the base.

The utility model has the advantages that: the utility model discloses a set up transformer mounting bracket into a plurality of amalgamation structures, realized easy to assemble and dismantle, improved the convenience when maintaining and changing greatly, improved the efficiency of work; the springs are arranged on the surfaces of the stabilizing plates, when the transformer works and shakes, the springs on the two sides buffer the transformer to a certain extent, so that the effect of shock absorption is achieved, the damage to the mounting frame is reduced, and the service life is prolonged.

The features and advantages of the present invention will be described in detail by embodiments with reference to the accompanying drawings.

[ description of the drawings ]

Fig. 1 is a schematic perspective view of an assembled transformer mounting rack for a general aircraft according to the present invention;

fig. 2 is a schematic perspective exploded view of an assembled universal aircraft transformer mounting bracket according to the present invention;

fig. 3 is a bottom schematic view of a base of an assembled universal aircraft transformer mounting bracket of the present invention;

fig. 4 is a schematic side sectional view of an assembled transformer mounting bracket for a general-purpose aircraft according to the present invention;

in the figure: 11-base, 12-first fixed groove, 13-second fixed groove, 21-sliding plate, 22-first screw hole, 23-second screw hole, 24-first sliding block, 25-second sliding block, 31-stabilizing plate, 32-spring, 41-transformer main body, 42-bracket, 43-bolt, 44-nut and 45-sliding groove.

[ detailed description ] embodiments

Referring to fig. 1, 2, 3 and 4, the assembled transformer mounting bracket for a general aircraft according to the present invention includes a base 11, a sliding plate 21, a stabilizing plate 31 and a transformer main body 41, wherein two sides of the transformer main body 41 are respectively provided with a bracket 42 and two sliding grooves 45, the surface of the bracket 42 is provided with two bolts 43, and the top ends of the bolts 43 are provided with nuts 44; the number of the sliding plates 21 is two, the sliding plates 21 are provided with a first screw hole 22, a second screw hole 23, a first sliding block 24 and a second sliding block 25, the first screw hole 22 and the second screw hole 23 are matched with a bolt 43, and the first sliding block 24 and the second sliding block 25 are matched with a sliding groove 45; a first fixing groove 12 and a second fixing groove 13 are formed on the surface of the base 11; the number of the stabilizing plates 31 is two, six springs 32 are arranged on the surfaces of the stabilizing plates 31, the stabilizing plates 31 are matched with the transformer body 41, and the stabilizing plates 31 are matched with the base 11.

The utility model discloses the working process:

the utility model relates to a transformer mounting bracket for general aircraft of assembled is in the course of the work, base 11 and aircraft fixed connection, transformer main part 41 places directly over base 11, and stabilizer plate 31 is fixed in between base 11 and the transformer main part 41, then slides sliding plate 21 from directly over transformer main part 41 along spout 45 downwards on the end, makes first screw 22 and second screw 23 pass bolt 43, installs bolt 43 with nut 44 at last on, accomplishes the equipment of mounting bracket.

The utility model is formed by assembling the device with the base 11, the sliding plate 21, the stabilizing plate 31 and the transformer main body 41, thereby shortening the assembling and disassembling time of the mounting frame, improving the working efficiency, and once the element is damaged, only the damaged element needs to be replaced, and other elements are kept to be continuously used; the stabilizing plate 31 and the spring 32 constitute the components for assembling the transformer mounting rack, and fix the base 11 and the transformer body 41, and when the transformer body 41 vibrates during operation, the stabilizing plate has a damping effect, thereby reducing the influence on the transformer. The utility model discloses simple structure, the equipment is quick, and it is convenient to change, can extensively promote and utilize.

The above-mentioned embodiment is right the utility model discloses an explanation, it is not right the utility model discloses a limited, any right the scheme after the simple transform of the utility model all belongs to the protection scope of the utility model.

Claims

1. The utility model provides a transformer mounting bracket for general aircraft of assembled which characterized in that: the transformer comprises a base (11), a sliding plate (21), a stabilizing plate (31) and a transformer main body (41), wherein a support (42) and two sliding grooves (45) are respectively arranged on two sides of the transformer main body (41), two bolts (43) are arranged on the surface of the support (42), and nuts (44) are arranged at the top ends of the bolts (43).

2. The modular universal aircraft transformer mount of claim 1, wherein: the number of the sliding plates (21) is two, the sliding plates (21) are provided with first screw holes (22), second screw holes (23), first sliding blocks (24) and second sliding blocks (25), the first screw holes (22) and the second screw holes (23) are matched with bolts (43), and the first sliding blocks (24) and the second sliding blocks (25) are matched with sliding grooves (45).

3. The modular universal aircraft transformer mount of claim 1, wherein: the surface of the base (11) is provided with a first fixing groove (12) and a second fixing groove (13).

4. The modular universal aircraft transformer mount of claim 1, wherein: the number of stabilizer plate (31) sets up to two, stabilizer plate (31) surface is provided with six springs (32), stabilizer plate (31) and transformer main part (41) looks adaptation, stabilizer plate (31) and base (11) looks adaptation.