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Aircraft hanging beam dismounting bracket

An aircraft and top block technology, which is applied to aircraft parts, wings, equipment for loading and unloading goods, etc., can solve the problems of difficult disassembly of vertical-axis aircraft hanger beams, achieve easy popularization and application, avoid damage and deformation, and facilitate production. Effect

Active Publication Date: 2019-04-12
JIANGXI HONGDU AVIATION IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The purpose of the present invention is to provide a dismantling bracket for an aircraft hanging beam. In order to solve the problem of difficulty in dismantling a vertical-axis aircraft hanging beam, a dismantling bracket for an aircraft hanging beam is provided here, which can ensure that the front and rear vertical shafts are disassembled synchronously

Method used

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  • Aircraft hanging beam dismounting bracket
  • Aircraft hanging beam dismounting bracket
  • Aircraft hanging beam dismounting bracket

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Embodiment Construction

[0025] The present invention is described in detail below in conjunction with accompanying drawing:

[0026] A dismantling bracket for an aircraft hanging beam, characterized in that: the dismantling bracket for an aircraft hanging beam includes: an upper top block 1, a left strut 2, a right strut 3, a left tie rod 4, a right pull rod 5, an adjusting screw 6, and a left top block 7 and top right block 8;

[0027] The two sides of the upper top block 1 are connected with the left strut 2 and the right strut 3 by bolts, the left pull rod 4 is connected with the left strut 2 through the hole, the right pull rod 5 is connected with the right strut 3 through the hole, and the adjusting screw 6 is connected with the screw thread. The left tie rod 4 and the right tie rod 5 are connected, the left jacking block 7 is connected with the left strut 2 through a spherical joint, and the right jacking block 7 is connected with the right strut 3 through a spherical joint.

[0028] There is ...

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PUM

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Abstract

The invention relates to an aircraft hanging beam dismounting bracket, which belongs to the technical field of aircraft design and relates to aircraft hanging beam design and ground maintenance technology. The aircraft hanging beam dismounting bracket includes an upper top block, a left supporting pole, a right supporting pole, a left pull rod, a right pull rod, an adjusting screw rod, a left topblock, and a right top block; and both sides of the upper top block are connected with the left supporting pole and the right supporting pole by bolts, the left pull rod is connected with the left supporting pole through a hole, the right pull rod is connected with the right supporting pole through the hole, the adjusting screw rod is connected with the left pull rod and the right pull rod throughthreads, the left top block is connected to the left supporting pole by a ball joint, and the right top block is connected to the right supporting pole by the ball joint. The bracket is simple in structure, is clear in principle, is convenient to produce, is strong in practicability, is easy to popularize and apply, and has great value.

Description

technical field [0001] The invention relates to a dismantling support for an aircraft hanging beam, belongs to the technical field of aircraft design, and relates to the design of an aircraft hanging beam and the ground maintenance technology. Background technique [0002] The ability to store weapons is an important indicator of the aircraft. Usually, external storage points are set on the wings and connected to the wings through hanging beams. For a simpler structure and lighter weight, a vertical shaft hanging beam is often used, and the front and rear vertical shafts are connected to the joints on the wings. However, problems such as difficulty in disassembly and damage to the wing skin often occur during the disassembly process of this hanging beam. During routine maintenance, the ground crew needs to stand on the wing and use a hammer to knock out the vertical shaft from the joint little by little. When one of the vertical shafts is knocked out, the hanging beam will ...

Claims

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Application Information

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IPC IPC(8): B64D9/00B64C3/00
CPCB64C3/00B64D9/00
Inventor 王震朱亲强张爱茹王红飞项小平杜龙杜兴刚张海周王月英龚思楚姜亚娟王学强朱翔李朝光余凌晶顾张亮
Owner JIANGXI HONGDU AVIATION IND GRP
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