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Aerospace cable fairing forming device

A technology for cable fairings and forming devices, which is applied in the direction of forming tools, transportation and packaging, safety equipment, etc., and can solve the problems of not having the function of ejecting blanks, calibration and adjustment of the position of the raw material alloy plate of the fairing, etc., so as to achieve easy replacement Or maintenance, convenient assembly and disassembly, and the effect of reducing labor intensity

Pending Publication Date: 2022-06-28
JIANGSU TONGDA MACHINERY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above problems, the object of the present invention is to propose a forming device for aerospace cable fairings, which solves the problem that existing stamping and forming devices for aerospace cable fairings cannot conveniently assemble and disassemble forming molds, do not have the function of blank ejection and cannot The problem of automatic position calibration and adjustment of the fairing raw material alloy sheet

Method used

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  • Aerospace cable fairing forming device
  • Aerospace cable fairing forming device
  • Aerospace cable fairing forming device

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Embodiment Construction

[0026] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0027] In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. The indicated orientation or positional relationship is based on the orientation or positional relationship shown in the accompanying drawings, which is only for the convenience of describing the present invention and simplifying the description, rather than ...

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Abstract

The spaceflight cable fairing forming device comprises a punching machine table, and a machine cover is fixed to the top end of the punching machine table; the first positioning columns on the supporting plate are automatically driven to be inserted into the first positioning holes in the two sides of the lower mold to complete assembling and fixing of the lower mold, and the second positioning columns are automatically driven to be inserted into the second positioning holes to complete assembling and fixing of the upper mold, so that the forming mold can be conveniently and rapidly assembled and disassembled through the device; a servo motor drives a second lead screw to rotate, a limiting box clamps the left side and the right side of the alloy plate, meanwhile, a two-way air cylinder is started to drive a clamping plate and a limiting plate to move towards the alloy plate and clamp the front side and the rear side of the alloy plate, and automatic calibration and adjustment of the position of the alloy plate are completed. Therefore, the device can automatically calibrate and adjust the position of a fairing raw material alloy plate, and the fairing body is ejected out of the fairing die cavity by rotating the rotary table to drive the ejection block, so that a fairing blank formed by punching is easy to take out.

Description

technical field [0001] The invention relates to the technical field of aerospace parts processing, in particular to an aerospace cable fairing forming device. Background technique [0002] Spacecraft, also known as space vehicle and space vehicle, operate in space according to the laws of celestial mechanics, and perform various types of aircraft such as exploration, development, and utilization of space and celestial bodies. Composed of instrument cabin, engine and control system, the spacecraft runs outside the earth's atmosphere after getting rid of the obstacles of the atmosphere, and can receive all electromagnetic radiation information from cosmic celestial bodies, opening up full-band astronomical observations. When the spacecraft is in the atmosphere During high-speed flight, the oncoming airflow and the spacecraft cabin are suddenly compressed, and the local airflow will be blocked. At the same time, friction between the air flow and the surface of the cabin will oc...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B21D22/02B21D37/14B21D37/10B21D55/00B21D45/02B21D53/92
CPCB21D22/02B21D37/14B21D37/10B21D55/00B21D45/02B21D53/92
Inventor 王雷沈进
Owner JIANGSU TONGDA MACHINERY