Titanium Alloy Notched Bolts

A titanium alloy and notch technology, applied in the field of spacecraft structure, can solve the problems of unknown interruption performance, uncontrollable separation method, failure to meet the requirements of the connection and separation performance of the two halves of the fairing, and achieve enhanced separation performance and increased The effect of large size ratio and increased surface contact stiffness

Active Publication Date: 2014-02-19
BEIJING INST OF ASTRONAUTICAL SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the existing connection is designed as a common bolt, which can only meet the connection reliability, its breaking performance is unknown, and the separation method is uncontrollable, which cannot meet the connection and separation performance requirements of the two halves of the fairing.

Method used

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  • Titanium Alloy Notched Bolts
  • Titanium Alloy Notched Bolts
  • Titanium Alloy Notched Bolts

Examples

Experimental program
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Embodiment Construction

[0019] The present invention will be further described below with reference to the accompanying drawings.

[0020] Such as figure 1 As shown, the titanium alloy recess bolt of the present invention includes bolt head 1 and screw 2; the upper portion of the bolt head 1 is a hexagonal shape, the lower portion of the bolt head 2 is a cylinder; the cylinder diameter is greater than the diameter of the hexagonal outer circle; screw 1 Mid-open recess 3; the bottom of the screw 1 is threaded 4, and the thread 4 is connected through the nut.

[0021] In this embodiment, the bolt tensile force is required to be 1.4 tons, and the material uses TB2 titanium alloy material. After solid solution, the aging heat treatment process, the design static indicator is achieved, and the static connection requirements of the long-range head longitudinal separation device are met.

[0022] The bolt head 1 of the titanium alloy recess bolts of the present invention uses the mesh, and the specific structur...

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PUM

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Abstract

The invention discloses a titanium alloy notch bolt, which comprises a bolt head (1) and a screw rod (2); the upper part of the bolt head (1) is hexagonal, and the lower part of the bolt head (1) is a cylinder; the cylinder The diameter is larger than the diameter of the hexagonal outer circle, and when the bolt head is in contact with the loaded surface, the cylinder acts as a gasket; the screw rod (2) has a notch (3) in the middle. In the notch bolt of the present invention, a notch (3) is designed in the middle of the screw rod (2). While satisfying the static connection performance, the separation power provided by the pyrotechnic device to the notch at the moment of separation realizes reliable and efficient separate. Simultaneously, the notch bolt of the present invention adopts an integrated design, and the cylinder at the lower part of the bolt head (1) plays the role of a gasket, which reduces the loading surface of the bolt head and the contact surface of the gasket, increases the surface contact stiffness, and makes the concave Port bolts improve separation performance by increasing the stiffness of the contact surface under high dynamic shock loads.

Description

Technical field [0001] The present invention belongs to the field of spacecraft structure, and in particular, the present invention relates to a bolt that can complete the connection and separation of dual functions. Background technique [0002] During the rocket launch, in the atmosphere, the rocket rectification provides a basic closed and temperature-stable space to avoid flying pneumatic heating to produce ablation, and guarantees a good pneumatic shape, reducing aerodynamic resistance, increasing flight stability. After flying out of the atmosphere, the Rocket needs to throw off the rectifier, reducing the rocket itself, and increasing the launch capacity. Therefore, a structure for connection is required during the rocket flight. In the atmosphere, the entire flow cover is connected to a whole; in addition to the atmosphere, the bolt will be bolted under the conditions of the fireworks. Interrupt to achieve a whole flow shield. When separated, the separation displacement p...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16B33/02F42B15/36
Inventor 任东鸿张晓晖苏晗卢红立宋保永
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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