Breaking-in tool for spacecraft ground and on-rack fasteners

A technology of spacecraft and fasteners, which is applied in the direction of manufacturing tools, metal processing, metal processing equipment, etc., and can solve the problems that fasteners cannot be removed normally

Inactive Publication Date: 2014-10-29
BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The purpose of the present invention is to provide a tool integrated with a general-purpose handheld drilling device, a dust suction device, and a waste control box, which is suitable for fasteners

Method used

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  • Breaking-in tool for spacecraft ground and on-rack fasteners
  • Breaking-in tool for spacecraft ground and on-rack fasteners

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Embodiment Construction

[0018] The following describes the spacecraft ground and on-orbit fastener breaking tool of the present invention in detail with reference to the accompanying drawings, but the description is only exemplary and is not intended to limit the protection scope of the present invention in any way.

[0019] See figure 1 , figure 1 It is the spacecraft ground and on-orbit fastener breaking tool of the present invention, which mainly includes a dust suction device 1, a handheld drilling device 2 and a redundant control box 3. Among them, the dust suction inlet of the dust suction device 1 passes through a dust suction pipe It is connected to the interface provided on the side of the excess control box. This interface is a rigid interface. The flexible inlet pipe of the dust suction device is compressed to ensure that the dust can be effectively sucked into the dust suction device while ensuring that the dust does not spread. There is a hole on the top so that the drill bit of the hand-hel...

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Abstract

The invention discloses a breaking-in tool for spacecraft ground and on-rack fasteners. The breaking-in tool mainly comprises a dust suction device, a handheld drilling device and a redundancy control box, wherein a dust suction pipe of the dust suction device is communicated with the interior of a box body of the redundancy control box through a connector arranged on the side face of the redundancy control box to ensure that powdered scraps can be effectively sucked into the dust suction device without diffusing; the top of the redundancy control box is provided with a hole so that a drill bit of the handheld drilling device can extend into the redundancy control box to break in and damage the fasteners; the redundancy control box is made of transparent organic glass, and multiple layers of brushes are arranged on the inner side of the box body of the redundancy control box and surrounding the hole in the top to tightly attach to the drill bit of the handheld drilling device and prevent the powdered scraps from diffusing out. The breaking-in tool achieves the technical effect of breaking-in of the fasteners in a confined space and a pollution-sensitive environment, achieves clean dismantling of the fasteners in an abnormal state, and meets the demand for assembly of the spacecraft ground and on-rack fasteners.

Description

Technical field [0001] The invention belongs to the technical field of spacecraft ground machinery, and in particular relates to a demolition tool, which uses a dust suction device, a surplus control box and a hand-held drilling device to destroy abnormal fastener nuts, thereby realizing fastener removal Features. Background technique [0002] At present, the transfer of cargo on the manned spacecraft and the maintenance and replacement of equipment on orbit involve the removal of fasteners. Due to the combined effects of structural deformation, fastener anti-loosening glue curing, fastener corrosion and other factors, there is a certain probability of occurrence Fasteners “seize” and rounded nuts cause the problem of fasteners that cannot be removed. For this reason, fasteners need to be destructively removed. For manned spacecraft fasteners, the following difficulties need to be addressed: [0003] Strict requirements for the control of redundant objects: Manned spacecraft has s...

Claims

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Application Information

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IPC IPC(8): B23P19/04B23B45/00B25F5/00
CPCB23B45/00B23Q11/0046B23Q11/0071
Inventor 邢帅杜瑞兆易旺民贺云代海林肖正懿孟伟张成立姜旭李东王鹏飞
Owner BEIJING INST OF SPACECRAFT ENVIRONMENT ENG
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