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A large-diameter non-metallic skin turning device

A processing device, non-metallic technology, applied in the field of large-diameter non-metallic skin turning processing device, to achieve the effect of reducing weight, fast, flexible and convenient processing, and improving mobility

Active Publication Date: 2019-02-19
CAPITAL AEROSPACE MACHINERY +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to overcome the above-mentioned deficiencies in the prior art, provide a large-diameter non-metallic skin turning processing device, solve the current urgent problem of turning the outer circle of the tail section skin, and develop new models for the follow-up The processing tooling required in the process provides basic data and design ideas

Method used

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  • A large-diameter non-metallic skin turning device
  • A large-diameter non-metallic skin turning device

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Embodiment Construction

[0022] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:

[0023] It is known that the commonly used materials for the skin of the tail section of the XX-5 launch vehicle are non-metallic materials such as high-strength glass cloth (SW180D-90a) or barium phenolic resin (DFQS-3-75). Combined with the structure diagram of the tail section skin, we can get: the tail section skin has a large diameter, small thickness and is easy to deform. During the turning process of the outer circle of the product, it is easy to produce large deformation, which affects the processing accuracy and processing quality. At present, the existing Processing tooling has been unable to meet the processing requirements. Therefore, there is an urgent need for a tool that can fully adapt to the turning of the outer circle of the tail section of a large launch vehicle, so a large-diameter non-metallic skin turning device came into b...

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Abstract

The invention relates to the field of large launcher tail section skin outer circle machining, in particular to a large-diameter nonmetal skin turning device. The large-diameter nonmetal skin turningdevice comprises a blank body, an upper end plate, a pedestal set, a bottom plate, an upper pressing plate set, a lower pressing plate set and a fastening device set. The blank body is of a hollow cylindrical structure which is vertically placed, and the upper end plate is of a circular plate structure and is concentrically fixedly mounted at the axial top end of the blank body. The bottom plate is of a ring structure and is concentrically fixedly mounted at the axial bottom end of the blank body, and the pedestal set is fixedly mounted on the connecting position of the blank body and the bottom plate. The outer wall of the blank body is wrapped with an outer skin structure, and the upper pressing plate set is fixedly mounted on the side wall of the top end of the outer skin structure. Thelower pressing plate set is fixedly mounted on the side wall of the bottom end of the outer skin structure, and the side wall of the outer skin structure is sleeved with the fastening device set. According to the large-diameter nonmetal skin turning device, the current impending technological problem of tail section skin outer circle turning is solved, and essential data and design thoughts are provided for machining tools needed in the subsequent new model development process.

Description

technical field [0001] The invention relates to the field of machining the outer circle of the skin of the tail section of a large launch vehicle, in particular to a large-diameter non-metallic skin turning processing device. Background technique [0002] The tail section skin of the large launch vehicle is composed of 4 columnar structures made of non-metallic materials with a centripetal angle of 90°, a diameter of Ф4996mm, and a height of 2624mm. The turning method is the most reliable forming method for the outer circle of the tail section skin of the launch vehicle at the present stage. This project is mainly aimed at the turning processing of the outer circle of the tail section of the large launch vehicle, and the design of the processing tooling. In view of the characteristics of large diameter, small thickness and easy deformation of the skin of the tail section of a large launch vehicle, the fixed tooling in the process of turning the outer circle of the skin not ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23B5/00B23Q3/00
CPCB23B5/00B23Q3/00B23Q2703/10
Inventor 冯宪冬孔德跃王志峰毕煌圣刘海燕毛京伟左官抒王玲胡改娟杨中宝陈振华
Owner CAPITAL AEROSPACE MACHINERY
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