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A special orthopedic equipment for aerospace special-shaped extrusion structural parts

A technology for structural parts and equipment, applied in the field of special orthopedic equipment, can solve the problems of poor versatility, low efficiency and precision

Inactive Publication Date: 2016-06-29
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These orthopedic machines have problems such as poor versatility, low efficiency and low precision in the orthopedics of aeronautical structural parts, so it is very necessary to design a flexible, high-precision and high-efficiency orthopedic machine for orthopedic aeronautical structural parts

Method used

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  • A special orthopedic equipment for aerospace special-shaped extrusion structural parts
  • A special orthopedic equipment for aerospace special-shaped extrusion structural parts
  • A special orthopedic equipment for aerospace special-shaped extrusion structural parts

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Embodiment Construction

[0022] Embodiments of the present invention will be described in detail below, and the same or similar symbols throughout the drawings of the embodiments represent the same or similar elements or elements with the same or similar functions. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0023] In the description of the present invention, the orientation or positional relationship indicated by the terms "front", "rear", "left", "right", "upper" and "lower" are based on the orientation or positional relationship shown in the drawings, The disclosure is merely for convenience in describing the invention and does not require that the invention must be constructed and operated in a particular orientation, and thus should not be construed as limiting the invention.

[0024] Below in conjunction with accompanying drawing and embodiment, design principl...

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Abstract

The invention relates to a shape-correcting device special for an aerial irregularly shaped extruding structure component. The shape-correcting device is composed of two parts, i.e., a hardware system and a software system, wherein the hardware system mainly comprises a roller system, a main driving system, a screw rod feeding system and a frame; the software system is divided into two parts; one part takes a displacement sensor as a main part for controlling the feeding precision; the other part takes a force sensor as a main part for optimizing the correcting according to a correcting experience. Compared with the prior art, the shape-correcting device has the advantages that the bending-torsion compound correcting is adopted, and the correcting precision is high; the digital correcting is adopted, so that the efficiency is high; parts in different sizes are corrected, and the flexibility is high.

Description

technical field [0001] The invention relates to a digitally adjustable special orthopedic device for testing different sizes of aerospace special-shaped extruded structures. Background technique [0002] The use of structural parts occupies a very important position in the design of aviation products, and is the most important part of the aircraft's aerodynamic shape and body skeleton. The material of aerospace structural parts is mostly made of aluminum alloy. Due to the complex shape and poor welding performance in the actual processing process, in order to ensure the accuracy, extrusion molding is often used for processing and production. Due to the influence of various factors, the workpiece often has shape defects during extrusion, cooling and transportation. Some profiles will have arc bending or section deformation such as flange inward, outward expansion and torsion. In order to control the accuracy of the workpiece, it is necessary to correct the workpiece to obta...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21D3/02B21C51/00
CPCB21C51/00B21D3/02
Inventor 吴琼李大鹏张以都司宇
Owner BEIHANG UNIV
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