Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Manufacturing method for large-scale thin-wall skin with inner ribs and complex mold cavities

A manufacturing method and skinning technology, applied in the field of mechanical processing, can solve the problems of high difficulty in CNC machining, low pass rate, large skin deformation, etc., and achieve the goals of simplifying the difficulty of CNC machining, accurately ensuring wall thickness, and improving surface accuracy Effect

Active Publication Date: 2016-03-16
BEIJING HANGXING MACHINERY MFG CO LTD
View PDF5 Cites 13 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, although large-scale thin-walled skins have many advantages in aviation weapons, the processing deformation of large-scale thin-walled skins has been plaguing the aerospace industry for many years. Measures are not perfect
[0003] At present, in the manufacturing process of this kind of parts, part of the panel is bent into a skin structure first, and then the ribs and weight-reducing cavity are processed by a multi-axis machining center. The CNC machining is difficult and complicated; The cavity is processed down, and then the skin is formed by mechanical means such as a bending machine, resulting in large deformation of the skin, and the precision of the formed skin surface is low, and the pass rate is low, which seriously affects the progress of the model product.

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Manufacturing method for large-scale thin-wall skin with inner ribs and complex mold cavities
  • Manufacturing method for large-scale thin-wall skin with inner ribs and complex mold cavities
  • Manufacturing method for large-scale thin-wall skin with inner ribs and complex mold cavities

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0019] The test part is a skin part in a certain type of missile. The material of the part is 7A04 aluminum alloy. The product structure is a thin-walled part with inner ribs and complex inner cavity. The wall thickness of the large skin is 4mm, see attached figure 1 .

[0020] (1) Collect the original skin geometric parameters, simulate and flatten the skin, collect the corresponding data after flattening, program rough machining and finishing machining, and calculate the required minimum blank:

[0021] According to the specific structure of the required skin, collect its geometric parameters, and then use UG sheet metal modeling software to simulate and expand it into a flat state, see the attached figure 2 , get the corresponding geometric parameters after flattening, and program roughing and finishing according to these parameters.

[0022] Principle: According to the specific structure and size of the skin parts and the characteristics of flat plate bending and circle...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

PropertyMeasurementUnit
Wall thicknessaaaaaaaaaa
Wall thicknessaaaaaaaaaa
Login to View More

Abstract

The invention provides a manufacturing method for a large-scale thin-wall skin with inner ribs and complex mold cavities. The manufacturing method comprises the steps that 1, simulation flattening is conducted on the skin according to a skin parameter, a parameter of the flattened skin is collected, a rough machining programming and a finish machining programming are conducted, and a minimum workblank is calculated; 2, the minimum workblank is selected to be machined roughly in order to release residual stress inside the workblank in advance; 3, a roughly machined skin plate is adsorbed and fixed through a vacuum tire, finish machining is conducted on the skin plate, and the rib strips and the weight reducing cavities inside the skin are machined out through numerical control milling machining; 4, a plurality of base plates which can fill and level up each weight reducing cavity are prepared, it is ensured that the skin machined through the step 3 again becomes a slab with the flat surface after each base plate is cushioned, and then the skin is machined to be formed through a matched mould thermal forming method, and 5, annealing and stress-relieving are conducted. According to the manufacturing method for the large-scale thin-wall skin with the inner ribs and the complex mold cavities, the deformation of the thin-wall skin in the machining process is effectively controlled, and the molded surface precision of the skin is greatly improved.

Description

technical field [0001] The invention belongs to the technical field of mechanical processing and relates to a method for manufacturing a large thin-walled aluminum alloy skin with internal ribs and complex cavities, which is suitable for the precise manufacture of large thin-walled skin parts for aerospace. Background technique [0002] At present, more and more large thin-walled skin parts are used in the aerospace field. In order to reduce the weight and improve the mechanical properties of aviation weapons in the modern aerospace field, more and more large thin-walled skinned Leather parts. However, although large thin-walled skins have many advantages in aviation weapons, the processing deformation of large-scale thin-walled skins has been plaguing the aerospace industry for many years. At present, the research on the processing technology of large thin-walled skins is not deep enough. The measures are not yet perfect. [0003] At present, in the manufacturing process ...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
IPC IPC(8): B23P15/00
CPCB23P15/00
Inventor 何艳涛王波张素敏闫寒张树科
Owner BEIJING HANGXING MACHINERY MFG CO LTD
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products