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A temperature compensation method for machining aluminium alloy components

A technology for aluminum alloy parts and temperature compensation, which is applied in the field of temperature compensation for machining aluminum alloy parts, and can solve the problems of thin wall thickness, poor rigidity, and large coefficient of linear expansion.

Inactive Publication Date: 2011-08-31
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Abstract
  • Description
  • Claims
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Problems solved by technology

[0002] Some aluminum alloy parts have complex structures, large diameters, and thin walls. At present, when processing such parts, the actual value of the part size after on-site processing is usually inconsistent with the actual value of the part at the standard temperature detected in the testing room. The reason is that Aluminum alloy parts have poor rigidity, weak strength, and large linear expansion coefficient. After processing at non-standard temperature, the actual value of the part size is very different from the actual value of the part measured at the standard temperature (20°C). error, resulting in parts being scrapped due to out-of-tolerance dimensions

Method used

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  • A temperature compensation method for machining aluminium alloy components
  • A temperature compensation method for machining aluminium alloy components

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Embodiment

[0020] The processed parts are made of aluminum alloy, the maximum diameter is Φ1167.0284±0.127, the diameter of a place being processed is Φ1145.7432, the tolerance is ±0.05, and the standard parts are tool steel;

[0021] The linear expansion coefficient of aluminum alloy parts is 0.0000225, and the linear expansion coefficient of tool steel standard parts is 0.0000117;

[0022] The specific working process is as follows:

[0023] 1) Measure the temperature of standard parts and the temperature of processed parts;

[0024] Use a contact temperature measuring instrument to measure the temperature of the part. After the reading is stable, record the actual temperature value. The temperature of the part is 24℃; the material of the standard part is tool steel. Use the contact temperature measuring instrument to measure the temperature of the standard part until the reading is stable. After recording the actual temperature value, the temperature is 22℃;

[0025] 2) After zeroing on the st...

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Abstract

The invention provides a temperature compensation method for machining aluminium alloy components. The method comprises the steps of (1) measuring temperatures of a standard component and a to-be-machined component; (2) measuring a dimension of the to-be-machined component after making a zero-setting of a measuring device according to the standard component; (3) making temperature compensation calculation according to formulas to obtain a conversion dimension; (4)doing compensation calculation according to the component temperature, the standard component temperature, the actual value of the component dimension under a working temperature and the conversion dimension. In the method, the conversion dimension is calculated from the relationship among temperature, coefficient of linear expansion, and nominal dimension. The actual value of the component dimension measured under a working temperature is converted to an actual value of the component dimension under a standard temperature, thereby realizing precise measurement. In component machining process, the value of the sum of the component nominal dimension and the conversion dimension is taken as a dimension value required for the component machining, thereby realizing the aim of precise machining. The method in the invention can be applied to the aluminium alloy components machining with high precision requirements.

Description

Technical field [0001] The invention belongs to the technical field of mechanical processing, and particularly relates to a temperature compensation method for cutting and processing aluminum alloy parts. Background technique [0002] Some aluminum alloy parts are complex in structure, large in diameter, and thin in wall thickness. At present, when processing such parts, the actual value of the part size after on-site processing is usually inconsistent with the actual value of the part detected in the inspection room at the standard temperature. The reason is The aluminum alloy parts have poor rigidity, weak strength, and large linear expansion coefficient. After processing at non-standard temperature, the actual value of the part size and the actual value of the part detected at the standard temperature (20℃) are very large. Errors cause the parts to be out of tolerance and scrapped. Summary of the invention [0003] In view of the above-mentioned problems in the prior art, the ...

Claims

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Application Information

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IPC IPC(8): G01B21/00G01D3/028
Inventor 邸阅文刘鸣陈桂荣叶红雨魏晓丽
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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