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Precision forging method for miniature TC11 titanium alloy blades

A technology of TC11 and titanium alloy, which is applied in the field of titanium alloy forging, can solve the problems of increased manufacturing cost, curved airfoil profile, large torsional deformation, and out-of-tolerance blade size, so as to reduce manufacturing cost, improve pass rate, Reduce the effect of bending

Active Publication Date: 2015-05-27
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantages of the above precision forging method are: the profile of the blade body is curved and the torsional deformation is large, resulting in out-of-tolerance blade dimensions, high product rejection rate, and increased manufacturing costs
The reason is that the temperature of the mold and the billet is low, the internal stress of the forging is large, the stack cooling and diffused air cooling are inconsistent after forging, and the temperature difference of the micro precision forging blade increases to cause deformation

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0015] Example 1: The first stage rotor blade of a certain type of TC11 titanium alloy missile fan is processed. The length of the blade body is 35.8mm, the minimum thickness of the exhaust edge of the blade body profile is only 0.056mm, and the phase transition point of this batch is 990°C.

[0016] 1. Heating the forging billet and precision forging die: put the forging billet of the miniature TC11 titanium alloy blade into the heating furnace and heat it to 940℃ below the phase transition point, and use the high-temperature converter for circulating heating, and put one piece into the furnace every 0.2min. , filled with 42 pieces and started forging the first piece. After each piece was forged, one piece was reloaded into the furnace, and the manual control of the converter rotation was repeated in this way, and the temperature was kept for 6min-18min; the use temperature of the precision forging die was 210 °C;

[0017] 2. Precision forging: Put the forging blank of the min...

Embodiment 2

[0020] Example 2, dealing with the secondary rotor blade of a certain type of TC11 titanium alloy missile fan, the length of the blade body is 32.3mm, the minimum thickness of the exhaust edge of the blade body profile is only 0.066mm, and the phase transition point of this batch is 995°C.

[0021] 1. Heating the forging billet and precision forging die: Put the forging billet of the miniature TC11 titanium alloy blade into the heating furnace and heat it to 945°C below the phase transition point, use a high-temperature converter for circulating heating, and put one piece into the furnace every 0.25min. , filled with 45 pieces and started forging the first piece. After each piece of forging, reloaded one piece into the furnace, and repeated the manual control of the converter rotation, and kept the temperature for 5min to 16min; the use temperature of the precision forging die was 215 ℃;

[0022] 2. Precision forging: Put the forging blank of the miniature TC11 titanium alloy b...

Embodiment 3

[0025] Example 3: The first stage stator blade of a certain type of TC11 titanium alloy missile fan is processed. The length of the blade body is 28.0mm, the minimum thickness of the exhaust edge of the blade body profile is only 0.086mm, and the phase transition point of this batch is 1000°C.

[0026] 1. Heating the forging billet and precision forging die: Put the forging billet of the miniature TC11 titanium alloy blade into the heating furnace and heat it to 950 ℃ below the phase transition point, and use the high-temperature converter for circulating heating, and put one piece into the furnace every 0.30min. , filled with 48 pieces and started forging the first piece. After each piece of forging, reloaded one piece into the furnace, and repeated the manual control of the converter rotation, and kept the temperature for 8min to 18min; the use temperature of the precision forging die was 220 ℃;

[0027] 2. Precision forging: Put the forging blank of the miniature TC11 titani...

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Abstract

The invention belongs to a titanium alloy forging technology and relates to an improvement of a precision forging method for miniature TC11 titanium alloy blades. The precision forging method is characterized by comprising the steps of stock heating and forging, and die precision forging; precision forging; cooling; and thermal processing. By means of the precision forging method, the bending and torsion deformation of blade profiles is reduced, the product qualified rate is improved, and the manufacture cost is reduced.

Description

technical field [0001] The invention belongs to the titanium alloy forging technology, and relates to the improvement of the precision forging method of the TC11 titanium alloy miniature precision forging blade. Background technique [0002] A TC11 titanium alloy miniature precision forging blade is characterized by small size, the length of the blade body is generally about 8-50mm, the blade body profile is thin, and the minimum thickness of the inlet and exhaust edges is only about 0.08mm. The current precision forging method is as follows: the first step, heating the forging blank and the precision forging die: put the forging blank of the miniature TC11 titanium alloy blade into a heating furnace and heat it to 940 ° C, and use a high-temperature converter to circulate and heat for 5 minutes to 20 minutes; The temperature of the forging die is 150℃~200℃; the second step, precision forging: put the forging blank of the miniature TC11 titanium alloy blade into the precisio...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B21K3/04C22F1/18
Inventor 宋占利李长青王永杰吴娟利范晖户良东徐迈阳
Owner AECC AVIATION POWER CO LTD