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A Method for Dimensional Accuracy Control of Precision Casting Turbine Guide Vanes without Allowance

A turbine guide vane and dimensional accuracy technology, applied in the field of precision casting, can solve the problems of low blade forming precision, mold scrapping, unstable quality, etc., and achieve the effect of shortening the setting cycle and ensuring consistency

Active Publication Date: 2019-05-21
AECC AVIATION POWER CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At present, the turbine guide vanes of aero-engines are affected by various factors such as precision casting molds, materials, and precision casting processes. The forming precision of the guide vanes is low, the quality is unstable, the weight is out of tolerance, and the scrap rate is high, which restricts the development of new aero-engines in my country. technical barriers
The dimensional accuracy of turbine guide vanes is mainly guaranteed by precision casting wax molds. The invention patent application "a shrinkage rate design method for multi-blade guide vane precision casting molds" (application number 201410604620.6) discloses a control of the dimensional accuracy of turbine guide vanes method, this method only considers the theoretical shrinkage of the guide vane in three dimensions, and does not take into account the influence of subsequent processing on the size of the guide vane. The dimensional accuracy of the guide vane produced by the wax mold mold designed by this method cannot meet According to the design requirements, after the guide vane is delivered for processing, if the size of the guide vane is found to be out of tolerance, the mold can only be repaired or the casting is polished, so that the setting cycle of the guide vane mold is greatly prolonged, the labor workload of the workers is increased, and the quality consistency of the guide vane cannot be guaranteed. Even cause the mold to be scrapped

Method used

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  • A Method for Dimensional Accuracy Control of Precision Casting Turbine Guide Vanes without Allowance
  • A Method for Dimensional Accuracy Control of Precision Casting Turbine Guide Vanes without Allowance

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0015] The guide vane of a high-pressure turbine of a certain machine has a blade shape tolerance of ±0.12mm and a thickness of the exhaust side of 0.8mm. The method of controlling the precision of its size is as follows:

[0016] 1. The accuracy control of the airfoil size of a high-pressure turbine guide vane: enlarge the cavity of the wax mold mold by 1.8% in the X and Y directions, and 2.2% in the Z direction, and make the airfoil surface outward along the normal direction Expanded by 0.048mm.

[0017] 2. Accurate control of the size of the exhaust side of a high-pressure turbine guide vane: extend 0.15mm along the free-form surface airfoil to the exhaust direction.

[0018] The guide vane of a high-pressure turbine manufactured by the above method meets the requirements of the design drawings, and the blade shape and chord width of each section meet the requirements of the design drawings.

Embodiment 2

[0020] The guide vane of a low-pressure turbine of a certain machine has a blade shape tolerance of ±0.14mm and a thickness of the exhaust edge of 0.6mm. The method of controlling the precision of its size is as follows:

[0021] 1. The accuracy control of the airfoil size of a high-pressure turbine guide vane: enlarge the cavity of the wax mold mold by 2.0% in the X and Y directions, and 2.3% in the Z direction, and make the airfoil surface outward along the normal direction Expanded by 0.07mm.

[0022] 2. Accurate control of the size of the exhaust side of a high-pressure turbine guide vane: extend 0.30mm along the free-form surface airfoil to the exhaust direction.

[0023] The guide vane of a low-pressure turbine manufactured by the above method meets the requirements of the design drawings, and the chord width of each section of the blade meets the requirements of the design drawings.

Embodiment 3

[0025] The guide vane of a low-pressure turbine of a certain machine has a blade shape tolerance of ±0.12mm and a thickness of the exhaust edge of 0.4mm. The method of controlling the precision of its size is as follows:

[0026] 1. The accuracy control of the airfoil size of a high-pressure turbine guide vane: enlarge the cavity of the wax mold mold by 2.0% in the X and Y directions, and 2.4% in the Z direction, and make the airfoil surface outward along the normal direction Expand 0.072mm.

[0027] 2. Accurate control of the size of the exhaust edge of a high-pressure turbine guide vane: extend 0.45mm along the free-form surface airfoil to the exhaust direction.

[0028] The guide vane of a low-pressure turbine manufactured by the above method meets the requirements of the design drawings, and the chord width of each section of the blade meets the requirements of the design drawings.

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Abstract

The invention belongs to the precision casting technology, and relates to a method for controlling the dimensional accuracy of a precision casting turbine guide vane without margin. It is characterized in that the steps of controlling the size precision of the guide vane are as follows: the precision control of the airfoil size of the guide vane; the precision control of the size of the exhaust side of the guide vane. The invention proposes a method for controlling the dimensional accuracy of the turbine guide vane without margin. Considering the impact of subsequent processing on the blade size, the dimensional accuracy of the guide vane meets the design requirements, shortens the setting cycle of the guide vane mold, and ensures Consistency of guide vane quality.

Description

technical field [0001] The invention belongs to the precision casting technology, and relates to a method for controlling the dimensional accuracy of a precision casting turbine guide vane without margin. Background technique [0002] Aeroengine turbine guide vane is a part composed of a large number of free-form surfaces and edge plates, and its aerodynamic shape, dimensional accuracy, edge plate profile, and forming accuracy require high requirements. At present, the turbine guide vanes of aero-engines are affected by various factors such as precision casting molds, materials, and precision casting processes. The forming precision of the guide vanes is low, the quality is unstable, the weight is out of tolerance, and the scrap rate is high, which restricts the development of new aero-engines in my country. technical obstacles. The dimensional accuracy of turbine guide vanes is mainly guaranteed by precision casting wax molds. The invention patent application "a shrinkage r...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B22C9/04B22C9/22B22C7/02G05D5/00
CPCG05D5/00B22C7/02B22C9/04B22C9/22
Inventor 朱珍珠王琳海潮常涛岐马李朝汪国峰闵蓉张军
Owner AECC AVIATION POWER CO LTD
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