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A process method for aluminizing the inner cavity and outer surface of a cobalt-based alloy blade

A technology of cobalt-based alloy and process method, which is applied in the field of heat treatment, can solve problems such as shallow penetration layer depth and uncontrollable gas method, and achieve the effects of improving oxidation resistance, wide application value, and prolonging service life

Active Publication Date: 2017-12-08
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The gas method is consistent with the chemical vapor deposition method in principle, but the gas method is uncontrollable and the depth of the infiltrated layer is shallow

Method used

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  • A process method for aluminizing the inner cavity and outer surface of a cobalt-based alloy blade
  • A process method for aluminizing the inner cavity and outer surface of a cobalt-based alloy blade
  • A process method for aluminizing the inner cavity and outer surface of a cobalt-based alloy blade

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Effect test

Embodiment 1

[0030] In this embodiment, in order to improve the anti-oxidation and anti-corrosion properties of the blade surface, the process of aluminizing the inner cavity and outer surface of the cobalt-based alloy blade is carried out according to the following steps:

[0031] 1. Preparation of aluminum particles

[0032] Appropriate amount of aluminum particles is spread in the reactor (generating reactor outside the reaction chamber and generating reactor inside the reaction chamber).

[0033] 2. Parts preparation

[0034] (1) Use a liquid sand blasting machine to perform water blasting treatment on the parts to be deposited on the coating to remove the surface oxide layer;

[0035] (2) Put the parts in a water-based detergent solution with a mass fraction of 8%, use an ultrasonic cleaner to ultrasonically clean them for 25 minutes, rinse them with clean water, dehydrate them with absolute ethanol, and dry them with a hair dryer;

[0036] (3) Install the parts on the fixture, and ...

Embodiment 2

[0043] In this embodiment, in order to improve the anti-oxidation and anti-corrosion properties of the blade surface, the process of aluminizing the inner cavity and outer surface of the cobalt-based alloy blade is carried out according to the following steps:

[0044] 1. Preparation of aluminum particles

[0045] Appropriate amount of aluminum particles is spread in the reactor (generating reactor outside the reaction chamber and generating reactor inside the reaction chamber).

[0046] 2. Parts preparation

[0047] (1) Use a liquid sand blasting machine to perform water blasting treatment on the parts to be deposited on the coating to remove the surface oxide layer;

[0048] (2) Put the parts in a water-based cleaning agent solution with a mass fraction of 5%, use an ultrasonic cleaner to ultrasonically clean them for 20 minutes, rinse them with clean water, dehydrate them with absolute ethanol, and dry them with a hair dryer;

[0049] (3) Install the parts on the fixture....

Embodiment 3

[0056] In this embodiment, in order to improve the anti-oxidation and anti-corrosion properties of the blade surface, the process of aluminizing the inner cavity and outer surface of the cobalt-based alloy blade is carried out according to the following steps:

[0057] 1. Preparation of aluminum particles

[0058] Appropriate amount of aluminum particles is spread in the reactor (generating reactor outside the reaction chamber and generating reactor inside the reaction chamber).

[0059] 2. Parts preparation

[0060] (1) Use a liquid sand blasting machine to perform water blasting treatment on the parts to be deposited on the coating to remove the surface oxide layer;

[0061] (2) Put the parts in a water-based cleaning agent solution with a mass fraction of 10%, use an ultrasonic cleaner to ultrasonically clean them for 30 minutes, rinse them with clean water, dehydrate them with absolute ethanol, and dry them with a hair dryer;

[0062] (3) Install the parts on the fixture...

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Abstract

The invention belongs to the field of heat treatment, in particular to a process method for aluminizing the inner cavity and the outer surface of a cobalt-based alloy blade. The high-pressure turbine guide vane of the engine is made of DZ40M cobalt-based casting alloy. It is an important hot-end part of the aero-engine. The working environment is relatively harsh. Technology, that is, the aluminized layer is prepared on the surface of the inner cavity and outer flow channel of the high guide vane at the same time to improve the reliability and service life of the blade. The method of the invention can meet the design and manufacture requirements of the high-pressure turbine guide vane of the engine, the depth of the aluminized layer on the surface of the outer flow channel of the high guide vane is 0.02mm-0.055mm, and the depth of the aluminized layer in the inner cavity is 0.01mm-0.035mm. The effect of chemical vapor deposition aluminizing on the surface of the blade is remarkable, the oxidation resistance of the blade is twice as high as that of the substrate, and the corrosion resistance is doubled, prolonging the service life of the blade.

Description

technical field [0001] The invention belongs to the field of heat treatment, in particular to a process method for aluminizing the inner cavity and the outer surface of a cobalt-based alloy blade. Background technique [0002] Engine high-pressure turbine guide vanes are important hot-end components of aero-engines. Under working conditions, high-temperature oxidation and corrosion phenomena exist on the surface of the guide vanes, especially the internal cavity corrosion and oxidation of the blades, which have become a technical problem in engine design. In order to improve the reliability of the blade and prolong the service life of the blade, the surface of the inner and outer flow channels of the high guide vane adopts high temperature protection technology at the same time, that is, an aluminized layer with a depth of 0.02mm to 0.055mm is prepared on the surface of the outer flow channel of the high guide vane, and the inner cavity is prepared 0.01mm~0.035mm aluminized ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C23C16/12C23C16/02C22C19/07
Inventor 牛静张尊礼陈仲强刘艳张平
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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