Method of Cleaning Turbine Blades

US2016101446A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016101446-A1
Application numberUS-201414511749-A
CountryUS
Kind codeA1
Filing dateOct 10, 2014
Priority dateOct 10, 2014
Publication dateApr 14, 2016
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

In a process for cleaning contaminating silicon dioxide SiO 2 off of turbine blades, silicon dioxide that is on the turbine blades is reduced selectively in a vacuum process that takes place in dry conditions and at elevated temperature inside a high vacuum furnace, by feeding gas having a reducing action, consisting of hydrogen gas or carbon monoxide, is introduced into the high vacuum furnace. The temperature inside the high vacuum furnace is at least about 1000 degrees Celsius, and the residence time of the turbine blades in the high vacuum furnace is determined with reference to the diminishment of the SiO concentration, as analysed with a mass spectrometer. The electrically heatable high vacuum furnace is evacuable by means of a vacuum system that consists of a backing pump and a turbomolecular pump with an adjustable throttle valve and a water-cooled baffle. Further, the gas with reducing action is fed into the furnace via a precision high vacuum regulating valve, and it is equipped with a mass spectrometer.

First claim

Opening claim text (preview).

1 . Process for cleaning contaminating silicon dioxide, SiO 2 , off of turbine blades, said process being carried out in a dry vacuum process that takes place at elevated temperature inside a high vacuum furnace, and in which at least some of the silicon dioxide on the turbine blades that are to be cleaned is removed by means of a gas with reducing action, characterised in that the silicon dioxide, SiO 2 , to be removed is reduced selectively to the silicon monoxide stage SiO by the gas with reductive action consisting of hydrogen gas H 2 or carbon monoxide CO, which contains a minimum quantity of H 2 O or CO 2 respectively, is then vaporised in a vacuum and pumped out in gas form, wherein the residence time of the turbine blades ( 2 ) in the high vacuum furnace ( 1 ) is selected until the time when the SiO concentration falls significantly. 2 . Process according to claim 1 , characterised in that the gas with reductive action consists of hydrogen gas, H 2 , which contains a minimum quantity of H 2 O with oxidising effect and is monitored for the maximum permitted concentration value of these reaction products by checking the gas flow rate by means of mass spectrometer analysis. 3 . Process according to claim 1 , characterised in that the gas with reductive action consists of carbon monoxide, CO, which contains a minimum quantity of CO 2 with oxidising effect and is monitored for the maximum permitted concentration value of these reaction products by checking the gas flow rate by means of mass spectrometer analysis. 4 . Process according to claim 1 , characterised in that the temperature in the high vacuum furnace ( 1 ) is at least 1000 degrees Celsius. 5 . Process according to claim 1 , characterised in that the residence time of the turbine blades ( 2 ) in the high vacuum furnace ( 1 ) is selected at least until the time when the SiO concentration ( 44 ) falls significantly (mass spectrometer). 6 . Device for performing the process according to claim 1 , characterised by a high vacuum furnace ( 1 ), in which the turbine blades ( 2 ) to be cleaned may be placed, and which is evacuable via a vacuum system ( 3 - 6 ), and into which the gas with reducing action can be introduced via a gas inlet system ( 7 ). 7 . Device according to claim 6 , characterised in that the vacuum system consists of a backing pump ( 3 ) and a turbomolecular pump ( 4 ) with an adjustable throttle valve ( 5 ) and a water-cooled baffle ( 6 ). 8 . Device according to claim 6 , characterised in that the gas inlet system consists of a precision high vacuum regulating valve ( 7 ). 9 . Device according to claim 6 , characterised in that the high vacuum furnace ( 1 ) is equipped with a mass spectrometer ( 8 ). 10 . Device according to claim 6 , characterised in that the high vacuum furnace ( 1 ) can be heated electrically.

Assignees

Inventors

Classifications

  • Repairing turbine components, e.g. moving or stationary blades, rotors, (B23P6/045 takes precedence) · CPC title

  • C23G5/00Primary

    Cleaning or de-greasing metallic material by other methods; Apparatus for cleaning or de-greasing metallic material with organic solvents · CPC title

  • Repairing methods or devices · CPC title

  • B08B7/04Primary

    by a combination of operations · CPC title

  • by heating (B08B7/0035 takes precedence) · CPC title

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What does patent US2016101446A1 cover?
In a process for cleaning contaminating silicon dioxide SiO 2 off of turbine blades, silicon dioxide that is on the turbine blades is reduced selectively in a vacuum process that takes place in dry conditions and at elevated temperature inside a high vacuum furnace, by feeding gas having a reducing action, consisting of hydrogen gas or carbon monoxide, is introduced into the high vacuum furnac…
Who is the assignee on this patent?
Airbus Ds Gmbh
What technology area does this patent fall under?
Primary CPC classification C23G5/00. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Thu Apr 14 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).