Method For In-Situ Cleaning Of Compressor Blades In A Gas Turbine Engine On An Aircraft And Compositions

• US 20140144473A1
• Filed: 01/29/2014
• Published: 05/29/2014
• Est. Priority Date: 07/29/2011
• Status: Abandoned Application

• Current Assignee: Formatex (Offshore) S.A.L.
• Original Assignee: Formatex (Offshore) S.A.L.
• Inventors: MARTIN, David William
• Application Number:
  US14/167,547
• Publication Number:
  US 20140144473A1
• Time in Patent Office: Days
• US Class Current: 134/26
• CPC Class Codes: C11D 2111/44 Multi-step processes
• CPC Class Codes: C11D 3/2041 Dihydric alcohols
• CPC Class Codes: C11D 3/43 Solvents
• CPC Class Codes: F01D 25/002 Cleaning of turbomachines
• CPC Class Codes: F04D 29/324 Blades
• CPC Class Codes: F04D 29/705 Adding liquids

Abstract

A method for in-situ cleaning of compressor blades in a gas turbine engine on an aircraft comprises the following sequential steps:

• • Step 1—washing said compressor blades by spraying a first liquid composition into the engine; and
  • Step 2—finally rinsing said washed compressor blades by spraying a second liquid composition into the engine,
    wherein the second liquid composition, has a freezing point of −10° C. or below and is non-aqueous and hydrophilic.

Claims

1. A method for in-situ cleaning of compressor blades in a gas turbine engine on an aircraft, said method comprising the following sequential steps:

Step 1—

washing said compressor blades by spraying a first liquid composition into the engine; and

Step 2—

as a final step in which any liquid composition is sprayed into the engine, rinsing said washed compressor blades by spraying a second liquid composition into the engine;

characterised in that said second liquid composition has a freezing point of −

10°

C. or below and is non-aqueous and hydrophilic; and

said first liquid composition is the same as or different from said second liquid composition.

3. The method according to claim 1, wherein said first liquid composition is aqueous.

4. The method according to claim 1, wherein said first liquid composition comprises the second liquid composition and water in a weight ratio of 1:

1-5, more preferably 1;

3-4.5, most preferably 1;

4.

6. The method according to claim 1, wherein said second liquid composition comprises:

a) one or more organic solvents chosen from methylene glycol, dimethylene glycol, trimethylene glycol, ethylene glycol, propylene glycol, dipropylene glycol and butyl glycol; and

/or

b) one or more surfactants chosen from alcohol ethoxylates, phenol alkoxylates, poly(oxyalkylene) glycols, poly(oxyalkylene) fatty acid esters, amine alkoxylates, poly(alkyl) succinimides, poly(alkenyl) succinimides, fatty acid esters of sorbitol and glycerol, fatty acid salts, sorbitan esters, poly(oxyalkylene) sorbitan esters, fatty amine alkoxylates, poly(oxyalkylene) glycol esters, fatty acid amides, fatty acid amide alkoxylates, fatty amines, EO/PO substituted siloxane, quaternary amines, alkyloxazolines, alkenyloxazolines, imidazolines, alkyl-sulphonates, alkylarylsulphonates, alkylsulfosuccinates, alkyl-phosphates, alkenylphosphates, and phosphates esters.

7. The method according to claim 6, wherein said organic solvent is trimethylene glycol.

8. The method according to claim 6, wherein said surfactant is one or more of polyisobutylenesuccinimide, oleic diethanolamide, EO/PO substituted siloxane and sorbitan ester, preferably sorbitan mono-oleate.

9. The method according to claim 6, wherein said second liquid composition also comprises one or more of silicone oil, preferably of viscosity<

50 cSt, synthetic oil, odourless kerosene and corrosion inhibitors, preferably triethanolamine.

10. The method according to claim 1, wherein the second liquid composition contains trimethylene glycol, Sorbitan mono-oleate, triethanolamine, silicone oil, synthetic oil and odourless kerosene.

12. A non-aqueous composition intended for use as the second liquid composition used in Step 2 of the method claimed in claim 1, said composition comprising:

a) 75-95 wt % of one or more organic solvents chosen from methylene glycol, dimethylene glycol and trimethylene glycol; and

b) at least 5 wt % of one or more surfactants, wherein the surfactants are chosen from alcohol ethoxylates, phenol alkoxylates, poly(oxyalkylene) glycols, poly(oxyalkylene) fatty acid esters, amine alkoxylates, poly(alkyl) succinimides, poly(alkenyl) succinimides, fatty acid esters of sorbitol and glycerol, fatty acid salts, sorbitan esters, poly(oxyalkylene) sorbitan esters, fatty amine alkoxylates, poly(oxyalkylene) glycol esters, fatty acid amides, fatty acid amide alkoxylates, fatty amines, EO/PO substituted siloxane, quaternary amines, alkyloxazolines, alkenyloxazolines, imidazolines, alkyl-sulphonates, alkylarylsulphonates, alkylsulfosuccinates, alkyl-phosphates, alkenylphosphates, and phosphates esters.

13. Use of a non-aqueous composition as claimed in claim 12, in a method for in-situ cleaning of compressor blades in a gas turbine engine on an aircraft, wherein said use is for preventing ice formation in the engine by absorbing residual water and maintaining it in the liquid state to temperatures below −

10°

C.

17. The method according to claim 7, wherein said surfactant is one or more of polyisobutylenesuccinimide, oleic diethanolamide, EO/PO substituted siloxane and sorbitan ester, preferably sorbitan mono-oleate.

2. A method for in-situ cleaning of compressor blades in a plurality of gas turbine engines on one or more aircraft, said method comprising the following sequential steps:

Step 1—

washing the compressor blades in a first gas turbine engine on an aircraft by spraying a first liquid composition into said engine and draining at least a portion of the used first liquid composition into a collecting tank;

Step 2—

as a final step in which any liquid composition is sprayed into said first gas turbine engine, rinsing said washed compressor blades in said first gas turbine engine by spraying a second liquid composition into said first engine, draining at least a portion of the used second liquid composition into said collecting tank and mixing said used second liquid composition with said first liquid composition in said collecting tank;

Step 3—

washing the compressor blades in a second gas turbine engine by spraying a liquid composition derived form said collecting tank into said second engine and draining at least a portion of said used liquid composition derived from said collecting tank back into said collecting tank; and

Step 4—

as a final step in which any liquid composition is sprayed into said second gas turbine engine, rinsing said washed compressor blades in said second gas turbine engine by spraying said second liquid composition into the engine, draining at least a portion of the used second liquid composition into said collecting tank and mixing said used second liquid composition with any liquid composition in said collecting tank; and

optionally repeating Step 3 and Step 4 as required to clean the compressor blades of subsequent gas turbine engine(s);

wherein said second liquid composition has a freezing point of −

10°

C. or below and is non-aqueous and hydrophilic; and

wherein said first liquid composition is the same as or different from said second liquid composition.

5. The method according to claim 2, wherein the liquid composition derived form said collecting tank comprises the second liquid composition and water in a weight ratio of 1:

1-5, more preferably 1;

3-4.5, most preferably 1;

4.

11. The method according to claim 2, wherein the gas turbine engines are on a plurality of aircraft.

14. The method according to claim 2, wherein said first liquid composition is aqueous.

15. The method according to claim 2, wherein said first liquid composition comprises the second liquid composition and water in a weight ratio of 1:

1-5, more preferably 1;

3-4.5, most preferably 1;

4.

16. The method according to claim 2, wherein said second liquid composition comprises:

a) one or more organic solvents chosen from methylene glycol, dimethylene glycol, trimethylene glycol, ethylene glycol, propylene glycol, dipropylene glycol and butyl glycol; and

/or

b) one or more surfactants chosen from alcohol ethoxylates, phenol alkoxylates, poly(oxyalkylene) glycols, poly(oxyalkylene) fatty acid esters, amine alkoxylates, poly(alkyl) succinimides, poly(alkenyl) succinimides, fatty acid esters of sorbitol and glycerol, fatty acid salts, sorbitan esters, poly(oxyalkylene) sorbitan esters, fatty amine alkoxylates, poly(oxyalkylene) glycol esters, fatty acid amides, fatty acid amide alkoxylates, fatty amines, EO/PO substituted siloxane, quaternary amines, alkyloxazolines, alkenyloxazolines, imidazolines, alkyl-sulphonates, alkylarylsulphonates, alkylsulfosuccinates, alkyl-phosphates, alkenylphosphates, and phosphates esters.

18. The method according to claim 2, wherein the second liquid composition contains trimethylene glycol, Sorbitan mono-oleate, triethanolamine, silicone oil, synthetic oil and odourless kerosene.