Composition for cleaning a gas turbine engine

• US 4,834,912 A
• Filed: 08/03/1987
• Issued: 05/30/1989
• Est. Priority Date: 02/13/1986
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Cellich, William A., Hodgens, Henry M. II
• Primary Examiner(s): Pal, Asok
• Application Number:
  US07/081,084
• Time in Patent Office: 666 Days
• Field of Search: 252/544, 252/545, 252/546, 252/548, 252/79.4, 252/156, 134/2
• US Class Current: 510/186
• CPC Class Codes: B08B 3/02 Cleaning by the force of jets or sprays
• CPC Class Codes: B08B 9/00 Cleaning hollow articles by methods or apparatus specially adapted thereto B08B6/00 takes precedence
• CPC Class Codes: C23G 1/14 with alkaline solutions
• CPC Class Codes: C23G 1/24 with neutral solutions
• CPC Class Codes: F01D 25/002 Cleaning of turbomachines
• CPC Class Codes: F02B 77/04 Cleaning of, preventing corrosion or erosion in, or preventing unwanted deposits in, combustion engines cleaning of fuel injection apparatus F02M65/00

Abstract

A composition and method for removing deposits (10) from the internal components (24) of a gas turbine engine (18) utilizing a cleaning composition (15) which comprises an aqueous solution of hydroxylamine sulfate, a chelating agent, a compound selected from the group consisting of ammonium sulfamate, ammonium sulfamide, and hydroxylamine-o-sulfonic acid, and, an alkaline pH modifying substance added in an amount sufficient to achieve a pH value of between 6.5 and 14. The method involves contacting the deposits with the cleaning composition, such as in an apply and soak type pattern, chemically dislodging the deposits from the component surfaces. The engine is rinsed to remove the dislodged deposits and residual cleaning composition.

Claims

1. A cleaning composition for chemically dislodging deposits from the internal components of a gas turbine engine, while preserving the alloys or coatings used therein, said composition comprising:

an aqueous solution of 0.1-2.0 molar hydroxylamine sulfate, a chelating agent, 0.1-4.0 molar concentration of a compound selected from the group consisting of ammonium sulfamate, sulfamide, and hydroxylamine-o-sulfonic acid, and, an alkaline pH modifying substance added in an amount sufficient to achieve a pH value of from 6.5 to 14.

2. The composition of claim 1 wherein said pH modifying substance is ammonium hydroxide.

3. The composition of claim 1 additionally comprising up to 2.0 molar ethylenediamine.

4. A cleaning composition for chemically dislodging deposits from the internal components of a gas turbine engine, while preserving the alloys or coatings used therein, said composition comprising an aqueous solution of 0.4 molar hydroxylamine sulfate, 0.4 molar ethylenediamine, 0.7 molar ammonium sulfamate, and 0.8 molar N-hydroxyethlethyenediaminetriacetic acid with ammonium hydroxide added in an amount sufficient to achieve a pH value of between 7 and 8.5.

5. A cleaning composition for chemically dislodging deposits from the internal components of a gas turbine engine, while preserving the alloys or coatings used therein, the composition comprising an admixture of:

a first solution comprising an aqueous solution of hydroxylamine sulfate and water, having a pH of less than 4; and

,

a second solution comprising a chelating agent, a compound selected from the group consisting essentially of ammonium sulfate, sulfamide and hydroxylamine-o-sulfonic acid, and, an alkaline pH modifying substance added in an amount sufficient to achieve a pH of between 9 and 14.