CPC C11D 3/2086 (2013.01) [B08B 3/08 (2013.01); C11D 1/83 (2013.01); C11D 1/94 (2013.01); C11D 3/2075 (2013.01); C11D 3/30 (2013.01); C11D 3/3409 (2013.01); C23G 1/02 (2013.01); C23G 1/061 (2013.01); C23G 1/088 (2013.01); F01D 25/002 (2013.01); C11D 1/72 (2013.01); C11D 1/88 (2013.01); C11D 2111/20 (2024.01); Y02T 50/60 (2013.01)] | 20 Claims |
1. A cleaning solution for an in-situ aircraft turbine engine, the cleaning solution comprising:
at least a first organic acidic component within a range between about 0.1 percent and about 15 percent of the cleaning solution;
isopropylamine sulphonate within a range between about 0.07 percent and 0.14 weight percent of the cleaning solution;
alcohol ethoxylate within a range between about 0.035 percent and 0.07 weight percent of the cleaning solution;
0.3 weight percent monosodium-N-lauryl-B-iminodipropionic acid; and
an organic base that was added by weight to tritate the cleaning solution to a pH within a range of 2.5 to 7.0.
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