Gas turbine offline compressor wash with buffer air from combustor
US9631512B2 · kind B2 · utility
9Cited by
12References
15Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jan 31, 2013 |
| Grant date | Apr 25, 2017 |
| Priority date | — |
| Expiry date | Feb 27, 2036 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C6/08
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A system and method for washing a gas turbine engine. The method for washing the gas turbine engine includes coupling a pressurized air supply assembly to an air supply and to a secondary air system, cranking a compressor rotor assembly of the gas turbine engine, supplying pressurized offline buffer air from the air supply to the pressurized air supply assembly, and spraying a cleaner into the compressor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.