Fluid injector for cooling a gas turbine engine component
US10480533B2 · kind B2 · utility
0Cited by
11References
4Claims
0Family size
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Key dates
| Filing date | Sep 8, 2014 |
| Grant date | Nov 19, 2019 |
| Priority date | — |
| Expiry date | Mar 4, 2036 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF05D2260/213
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
An example method of cooling a compressor of a gas turbine includes, among other things, diverting a flow from a compressor, and directing the flow at the compressor in a direction, the direction having a circumferential component and an axial component.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.