Gas turbine engine bleed control system
US4815285A · kind A · utility
6Cited by
6References
6Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Mar 9, 1987 |
| Grant date | Mar 28, 1989 |
| Priority date | — |
| Expiry date | Mar 9, 2007 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF02C6/08
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Apparatus for controlling bleed gas in the bleed gas system of a compressor for gas turbine engine wherein a valve disposed in the bleed conduit of a compressor is moved from closed to open position in a selectively controlled manner in accordance with a preselected bleed gas pressure sensed in the bleed gas system of the compressor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.