Gas turbine engine bleed scoops
This invention relates generally to gas turbine engines, and more specifically to bleed scoops used in gas turbine engine high-pressure compressors. A gas turbine engine includes a compressor including a casing and a stator assembly. The casing extends around the stator assembly, the stator assembly...
Saved in:
Main Authors | , , , , , , , |
---|---|
Format | Patent |
Language | English |
Published |
22.04.2003
|
Online Access | Get full text |
Cover
Loading…
Summary: | This invention relates generally to gas turbine engines, and more specifically to bleed scoops used in gas turbine engine high-pressure compressors.
A gas turbine engine includes a compressor including a casing and a stator assembly. The casing extends around the stator assembly, the stator assembly including a plurality of stator vanes, and a plurality of bleed scoops. Adjacent stator vanes define a static high-pressure region, the bleed scoops formed at least partially within the high pressure region. |
---|