20250179965. Gas Turbine Engine Bl (General Electric)
GAS TURBINE ENGINE BLEED SYSTEMS INCLUDING BLEED DISCHARGE EXHAUST DEVICES
Abstract: gas turbine engine bleed systems including bleed discharge exhaust devices are disclosed. an apparatus comprising an exhaust device disposed in a bifurcation of a gas turbine engine, the bifurcation disposed in a bypass airflow passage of the gas turbine engine, and a bleed flow conduit including a first end coupled to a bleed slot of the gas turbine engine, and a second end coupled to the exhaust device.
Inventor(s): Brandon W. Miller, Stephen G. Matava, Egbert Geertsema, John C. Glessner, John R. Holland, Steven Douglas Johnson, Ryan T. Roehm
CPC Classification: F02C9/18 (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines ; jet-propulsion plants ; construction of compressors or fans ; generating combustion products of high pressure or high velocity ; using gas turbines in compression refrigeration plants ))
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- Patent Applications
- General Electric Company
- CPC F02C9/18
- Brandon W. Miller of West Chester OH US
- Stephen G. Matava of Andover MA US
- Egbert Geertsema of Cincinnati OH US
- John C. Glessner of Kings Mills OH US
- John R. Holland of West Chester OH US
- Steven Douglas Johnson of Milford OH US
- Ryan T. Roehm of West Chester OH US