Invention Grant
- Patent Title: Auxiliary propulsor for a variable cycle gas turbine engine
- Patent Title (中): 用于可变循环燃气涡轮发动机的辅助推进器
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Application No.: US12072353Application Date: 2008-02-26
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Publication No.: US08127528B2Publication Date: 2012-03-06
- Inventor: Gary D. Roberge
- Applicant: Gary D. Roberge
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Kinney & Lange, P.A.
- Main IPC: F02K3/02
- IPC: F02K3/02

Abstract:
A core engine of a variable cycle gas turbine engine includes a low pressure spool for generating streams of bypass air and pressurized air, and a high pressure spool for further pressurizing the stream of pressurized air to generate streams of combustion air and supercharged auxiliary air. A peripheral case surrounds the engine case to form a peripheral duct. An auxiliary combustor and propulsor are positioned within the peripheral duct. A bleed duct extends from the high pressure spool to the auxiliary combustor. Variable ductwork directs airflow through the bleed duct and peripheral duct in two modes. A first mode comprises directing the stream of auxiliary air to the auxiliary combustor, and directing stream of inlet air through the peripheral duct. A second mode comprises directing the stream of auxiliary air into the stream of bypass air, and preventing inlet air from entering the peripheral duct.
Public/Granted literature
- US20090211221A1 Auxiliary propulsor for a variable cycle gas turbine engine Public/Granted day:2009-08-27
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