Invention Grant
- Patent Title: Reverse flow gas turbine engine airflow bypass
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Application No.: US14190144Application Date: 2014-02-26
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Publication No.: US09726112B2Publication Date: 2017-08-08
- Inventor: Gabriel L. Suciu , Brian D. Merry
- Applicant: United Technologies Corporation
- 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: F02K3/06
- IPC: F02K3/06
Abstract:
A gas turbine engine has a propulsor including a fan and a power turbine, an engine core aerodynamically connected to the propulsor by a transition duct, and a bypass valve in the transition duct that allows for air from the engine core to bypass the power turbine.
Public/Granted literature
- US20140250862A1 REVERSE FLOW GAS TURBINE ENGINE AIRFLOW BYPASS Public/Granted day:2014-09-11
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