Invention Grant
- Patent Title: Gas turbine engine bifurcation located fan variable area nozzle
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Application No.: US15889304Application Date: 2018-02-06
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Publication No.: US10989143B2Publication Date: 2021-04-27
- Inventor: Constantine Baltas
- Applicant: RAYTHEON TECHNOLOGIES CORPORATION
- Applicant Address: US CT Farmington
- Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee: RAYTHEON TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02K1/06
- IPC: F02K1/06 ; F02K1/15 ; F02K3/06 ; F02K1/12 ; F02K3/075 ; F02C3/107
Abstract:
A gas turbine engine includes a core engine defined about an axis, a gear system driven by the core engine, and a pylon variable area flow system. A fan is driven by the gear system. The variable area flow system operates to effect the bypass flow.
Public/Granted literature
- US20180274483A1 GAS TURBINE ENGINE BIFURCATION LOCATED FAN VARIABLE AREA NOZZLE Public/Granted day:2018-09-27
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