Invention Grant
- Patent Title: Exhaust nozzle control for a gas turbine engine
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Application No.: US14753637Application Date: 2015-06-29
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Publication No.: US09964069B2Publication Date: 2018-05-08
- Inventor: Gary D. Roberge
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02K1/00
- IPC: F02K1/00 ; F02K1/12 ; F02K1/15 ; F02K1/08 ; F02K1/42 ; F02K1/58 ; F02K1/76 ; F02K3/02

Abstract:
An exhaust nozzle for a gas turbine engine according to an example of the present disclosure includes, among other things, a duct having a first surface and a second surface extending about a duct axis to define an exhaust flow path, and at least one effector positioned along the first surface. The at least one effector is pivotable about an effector axis to vary a throat area of the exhaust flow path. The at least one effector tapers along the effector axis. A method of exhaust control for a gas turbine engine is also disclosed.
Public/Granted literature
- US20160377026A1 EXHAUST NOZZLE CONTROL FOR A GAS TURBINE ENGINE Public/Granted day:2016-12-29
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