Invention Grant
- Patent Title: Dual function cascade integrated variable area fan nozzle and thrust reverser
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Application No.: US15674576Application Date: 2017-08-11
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Publication No.: US10677192B2Publication Date: 2020-06-09
- Inventor: Richard M. Marshall
- Applicant: United 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: F02K1/09
- IPC: F02K1/09 ; F02K1/42 ; F02K1/72
Abstract:
A gas turbine engine system according to an exemplary aspect of the present disclosure may include a fan nacelle that extends circumferentially about a fan, and at least one integrated mechanism coupled to the fan nacelle. The at least one integrated mechanism includes a variable fan nozzle and a thrust reverser, with the thrust reverser and the variable fan nozzle having a common part.
Public/Granted literature
- US20170356387A1 DUAL FUNCTION CASCADE INTEGRATED VARIABLE AREA FAN NOZZLE AND THRUST REVERSER Public/Granted day:2017-12-14
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