Invention Grant
- Patent Title: Gas turbine engine thrust reverser system
- Patent Title (中): 燃气轮机反推系统
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Application No.: US13431356Application Date: 2012-03-27
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Publication No.: US09097209B2Publication Date: 2015-08-04
- Inventor: Michael N. Charron , James L. Lucas
- Applicant: Michael N. Charron , James L. Lucas
- Applicant Address: US CT Hartford
- Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee: UNITED TECHNOLOGIES CORPORATION
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F02K3/02
- IPC: F02K3/02 ; F02K1/72

Abstract:
A gas turbine engine thrust reverser system includes a fan nacelle having a fixed portion and a movable portion configured to move relative to the fixed portion between opened and closed positions in response to a command to selectively provide an opening between the fixed and movable portions. A fan case is arranged within the fan nacelle. The fan case includes an integral bull nose adjacent to the opening in the open position and to the movable portion in the closed position. The bull nose has a curved wall sloping radially outward.
Public/Granted literature
- US20130255225A1 GAS TURBINE ENGINE THRUST REVERSER SYSTEM Public/Granted day:2013-10-03
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