Invention Grant
- Patent Title: Fan exhaust nozzle for turbofan engine
- Patent Title (中): 涡扇发动机风机排气喷嘴
-
Application No.: US11513707Application Date: 2006-08-31
-
Publication No.: US07900433B2Publication Date: 2011-03-08
- Inventor: John McCall
- Applicant: John McCall
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds PC
- Main IPC: F02K1/00
- IPC: F02K1/00 ; F02C3/00
Abstract:
The cross sectional flow area of a fan discharge nozzle on one side of a central plane of an associated gas turbine engine power plant is greater than the corresponding flow area of the fan discharge nozzle on an opposite side of the central plane to compensate for the blockage of fan airflow by a pylon.
Public/Granted literature
- US20080053061A1 Fan exhaust nozzle for turbofan engine Public/Granted day:2008-03-06
Information query
