Turbofan engine cowl assembly and method of operating the same

Details Turbofan engine cowl assembly and method of operating the same Turbofan engine cowl assembly and method of operating the same

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/08 (2006.01) F01D 17/10 (2006.01) F02C 9/16 (2006.01)

Patent

CA 2609291

An inner core cowl baffle assembly (100) for a turbofan engine assembly (10) including a core gas turbine engine (20), a core cowl (22) which circumscribes the core gas turbine engine, a nacelle (24) positioned radially outward from the core cowl, and a fan nozzle duct (26) defined between the core cowl and the nacelle. The inner core cowl baffle assembly includes a first core cowl baffle (101) coupled to a portion (19) of the core cowl within the fan nozzle duct, a second core cowl baffle (102) coupled to a portion (21) of the core cowl and positioned a distance radially inward from the first core cowl baffle, and an actuator assembly (110) configured to vary the throat area of the fan nozzle duct by selectively repositioning the second core cowl baffle with respect to the first core cowl baffle.

Affiliated with

Also associated with

Rating

Turbofan engine cowl assembly and method of operating the same does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbofan engine cowl assembly and method of operating the same, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbofan engine cowl assembly and method of operating the same will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1963642