Gas turbine engine nozzle apparatus including a nozzle flap...

Details Gas turbine engine nozzle apparatus including a nozzle flap... Gas turbine engine nozzle apparatus including a nozzle flap...

F - Mech Eng,Light,Heat,Weapons

02

K

60/99

F02K 1/12 (2006.01)

Patent

CA 1083364

GAS TURBINE ENGINE NOZZLE APPARATUS INCLUDING A NOZZLE FLAP SLOT SEAL ABSTRACT Apparatus for modulating the area of a gas turbine engine nozzle which provides for positive sealing between overlapping articulated flaps when the overlapped flap is axially slotted to receive a portion of the overlapping flap. An arcuate seal is attached to the overlapping flap by means of a floating connection, the overlapping flap dragging the seal therewith in the axial direction. A seat is mounted on either side of the slot to slidingly receive a pair of shoulders laterally extending from the seal. A portion of the seal is received within the slot and is so contoured as to partially define the nozzle flow path. A sleeve captures and supports the seal shoulders during their axial travel.

285931

Affiliated with

Also associated with

Rating

Gas turbine engine nozzle apparatus including a nozzle flap... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Gas turbine engine nozzle apparatus including a nozzle flap..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Gas turbine engine nozzle apparatus including a nozzle flap... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-650605