Methods and apparatus to reduce turbine engine nozzle...

Details Methods and apparatus to reduce turbine engine nozzle... Methods and apparatus to reduce turbine engine nozzle...

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/78 (2006.01) F02C 7/20 (2006.01) F02K 1/12 (2006.01) F02K 1/82 (2006.01)

Patent

CA 2478202

An assembly (100) for a gas turbine engine exhaust nozzle (30) includes a backbone (104) and a basesheet (106) configured to couple to the backbone. The basesheet includes at least one relief cut (200) and a pair of circumferentially-spaced sides (114 and 116) coupled together by an upstream side (110) and a downstream side (112). The at least one relief cut extends from at least one of the circumferentially- spaced sides towards the other respective circumferentially-spaced side.

Dispositif (100) pour la tuyère d'éjection d'une turbine à gaz (30) comprenant une épine dorsale (104) et une tôle (106) configurée pour être raccordée à l'épine dorsale. La tôle comprend au moins une rainure (200) et une paire de côtés (114 et 116) espacés sur la circonférence, reliés ensemble par un côté en amont (110) et un côté en aval (112). Au moins une rainure s'étend d'au moins un des côtés espacés sur la circonférence vers l'autre côté espacé sur la circonférence.

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