Nozzle flap cooling air supply system

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/18 (2006.01) F02K 1/12 (2006.01) F02K 1/78 (2006.01) F02K 1/82 (2006.01)

Patent

CA 2492149

The device of the invention for supplying cooling air to a flap of an exhaust nozzle (21) in a gas turbine (1), comprises a tube (30) connecting the flap (21) to a cooling air source (31). The tube comprises (30) at least one telescopic portion (32) and one ball-joint connection (33, 34).

Le dispositif de l'invention, d'alimentation, en air de refroidissement, d'un volet (21) de tuyère d'éjection (1) d'une turbomachine, comprend une canalisation (30) reliant le volet (21) à une source d'air de refroidissement (31). La canalisation (30) comprend au moins une portion télescopique (32) et une liaison rotule (33,34).

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