Chemise refroidie d'une tuyère pour turbine à gaz

N° de brevet: EP1882822 (A2)
Date de publication: 2008-01-30
Inventeur(s): LAVIN JEFFREY R [US];MURPHY MICHAEL J [US];
Demandeur(s): UNITED TECHNOLOGIES CORP [US];
Classification: F01D11/00;F01D25/12;F01D25/30;F02K1/82;
N° de demande: EP20070252042 20070518 
Numéro(s) de priorité: US20060491891 20060724 
An exhaust liner assembly (24) including an interface (30) between moveable parts (50, 52) includes a seal liner (35) having a plurality of slots (42). The size of each slot (42) varies with the circumferential position of the liner assembly (24) to provide a stable cavity pressure within the interface (30) to create a stable barrier about the entire circumference of the exhaust liner assembly (24).

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