F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 1/00 (2006.01) F23D 14/48 (2006.01)
Patent
CA 2451481
A wear reduction means for a fuel nozzle interface of an industrial gas turbine combustor (10) is disclosed. The wear reduction means includes a replaceable insert (47) welded into to the engagement location (45) of the fuel nozzle tip (44). The fuel nozzle tip is coated (48) with a material harder than the replaceable insert, such that any wear due to mechanical contact of the mating components is directed to the replaceable insert.
L'invention concerne une unité de réduction d'usure destinée à une zone d'interface de l'injecteur de carburant d'une chambre à combustion (10) d'une turbine à gaz industrielle. Cette unité de réduction d'usure comprend une pièce rapportée remplaçable (47) soudée dans une zone de logement (45) destinée à la buse (44) de l'injecteur de carburant. Cette buse d'injecteur de carburant est revêtue (48) d'une matière plus dure que la pièce rapportée remplaçable de façon que l'usure due à un contact mécanique des composants accouplés ne se produise que sur la pièce rapportée remplaçable.
Biondo Charles
Hoegler Frank
Biondo Charles
Gowling Lafleur Henderson Llp
Hoegler Frank
Power Systems Mfg. Llc
LandOfFree
Means for wear reduction in a gas turbine combustor does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Means for wear reduction in a gas turbine combustor, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Means for wear reduction in a gas turbine combustor will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1445534