F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
60/113, 60/170
F02C 3/00 (2006.01)
Patent
CA 1112059
BURNER NOZZLE ASSEMBLY FOR GAS TURBINE ENGINE ABSTRACT OF THE DISCLOSURE An axial flow gas turbine engine has a combustion section with a number of nozzle assemblies for injecting fluent materials, such as fuel, combustion enhancers, or pollutant redu- cers, into a burner can which is supplied with air from the combus- tion section plenum. The nozzle assemblies are carried by a wall separating the plenum from the outside of the engine and extend from the wall to associated openings in the burner can. The nozzle head and an associated feeder tube is easily removable from the remainder of each nozzel assembly for cleaning, repair or replace- ment of the nozzel head, or for other purposes. The nozzle assem- blies and their supply manifolds are further arranged so that a central liner of the burner can may be removed through the wall without disturbing the nozzle assemblies or the supply manifolds. Also, the wall is provided by a member removably attached to the engine case or frame and supporting the nozzle assemblies and the burner can liner, so that by a more complete procedure all of the nozzle assemblies, and the burner can liner, may be entirely removed from the engine, if desired.
321502
Denegris Michael A.
Lees Philip
Swabey Ogilvy Renault
United Technologies Corporation
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