Reduced cost dry low nox combustor cap primary assembly

F - Mech Eng,Light,Heat,Weapons – 01 – D

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Details

F01D 25/00 (2006.01) F02C 3/00 (2006.01) F23R 3/10 (2006.01) F23R 3/34 (2006.01) F23R 3/50 (2006.01)

Patent

CA 2092947

51DV04050 ABSTRACT OF THE DISCLOSURE A combustor cap assembly for a gas turbine includes an outer sleeve (12); an impingement plate (14) fixed to a forward end of the outer sleeve. The impingement plate is provided with a plurality of primary fuel nozzle openings (18) and a single secondary fuel nozzle opening (20). A plurality of open-ended nozzle cups (28) are fixed to the impingement plate (14) in alignment with respective primary fuel nozzle openings (18); and a nozzle collar (32) is fixed to a rearward end of each nozzle cup (28).

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