Segmented bulkhead liner for a gas turbine combustor

Details Segmented bulkhead liner for a gas turbine combustor Segmented bulkhead liner for a gas turbine combustor

1994-12-15

1996-06-11

Thorpe, Timothy S.

Power plants

Combustion products used as motive fluid

Combustion products generator

60752, F02C 100

Patent

active

055244386

ABSTRACT:
Truncated pie shaped bulkhead liner sections 60 are each divided into two liner segments 62. The division occurs adjacent fuel nozzle opening 20. Upstream extending lips 71, 75 and 77 abut the bulkhead 14. Cooling air passes through cooling flow openings in the bulkhead with all the flow continuing toward the shell 38, 40 edges of the liner segments.

REFERENCES:
patent: 4414816 (1983-11-01), Craig et al.
patent: 4870818 (1989-10-01), Suliga
patent: 4914918 (1990-04-01), Sullivan

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