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.
申请公布号
WO9618851(A1)
申请公布日期
1996.06.20
申请号
WO1995US15095
申请日期
1995.11.17
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
JOHNSON, THOMAS, E.;MADDEN, THOMAS, J.;SODERQUIST, ROBERT, W.
