<p>A reverse flow combustor for a gas turbine engine having an outer combustor liner and an inner combustor liner defining an annular combustion chamber,and a compound-angle frustoconical portion in the outer liner having a first and second conical slopes towards an engine centreline..</p>
申请公布号
CA2572044(C)
申请公布日期
2015.04.28
申请号
CA20062572044
申请日期
2006.12.22
申请人
PRATT & WHITNEY CANADA CORP.
发明人
RUDRAPATNA, NAGARAJA;MORENKO, OLEG;PATEL, BHAWAN B.
