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RADIAL MIDFRAME BAFFLE FOR CAN-ANNULAR COMBUSTOR ARRANGEMENT HAVING TANGENTIALLY ORIENTED COMBUSTOR CANS
RADIAL MIDFRAME BAFFLE FOR CAN-ANNULAR COMBUSTOR ARRANGEMENT HAVING TANGENTIALLY ORIENTED COMBUSTOR CANS
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机译:具有切向定向燃烧室罐的环形燃烧室布置的径向中间框架
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摘要
A can-annular gas turbine engine combustion arrangement (10), including: a combustor can (12) comprising a combustor inlet (38) and a combustor outlet circumferentially and axially offset from the combustor inlet; an outer casing (24) defining a plenum (22) in which the combustor can is disposed; and baffles (70) configured to divide the plenum into radial sectors (72) and configured to inhibit circumferential motion of compressed air (16) within the plenum.
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