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CAN-ANNULAR GAS TURBINE ENGINE COMBUSTOR ARRANGEMENT HAVING TANGENTIALLY ORIENTED COMBUSTOR CANS WITH RADIAL MIDFRAME BAFFLES
CAN-ANNULAR GAS TURBINE ENGINE COMBUSTOR ARRANGEMENT HAVING TANGENTIALLY ORIENTED COMBUSTOR CANS WITH RADIAL MIDFRAME BAFFLES
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机译:带有径向中间框的切向定向燃烧室罐的环形燃气轮机发动机燃烧室布置
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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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