发明名称 BLOW-OFF DEVICE FOR A BYPASS GAS TURBINE ENGINE
摘要 A blow-off device for a gas turbine bypass engine having a primary air flow path separated from an outer secondary air flow path by a partition includes a plurality of discharge passages passing through the partition from the primary air flow path to the secondary air flow path, each of the discharge passages having a first hinged flap in the outer wall of the primary air flow path, a second hinged flap in the inner wall of the secondary air flow path, and a connecting rod mechanically interlinking the first and second flaps, the connecting rod being hinged at one of its end to the first flap and at its other end to the second flap.
申请公布号 US5119625(A) 申请公布日期 1992.06.09
申请号 US19900545643 申请日期 1990.06.29
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTORS D'AVIATION "S.N.E.M.C.A." 发明人 GLOWACKI, PIERRE A.
分类号 F04D27/02 主分类号 F04D27/02
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