发明名称 THRUST REVERSER FAN RAMP WITH NOISE SUPPRESSION
摘要 A fan ramp for use in a thrust reverser portion of a nacelle is disclosed. The nacelle is included in a propulsion system. The fan ramp extends circumferentially about an axial fan ramp centerline. The fan ramp includes a forward edge, an aft edge, and a noise suppression feature. The forward edge is disposed proximate an aft end of a fan case. The fan case at least partially surrounds a fan section of a gas turbine engine. The aft edge is disposed proximate a forward end of an array of cascades. The array of cascades is operable to permit a bypass airstream to pass there through during a thrust reversing operation. The noise suppression feature is operable to suppress noise within the propulsion system.
申请公布号 US2015108248(A1) 申请公布日期 2015.04.23
申请号 US201314060194 申请日期 2013.10.22
申请人 Rohr, Inc. 发明人 Aten Michael
分类号 F02K1/82;F02K1/62 主分类号 F02K1/82
代理机构 代理人
主权项 1. A fan ramp for use in a thrust reverser portion of a nacelle, the nacelle being included in a propulsion system, the fan ramp extending circumferentially about an axial fan ramp centerline, the fan ramp comprising: a forward edge disposed proximate an aft end of a fan case, the fan case at least partially surrounding a fan section of a gas turbine engine; an aft edge disposed proximate a forward end of an array of cascades, the array of cascades being operable to permit a bypass airstream to pass there through during a thrust reversing operation; and a noise suppression feature operable to suppress noise within the propulsion system.
地址 Chula Vista CA US
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