An engine inlet assembly includes an inlet duct having a first inlet duct leg and a second inlet duct leg, the first inlet duct leg and the second inlet duct leg extending toward a common inlet duct outlet located at an engine inlet. The first inlet duct leg and the second inlet duct leg are fixedly secured to an airframe of an aircraft at an air inlet. The duct outlet has a floating interface with the engine inlet.
申请公布号
WO2015160679(A1)
申请公布日期
2015.10.22
申请号
WO2015US25507
申请日期
2015.04.13
申请人
SIKORSKY AIRCRAFT CORPORATION
发明人
BOFILL, STEVEN;CHASEN, SCOTT A.;SIMONETTI, JOSEPH LAWRENCE;LAMB, DONALD WILLIAM, JR.