发明名称 Controlled bypass inlet duct
摘要 A separating inlet duct (14) is provided with a reduced arm, bypass throat section (46) to restrict the bypass flow (18b) during periods of high speed aircraft flight. An ejector (34) ensures a minimum bypass flow (18b) during hover or low speed flight. An icing resistance baffle (40) having a rounded leading edge (42) defines the sized throat section (46).
申请公布号 US4972672(A) 申请公布日期 1990.11.27
申请号 US19890413660 申请日期 1989.09.28
申请人 PRATT & WHITNEY CANADA, INC. 发明人 SANDERSON, JOHN J.;BANKS, IVOR
分类号 F02C7/052 主分类号 F02C7/052
代理机构 代理人
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