发明名称 TRIJET AIRCRAFT
摘要 An aircraft having a pair of wing mounted jet engines and an aft engine of the high-bypass turbofan type mounted in the vertical stabilizer of the tail section. The aft engine has a straight air inlet duct passing through vertical stabilizer spars attached directly to fuselage bulkheads. Each spar is a ring frame of a one-piece forging. A pylon beam extending aft from the base of the vertical stabilizer provides a top engine interface similar to that on the wing.
申请公布号 US3666211(A) 申请公布日期 1972.05.30
申请号 USD3666211 申请日期 1970.03.12
申请人 MCDONNELL DOUGLAS CORP. 发明人 RICHARD T. CATHERS;WILLIAM M. DOUGLASS;FREDERICK D. HESS JR.;JOHN MORRIS;JAMES E. ROBERTS
分类号 B64D27/20;B64F5/00;(IPC1-7):B64D27/20 主分类号 B64D27/20
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