发明名称 CONTROL UNIT FOR THE LIFT ENGINES OF VERTICAL AND SHORT TAKEOFF AIRCRAFT
摘要 Control unit for the lift engines of vertical or short takeoff aircraft for correction of motion preferably in relation to the roll axis. The lift engine discharges into a branched conduit of which each respective branch discharges to opposite external sides of the aircraft fuselage Infinitely adjustable means are provided for selecting and proportioning as desired the respective amounts of the engine discharge introduced into and conducted through said respective branches.
申请公布号 US3703266(A) 申请公布日期 1972.11.21
申请号 USD3703266 申请日期 1970.05.18
申请人 MESSERSCHMITT-BOLKOW-BLOHM GMBH. 发明人 HANS LINCKS;ERICH W. WEIGMANN
分类号 B64C29/00;(IPC1-7):B64B1/36 主分类号 B64C29/00
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