发明名称 TURBO-FAN ENGINE AND VERTICAL TAKEOFF AND LANDING AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To realize an unwasteful and rational structure regarding heat resistance of a material, to facilitate a design and suppress a whole cost including a cost of the material by dividing respective nozzles for by-pass air and jet in a turbo-fan engine having a vertical takeoff and landing function. SOLUTION: The turbo-fan engine E is provided with a by-pass-nozzle 3 for injecting by-pass air of low temperature passed through a fan 21 and injected as it is and a jet nozzle 27 for injecting jet of high temperature passed through a compressor from the fan 21 and burned. The by-pass nozzle 3 has a downward injection port 33 capable of downwardly injecting the by-pass air and a horizontal injection port 32 capable of horizontally injecting the by-pass air. The downward injection port 33 and the horizontal injection port 32 are constituted such that they can selectively inject the by-pass air to a downward direction and a horizontal direction by blocking one side by a blocking body 34. The jet nozzle 27 is constituted such that the jet can be downwardly injected.
申请公布号 JP2003028005(A) 申请公布日期 2003.01.29
申请号 JP20010215945 申请日期 2001.07.16
申请人 TOMIYASU KATSUAKI 发明人 TOMIYASU KATSUAKI
分类号 B64C29/00;F02K1/78;F02K3/06;(IPC1-7):F02K1/78 主分类号 B64C29/00
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