发明名称 Thrust nozzle for turbo airstream
摘要 The thrust nozzle, with or without vectorisation, particularly for turbo airstream transmissions with or without an afterburner, has a square construction. An even number of blades (5-16) is installed, and, in the case of only two blades, they are able to pivot both in line and in opposition to each other. With four or more blades, they are installed with alternating small and large axis spacing. Two blades with small axis spacing form a functional pair, and all left and all right blades are kinematically linked so that they pivot in the same direction.
申请公布号 DE4426195(A1) 申请公布日期 1996.01.25
申请号 DE19944426195 申请日期 1994.07.23
申请人 DAIMLER-BENZ AEROSPACE AG, 80804 MUENCHEN, DE 发明人 HERRMANN, OTFRID, DIPL.-ING., 84098 HOHENTHANN, DE
分类号 F02K1/00;F02K1/82;(IPC1-7):F02K1/40;F02K11/00 主分类号 F02K1/00
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