发明名称 Utloppsmunstycke till en jetmotor och förfarande för styrning av ett gasflöde från jetmotorn
摘要 An outlet nozzle for a jet engine has a gas intake and a gas outlet, at least one opening being provided through the nozzle boundary wall for the injection of a fluid into the nozzle in a direction perpendicular to one plane, for the purpose of controlling the direction of a gas flow from the jet engine so that vectoring occurs substantially tangentially in this plane. A first opening configuration is provided through the nozzle boundary wall on a first side of the nozzle center line and a second opening configuration is provided through the nozzle boundary wall on a second side of the nozzle center line. At least one of said first and second opening configurations has a substantial extension in the axial direction of the nozzle, in order to permit selective injection of the fluid through said opening configuration to a varying extent in the axial direction of the nozzle.
申请公布号 SE0402951(D0) 申请公布日期 2004.12.02
申请号 SE20040002951 申请日期 2004.12.02
申请人 VOLVO AERO CORP 发明人 BERNHARD GUSTAFSSON;ANDERS LUNDBLADH
分类号 F02K;F02K1/28;(IPC1-7):F02K/ 主分类号 F02K
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