公开(公告)号：US20110083418A1

公开(公告)日：2011-04-14

申请号：US12903504

申请日：2010-10-13

申请人： Helmut Ciezki ,  Ralf Stark

发明人： Helmut Ciezki ,  Ralf Stark

IPC分类号： F02K9/90

CPC分类号： F42B10/64 ,  F02K9/90 ,  F42B10/665

摘要： In order to provide a flying object with an engine comprising a combustion chamber with a combustion space and a nozzle with a nozzle space following the combustion chamber, the transition between combustion chamber and nozzle lying in a plane in which a cross-section of the combustion space converges, in which thrust control in terms of magnitude and/or thrust vector can be carried out in a simple manner, it is provided that a centre body adapted to have combustion products flowing around it is at least partially arranged in the nozzle space, outside of the combustion space, and at least three jet vanes are arranged at the centre body.

摘要翻译： 为了提供具有发动机的飞行物体，发动机包括具有燃烧空间的燃烧室和具有跟随燃烧室的喷嘴空间的喷嘴，燃烧室和喷嘴之间的过渡位于其中燃烧截面的平面中 空间会聚，其中以幅度和/或推力矢量为基础的推力控制可以以简单的方式进行，其中，适于具有围绕其流动的燃烧产物的中心体至少部分地布置在喷嘴空间中， 在燃烧空间外部，并且至少三个喷射叶片布置在中心体。

公开(公告)号：US08561385B2

公开(公告)日：2013-10-22

申请号：US12903504

申请日：2010-10-13

申请人： Helmut Ciezki ,  Ralf Stark

发明人： Helmut Ciezki ,  Ralf Stark

IPC分类号： F02K1/00

CPC分类号： F42B10/64 ,  F02K9/90 ,  F42B10/665

摘要： A flying object is provided with an engine comprising a combustion chamber with a combustion space and a nozzle with a nozzle space following the combustion chamber, the transition between combustion chamber and nozzle lying in a plane in which a cross-section of the combustion space converges, in which thrust control in terms of magnitude and/or thrust vector can be carried out in a simple manner, it is provided that a centre body adapted to have combustion products flowing around it is at least partially arranged in the nozzle space, outside of the combustion space, and at least three jet vanes are arranged at the centre body.

摘要翻译： 飞行物体设置有发动机，发动机包括具有燃烧空间的燃烧室和具有跟随燃烧室的喷嘴空间的喷嘴，燃烧室和喷嘴之间的过渡位于燃烧空间的横截面收敛的平面中 ，其中可以以简单的方式执行在大小和/或推力矢量方面的推力控制，其中，适于使其周围流动的燃烧产物的中心体至少部分地布置在喷嘴空间中， 燃烧空间和至少三个喷射叶片布置在中心体。