公开(公告)号：US20110030341A1

公开(公告)日：2011-02-10

申请号：US12935445

申请日：2009-03-31

申请人： Jerome Huber ,  Jean-Paul Nonnet ,  Joel Delville ,  Peter Jordan ,  Francois Strekowski

发明人： Jerome Huber ,  Jean-Paul Nonnet ,  Joel Delville ,  Peter Jordan ,  Francois Strekowski

IPC分类号： F02K1/34

CPC分类号： F02K1/34 ,  F02K1/46 ,  F05D2240/40 ,  F05D2250/11

摘要： An aircraft jet engine including a wall centered about a longitudinal axis and surrounding a stream of gas ejected at a downstream end of the wall in the direction of the axis, primary ducts distributed at the periphery of the downstream end of the wall configured on command each to eject a jet of primary fluid to interact with the ejected stream of gas, the primary ducts of each pair converging towards one another near the downstream end of the wall so that the primary jets ejected form two sides of a triangle that meet at the vertex thereof in a view projected onto a plane perpendicular to a transverse plane, and secondary ducts each associated with each pair of primary ducts and configured on command to eject a jet of secondary fluid directed into the triangle formed by the primary jets.

摘要翻译： 一种飞机喷气式发动机，其包括围绕纵向轴线居中并围绕沿着轴线方向在壁的下游端喷射的气体流的壁，分配在壁的下游端的周边的主要管道，其分配在每个 喷射主流体的喷射流与喷射的气流相互作用，每对的主要管道在壁的下游端彼此会聚，使得主喷嘴从三角形的两侧喷射，该三角形在顶点处相遇 它们在投影到垂直于横向平面的平面上的视图中，以及每个与每对主要管道相关联的辅助管道，并且根据命令配置以喷射引导到由主喷嘴形成的三角形形成的三角形的二次流体的射流。