发明名称 Method for the manufacture of an ejector nozzle tube
摘要 A method for manufacturing an ejector nozzle tube, includes forming an essentially rectangular plate-type blank 1 to have an undulating configuration on two opposite edge areas 2, 3, subsequently bending the blank around an axis 4, which is arranged centrically and parallel to the edge areas 2, 3, with the edge areas 2, 3 being superposed and subsequently joining the edge areas by point connections 6, providing for the formation of ejector nozzles 5 between the point connections.
申请公布号 US8782896(B2) 申请公布日期 2014.07.22
申请号 US200912566803 申请日期 2009.09.25
申请人 Rolls-Royce Deutschland Ltd & Co KG 发明人 Todorovic Predrag
分类号 B05B15/00;F02K1/36;F01D25/12;B64D33/10;F01D25/18;B21D51/06;B21D53/06;B21D51/10 主分类号 B05B15/00
代理机构 Shuttleworth & Ingersoll, PLC 代理人 Klima Timothy J.;Shuttleworth & Ingersoll, PLC
主权项 1. A method for manufacturing and using an ejector nozzle tube, comprising: forming an essentially rectangular sheet blank to have an undulating configuration on each of two opposite edge areas; forming the undulated opposite edge areas with different geometries relative to each other; subsequently bending the sheet around an axis, which is arranged centrally and parallel to the edge areas to superpose the edge areas to form an exterior surface having an aerodynamic drop shaped cross-section having a rounded inflow side and a flattened ejector side; and subsequently joining portions of the superposed edge areas which converge toward each other with point connections to form ejector nozzles between the point connections from portions of the superposed edge areas which diverge from each other to form the elector nozzle tube; wherein the different geometries form ejector nozzles having exit directions offset with respect to each other; positioning the ejector nozzle tube in a flow duct of a heat exchanger and passing a main flow through the flow duct and around the aerodynamic drop shaped exterior surface from the rounded inflow side to the flattened ejector side; introducing a secondary flow through the ejector nozzles into the main flow duct at a higher velocity than a velocity of the main flow to accelerate the main flow.
地址 DE