发明名称 Axisymmetric thrust augmenting ejector with discrete primary air slot nozzles
摘要 A circular thrust augmenting ejector has an annular wall which defines a central passageway and a convergent contoured inlet section, a constant area cylindrical mixing section and a divergent conical diffuser outlet section. The inlet, mixing and outlet sections merge one into the next in axisymmetric serial relationship. The ejector also has a plurality of discrete primary nozzles arranged about the periphery of the annular wall at the entrance to the inlet section thereof for injecting a primary flow of high velocity air into the inlet section and thereby entraining a secondary flow of ambient air into the central passageway of the ejector.
申请公布号 US4448354(A) 申请公布日期 1984.05.15
申请号 US19820401163 申请日期 1982.07.23
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 REZNICK, STEVEN G.;FRANKE, MILTON E.
分类号 B64C29/00;F02K1/36;(IPC1-7):B64C15/00 主分类号 B64C29/00
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