发明名称 Axial divergent section slot nozzle
摘要 <p>An axial divergent section slot nozzle (10) for an engine is provided. The nozzle has a plurality of spaced apart divergent flaps (12), at least one device for moving the divergent flaps (12) to change a cross sectional area of the nozzle in a throat region, and a bridge member (20) positioned intermediate adjacent ones of the flaps (12). The bridge member (20) includes a bridge bracket (216) and a sealing element (204) joined to the bridge bracket (216). The sealing element (204) has an upper surface (226). The bridge bracket (216) has a lower surface (222,224) which diverges from the upper surface (226) of the sealing element (204). In a preferred embodiment of the present invention, the bridge bracket (216) has a shape which allows variable slot size depending on nozzle throat jet area.</p>
申请公布号 EP1580420(B1) 申请公布日期 2008.01.30
申请号 EP20050251808 申请日期 2005.03.23
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 BUSH, ROBERT;ZAMORA, SEAN;CULVER, HARRY;PETERS, DONALD WILLIAM
分类号 F02K1/80;F02K1/00;F02K1/12;F02K1/36 主分类号 F02K1/80
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