发明名称 Double lobed mixer for turbofan engine
摘要 <p>A lobed mixer (7) has major and minor lobes (8,9). The major lobes increase in both height and width in the downstream axial direction. Each major lobe (8) has two minor lobes (9) positioned on its radially outer surface located downstream of the beginning of the major lobe. The radial depth of the minor lobes increases with downstream axial distance but is never greater than the depth of the major lobes. Each of the chutes (11) formed between the minor lobes introduces an additional stream of cold, low velocity fan flow into the hot, high velocity core flow to improve the uniformity of mixing. The double lobed mixer decreases acoustic intensity while having little or no effect on engine performance. <IMAGE></p>
申请公布号 EP0761956(A2) 申请公布日期 1997.03.12
申请号 EP19960306545 申请日期 1996.09.09
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 ZYSMAN, STEVEN H.;LORD, WESLEY K.;BARBER, THOMAS J.
分类号 F02K1/40;F02K1/38;F02K1/46;F02K1/48;F02K3/06;(IPC1-7):F02K1/48 主分类号 F02K1/40
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