发明名称 Gas turbine engine diffuser - has flow separating vanes in sidewalls formed with slots opening into cavities within vanes
摘要 <p>A flow stabiliser equalises the flow of fluid through the passageways of the channel diffuser used with a centrifugal type rotary compressor. Slots are formed in the sidewalls of the flow separating vanes in the diffuser. The slots open into cavities within the vanes. The cavities communicate by openings thrugh the diffuser wall into a common closed manifold. The fluid interconnection between the passageways in the diffuser and the encircling common manifold increases the operating range of the compressor since pressure surges in one or more passageways are quickly equalised.</p>
申请公布号 IT1101459(B) 申请公布日期 1985.09.28
申请号 IT19780030363 申请日期 1978.11.30
申请人 AVCO CORP 发明人
分类号 F04D;(IPC1-7):F04D/ 主分类号 F04D
代理机构 代理人
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