发明名称 |
SEPARATEUR DE PARTICULES DE FLUX D'AIR D'ENTREE POUR MOTEUR A TURBINE A GAZ |
摘要 |
<p>The invention is an improved inlet particle separator for removing extraneous matter from a stream of air directed into the engine's core section. The improved separator utilizes two stages of separation. The first stage is an axial flow separator for initially separating engine inlet air into a first flow of relatively contaminated air and a second flow of relatively clean air. This first stage of separation is accomplished by sharply turning the air flow radially inwardly so that the relatively dense extraneous matter continues in its original direction into a scavenge system. A second stage of separation is accomplished in the scavenge system and comprises a centrifugal separator that separates the first flow of air into third and fourth flows of relatively contaminated air for the purpose of protecting a blower that powers the flow through the scavenge system and which is in flow communication with only the relatively less contaminated fourth flow of air.</p> |
申请公布号 |
FR2538452(B1) |
申请公布日期 |
1989.03.03 |
申请号 |
FR19830019907 |
申请日期 |
1983.12.13 |
申请人 |
GENERAL ELECTRIC CY |
发明人 |
DAVID DUBBLE KLASSEN, ROY ELBERT MOYER, FRANK ANTHONY LASTRINA ET ROBERT PATRICK TAMEO;MOYER ROY ELBERT;LASTRINA FRANK ANTHONY;TAMEO ROBERT PATRICK |
分类号 |
F02C7/052;(IPC1-7):02C7/05 |
主分类号 |
F02C7/052 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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