发明名称 |
УСТРОЙСТВО ОБЕСПЕЧЕНИЯ ГЕРМЕТИЧНОСТИ В ТУРБОРЕАКТИВНОМ ДВИГАТЕЛЕ, ВЫПОЛНЕННОЕ В ВИДЕ ЩЕТОЧНОЙ ПРОКЛАДКИ ДЛЯ ЗАБОРА ВОЗДУХА В КАБИНУ |
摘要 |
The engine has a crankcase whose outer shell is fixed to an annular structure (7) by a joint with brush (50) fixed to a periphery of an upstream part of an outer case (12) of a diffuser grid (10). The joint has radially extending bristles (52) supported on an inner surface (54) of a cylindrical sleeve (53). The sleeve integrated to the structure that is connected to an outer shell (6) of a compressor (1), surrounds the joint. |
申请公布号 |
RU2004127896(A) |
申请公布日期 |
2006.02.20 |
申请号 |
RU20040127896 |
申请日期 |
2004.09.17 |
申请人 |
СНЕКМА МОТЕР (FR) |
发明人 |
ЛЕПРЕТР Жилль (FR);МАРНА Лоран (FR) |
分类号 |
F02K1/80;F02K3/00;F01D11/00;F01D25/24;F02C7/28;F02K1/00 |
主分类号 |
F02K1/80 |
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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