发明名称 |
GAS-TURBINE ENGINE EXHAUST UNIT |
摘要 |
FIELD: aviation; exhaust devices operating in hot media. SUBSTANCE: inner fairing has holes uniformly spaced over surface and accommodating cups made to suit outer profile of struts fitted radially with clearance through cups into fairing and connected with inner surface of fairing by means of Z-shaped thin-walled dampers. EFFECT: enhanced reliability of operation of exhaust unit. 1 dwg |
申请公布号 |
RU94028910(A) |
申请公布日期 |
1996.05.27 |
申请号 |
RU19940028910 |
申请日期 |
1994.07.28 |
申请人 |
NAUCHNO-PROIZVODSTVENNOE PREDPRIJATIE "ZAVOD IM.V.JA.KLIMOVA" |
发明人 |
DOLGOPOLOV JU.A.;KHROMENKOV V.S. |
分类号 |
F01D25/30;F02C7/00;F02K1/04 |
主分类号 |
F01D25/30 |
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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