发明名称 |
HELICOPTER TRANSMISSION TAIL GEARBOX |
摘要 |
FIELD: aircraft engineering.SUBSTANCE: tail gearbox comprises drive and driven bevel gears fitted in crankcase and gear shafts bearings. Tail rotor incorporates two-bearing shaft with end section fitted in roller bearing of driven gear shaft inner support. Driven gear shaft outer bearing is fitted at crankcase taper cover and composed of two thrust ball bearings with adjustment rings. Crankcase has four connection clamps to upper attachment of gearbox to helicopter tail boom pylon.EFFECT: higher reliability.2 cl, 3 dwg |
申请公布号 |
RU2505459(C1) |
申请公布日期 |
2014.01.27 |
申请号 |
RU20120155780 |
申请日期 |
2012.12.24 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "MOSKOVSKIJ VERTOLETNYJ ZAVOD IM. M.L. MILJA" |
发明人 |
PRIVALOV EVGENIJ GRIGOR'EVICH;STEPANCHIKOV VLADIMIR ALEKSEEVICH;CHUGUNOV VLADIMIR IL'ICH;KARTASHOV VALENTIN FILIPPOVICH;ASTAF'EV VALERIJ IVANOVICH |
分类号 |
B64D35/00 |
主分类号 |
B64D35/00 |
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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