发明名称 HELICOPTER TRANSMISSION TAIL SHAFT
摘要 FIELD: transport. ^ SUBSTANCE: helicopter transmission tail shaft comprises tubular sections (1) with coupling flanges and bearing splined couplings (3, 4) jointing the sections together, torque measuring device with pickup (19) and two indicators representing toothed rims (13, 18). Length of one tubular section is taken to be the base of measurements. Note that this section is furnished with inner shaft (7) with one end rigidly attached to one end of the said section and its other end is mounted with the help of support (20) nearby the other end of the said tubular section. Note that the latter end is provided with an end flange arranged between the section coupling flange and that of the splined bearing sleeve to run free around the inner shaft end flange. Toothed rim of one inductor is fitted on the inner shaft end flange, while the other inductor toothed rim is located on the section coupling flange. ^ EFFECT: higher safety of helicopter. ^ 3 cl, 3 dwg
申请公布号 RU2350515(C1) 申请公布日期 2009.03.27
申请号 RU20070146210 申请日期 2007.12.14
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "MOSKOVSKIJ VERTOLETNYJ ZAVOD IM. M.L. MILJA" 发明人 KARTASHOV VALENTIN FILIPPOVICH;PRIVALOV EVGENIJ GRIGOR'EVICH;STEPANCHIKOV VLADIMIR ALEKSEEVICH
分类号 B64D35/00;B64D43/00 主分类号 B64D35/00
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