发明名称 LIQUID-PROPELLANT ROCKET ENGINE UNITS ATTACHMENT
摘要 FIELD: engines and pumps.SUBSTANCE: invention relates to rocketry and can be used in production of liquid-propellant engines. Claimed device comprises the link composed by the tube with spherical blocks for attachment to the frame or to the bodies of rocket units, the main bearings with axial bores, mid bearings with threaded parts and axial bores, captive nuts, washers with spherical inner surface, adapters with LH and RH threads and lock nuts. The bores from identical material with the main bearings. Distinguishing circular mark is made at one of the main bearings.EFFECT: higher reliability and resistance to vibrations.5 cl, 12 dwg
申请公布号 RU2573628(C2) 申请公布日期 2016.01.20
申请号 RU20140103949 申请日期 2014.02.04
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "KONSTRUKTORSKOE BJURO KHIMAVTOMATIKI" 发明人 KUZNETSOV ALEKSANDR VASIL'EVICH;SOLDATOV DMITRIJ VALER'EVICH
分类号 F02K9/00;F16B2/20 主分类号 F02K9/00
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