发明名称 METHOD OF FABRICATING SPACECRAFT THERMAL CONTROL SYSTEM LIQUID CIRCUIT
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to thermal control systems (TCS) mainly, of telecommunication satellites, to their manufacture and ground tests. TCS fluid circuit comprises hydraulic accumulator with its tight gas chamber filled with two-phase fluid and separated from fluid chamber by bellows. Proposed method comprises controlling total tightness of fluid circuit prior to filling it with heat carrier and feeding check gas, for example, helium, thereto. Note here that said check gas is fed at maximum tolerable operating pressure in said circuit prior to connecting hydraulic accumulator thereto. Then, hydraulic accumulator chamber is welded to fluid circuit to test tightness of welded butt joint by probe. Fluid circuit as-assembled is subjected to test of total tightness prior to filling it with heat carrier. ^ EFFECT: higher validity of tightness tests. ^ 4 dwg
申请公布号 RU2446999(C1) 申请公布日期 2012.04.10
申请号 RU20100135075 申请日期 2010.08.20
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "INFORMATSIONNYE SPUTNIKOVYE SISTEMY" IMENI AKADEMIKA M.F. RESHETNEVA" 发明人 BARTENEV VLADIMIR AFANAS'EVICH;KHALIMANOVICH VLADIMIR IVANOVICH;KOLESNIKOV ANATOLIJ PETROVICH;TURKENICH ROMAN PETROVICH;NIKITIN VLADISLAV NIKOLAEVICH;AKCHURIN GEORGIJ VLADIMIROVICH
分类号 B64G1/50;B64G7/00 主分类号 B64G1/50
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