发明名称 TEST RIG FOR DETERMINATION OF HYDRAULIC RESIDUES OF FUEL IN MISSILE TANK
摘要 FIELD: machine building.SUBSTANCE: test rig contains movable horizontal platform with drive, drain tank with consumption pipeline, drain pipeline with continuity transmitter and flexible link. The platform is installed on the rig frame by means of the several parallel pendulum posts. On the platform the tested tank with intake device and drain pipeline with continuity transmitter are rigidly secured. In the consumption pipeline the flowmeter, shutoff valve, flowrate controller, hydraulic pump are installed. Pump inlet is connected to the drain tank by loop main with installed valve. The drain pipeline is rigidly secured on the platform, connected to tested tank and via the flexible link is connected with the consumption pipeline. The flexible link is made in form of a pipe with tight spherical hinges at ends and is located parallel to the posts. The flexible link length is equal to the posts height.EFFECT: increased accuracy of hydraulic residues determination in the tested tank of the missile, and exclusion of the loads on the drain pipeline of the tested tank.1 dwg
申请公布号 RU2543703(C1) 申请公布日期 2015.03.10
申请号 RU20130139413 申请日期 2013.08.23
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "GOSUDARSTVENNYJ RAKETNYJ TSENTR IMENI AKADEMIKA V.P. MAKEEVA" 发明人 TABAROV GAJ ZAKIEVICH;IL'ICHENKO EVGENIJ KONSTANTINOVICH
分类号 G01M10/00;F02K9/96 主分类号 G01M10/00
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