TANK FOR STORAGE AND EXPULSION OF LIQUID

mechanical engineering; devices for storage and expulsion of liquids under pressure of gas; expulsion of starting fuel in starting liquid- propellant rocket engine. SUBSTANCE: proposed tank includes load- bearing envelope 1, tubular flange 2 with circular groove 3, pipe union 4 for filling the tank...

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Bibliographische Detailangaben
Hauptverfasser:	SOLOV'EV V.P, MAKAROV M.M, BABOSHIN A.A, POLUSHIN V.G, OSOKIN M.I
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLUID-PRESSURE ACTUATORS FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS HYDRAULICS OR PNEUMATICS IN GENERAL JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	mechanical engineering; devices for storage and expulsion of liquids under pressure of gas; expulsion of starting fuel in starting liquid- propellant rocket engine. SUBSTANCE: proposed tank includes load- bearing envelope 1, tubular flange 2 with circular groove 3, pipe union 4 for filling the tank and discharge of liquid, hold-down ring 5, flexible diaphragm 6 with end projection 7, bottom 8, pipe union 9 for delivery of control gas, thin-walled ring 10, sealing gasket 22 and union nut 23. Bottom is provided with cavity 14. Inner surface of bottom is provided with holes 15. Cavity of bottom is provided with splitter 16 having holes 21. EFFECT: enhanced reliability at high pressures. 7 cl, 4 dwg