FIELD: automatic gas control and distributing systems for plasma accelerators; process plasma sources. SUBSTANCE: system is designed for feeding working medium to plasma accelerators in wide range of temperatures and at high levels of mechanical loads encountered in the course of operation; it has interconnected valves and throttling devices; longitudinal axes of valves and throttling devices lie in same locating plane; valves are placed between pair of brackets provided with cradle- shaped slots accommodating these valves; holes are made in brackets in valve-to-valve clearances; second pair of similar brackets is placed around joints between valves and throttling devices; outer surfaces of brackets on one side relative to location plane form first locating plane; opposing surfaces and those of opposing brackets form second locating surface. Brackets located on one side relative to locating plane may have tie plate with holes; flexible gaskets may be installed in joints between valve and cradle-shaped slots. EFFECT: enhanced operating efficiency and reliability of system. 3 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
CLOSED-ELECTRON-DRIFT PLASMA-JET ENGINE | 2000 |
|
RU2191290C2 |
PLASMA ENGINE WITH CLOSED ELECTRON DRIFT | 2000 |
|
RU2196922C2 |
CLOSED-ELECTRON-DRIFT PLASMA-JET ENGINE | 2000 |
|
RU2191289C2 |
CLOSED-ELECTRON-DRIFT PLASMA-JET ENGINE | 2000 |
|
RU2191487C2 |
CLOSED ELECTRON DRIFT PLASMA JET ENGINE | 2000 |
|
RU2188337C2 |
PLASMA-JET WITH CLOSED DRIFT OF ELECTRONS | 2000 |
|
RU2204053C2 |
COMPENSATING CATHODE | 2000 |
|
RU2173002C1 |
COMPENSATING CATHODE | 2000 |
|
RU2173001C1 |
ELECTRIC ROCKET PROPULSION SYSTEM | 2001 |
|
RU2200874C2 |
CLOSED-ELECTRON-DRIFT PLASMA-JET ENGINE | 2000 |
|
RU2191291C2 |
Authors
Dates
2002-03-10—Published
2000-05-15—Filed