ANODE-LAYER ACCELERATOR

FIELD: plasma and space engineering. SUBSTANCE: insulating coat is applied to external surfaces of poles and screens an to those facing anode, as well as to side surfaces of anode on screen side and poles. EFFECT: reduced erosion of accelerator magnetic system poles and screens; reduced probability...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	NESTERENKO A.N, KOVALENKO S.I, SHABROV O.B
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY HEATING LIGHTING MACHINES OR ENGINES FOR LIQUIDS MECHANICAL ENGINEERING OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR PLASMA TECHNIQUE PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDEDFOR PRODUCING MECHANICAL POWER PRODUCTION OF ACCELERATED ELECTRICALLY-CHARGED PARTICLES OR OFNEUTRONS PRODUCTION OR ACCELERATION OF NEUTRAL MOLECULAR OR ATOMICBEAMS WEAPONS WIND, SPRING WEIGHT AND MISCELLANEOUS MOTORS
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Beschreibung
Zusammenfassung:	FIELD: plasma and space engineering. SUBSTANCE: insulating coat is applied to external surfaces of poles and screens an to those facing anode, as well as to side surfaces of anode on screen side and poles. EFFECT: reduced erosion of accelerator magnetic system poles and screens; reduced probability of anode-to-magnetic-system insulation breakdown. Использование: плазменная технология и космическая техника. Цель: уменьшение эрозии полюсов и экранов магнитной системы ускорителя, а также вероятности электрических пробоев между анодом и магнитной системой. Сущность изобретения: диэлектрическое покрытие нанесено на внешних и обращенные к аноду поверхностях полюсов и экранов, а также на боковых поверхностях анода со стороны экранов и полюсов.