SYSTEMS AND METHODS FOR REGULATORS FOR INFLATION SYSTEMS FOR EVACUATION ASSEMBLIES

A regulator arrangement (300) for an inflatable includes a regulator housing (302) comprising a bore (303), the bore comprising a longitudinal axis (390), a piston (304) disposed in the bore and configured to translate, with respect to the regulator housing, along the longitudinal axis, an adjuster...

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Bibliographische Detailangaben
Hauptverfasser:	KRUTS, Ivan, CZECHOWSKI, Kamil
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ACTUATING-FLOATS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COCKS COSMONAUTICS DEVICES FOR VENTING OR AERATING ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TAPS THERMAL INSULATION IN GENERAL TRANSPORTING VALVES WEAPONS
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Beschreibung
Zusammenfassung:	A regulator arrangement (300) for an inflatable includes a regulator housing (302) comprising a bore (303), the bore comprising a longitudinal axis (390), a piston (304) disposed in the bore and configured to translate, with respect to the regulator housing, along the longitudinal axis, an adjuster plug (306) disposed in the bore and axially adjacent the piston, an adjuster plug stop (308) disposed at least partially within the bore, and a spring member (310) disposed between the adjuster plug and the piston. The adjuster plug comprises a tapered head (314) and a shaft portion (316) extending from the tapered head. The adjuster plug stop comprises a tapered surface (320) configured to contact the tapered head.