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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creator | KRUTS, Ivan CZECHOWSKI, Kamil |
description | 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. |
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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.</description><language>eng ; fre ; ger</language><subject>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</subject><creationdate>2022</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220126&DB=EPODOC&CC=EP&NR=3943397A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,781,886,25569,76552</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20220126&DB=EPODOC&CC=EP&NR=3943397A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KRUTS, Ivan</creatorcontrib><creatorcontrib>CZECHOWSKI, Kamil</creatorcontrib><title>SYSTEMS AND METHODS FOR REGULATORS FOR INFLATION SYSTEMS FOR EVACUATION ASSEMBLIES</title><description>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.</description><subject>ACTUATING-FLOATS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COCKS</subject><subject>COSMONAUTICS</subject><subject>DEVICES FOR VENTING OR AERATING</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TAPS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>VALVES</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZAgKjgwOcfUNVnD0c1HwdQ3x8HcJVnDzD1IIcnUP9XEM8Q-CcD393IA8T38_BZgGkKhrmKNzKETYMTjY1dfJx9M1mIeBNS0xpziVF0pzMyi4uYY4e-imFuTHpxYXJCan5qWWxLsGGFuaGBtbmjsaGhOhBACvky-8</recordid><startdate>20220126</startdate><enddate>20220126</enddate><creator>KRUTS, Ivan</creator><creator>CZECHOWSKI, Kamil</creator><scope>EVB</scope></search><sort><creationdate>20220126</creationdate><title>SYSTEMS AND METHODS FOR REGULATORS FOR INFLATION SYSTEMS FOR EVACUATION ASSEMBLIES</title><author>KRUTS, Ivan ; CZECHOWSKI, Kamil</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3943397A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>ACTUATING-FLOATS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COCKS</topic><topic>COSMONAUTICS</topic><topic>DEVICES FOR VENTING OR AERATING</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TAPS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>VALVES</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KRUTS, Ivan</creatorcontrib><creatorcontrib>CZECHOWSKI, Kamil</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KRUTS, Ivan</au><au>CZECHOWSKI, Kamil</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEMS AND METHODS FOR REGULATORS FOR INFLATION SYSTEMS FOR EVACUATION ASSEMBLIES</title><date>2022-01-26</date><risdate>2022</risdate><abstract>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.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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source | esp@cenet |
subjects | 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 |
title | SYSTEMS AND METHODS FOR REGULATORS FOR INFLATION SYSTEMS FOR EVACUATION ASSEMBLIES |
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