Ball Valve
An aircraft fuel system ball valve (fig.2a,100) has an integrated valve housing 120 with a support portion (fig.2a,116), and a ball housing (fig.2a,115) with a first conduit 113 and an opposing aperture 122; a ball 112 received in the ball housing; and a second conduit 114. The second conduit and ap...
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| creator | Guruprasad Ramesh Pujar Thenard Olivier Manish M Bharti Vismay Vinod Walle Ravindra Pradip Dhotre |
| description | An aircraft fuel system ball valve (fig.2a,100) has an integrated valve housing 120 with a support portion (fig.2a,116), and a ball housing (fig.2a,115) with a first conduit 113 and an opposing aperture 122; a ball 112 received in the ball housing; and a second conduit 114. The second conduit and aperture have complimentary engagement features (such a snap-fit features or a bayonet fitting) so the second conduit may be removably attached. A seal may be provided on an inner surface of the aperture or an outer surface of an interface of the second conduit received in the aperture. The valve housing may be moulded from carbon reinforced polyether ether ketone (PEEK). Preferably, the engagement features are arranged around the periphery of the aperture and an end of second conduit. Snap-fit engagement features may have a resilient part which is deflected during assembly and engages an internal recess of the second conduit when assembled; an aperture in the housing is aligned with the snap-fit features to allow disassembly. Bayonet connections may utilise a sprung pin as a latch to maintain alignment of the second conduit and the housing. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_GB2568336A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>GB2568336A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_GB2568336A3</originalsourceid><addsrcrecordid>eNrjZOBySszJUQhLzClL5WFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8e5ORqZmFsbGZo7GhFUAAC7lG7g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Ball Valve</title><source>esp@cenet</source><creator>Guruprasad Ramesh Pujar ; Thenard Olivier ; Manish M Bharti ; Vismay Vinod Walle ; Ravindra Pradip Dhotre</creator><creatorcontrib>Guruprasad Ramesh Pujar ; Thenard Olivier ; Manish M Bharti ; Vismay Vinod Walle ; Ravindra Pradip Dhotre</creatorcontrib><description>An aircraft fuel system ball valve (fig.2a,100) has an integrated valve housing 120 with a support portion (fig.2a,116), and a ball housing (fig.2a,115) with a first conduit 113 and an opposing aperture 122; a ball 112 received in the ball housing; and a second conduit 114. The second conduit and aperture have complimentary engagement features (such a snap-fit features or a bayonet fitting) so the second conduit may be removably attached. A seal may be provided on an inner surface of the aperture or an outer surface of an interface of the second conduit received in the aperture. The valve housing may be moulded from carbon reinforced polyether ether ketone (PEEK). Preferably, the engagement features are arranged around the periphery of the aperture and an end of second conduit. Snap-fit engagement features may have a resilient part which is deflected during assembly and engages an internal recess of the second conduit when assembled; an aperture in the housing is aligned with the snap-fit features to allow disassembly. Bayonet connections may utilise a sprung pin as a latch to maintain alignment of the second conduit and the housing.</description><language>eng</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>2019</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=20190515&DB=EPODOC&CC=GB&NR=2568336A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190515&DB=EPODOC&CC=GB&NR=2568336A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Guruprasad Ramesh Pujar</creatorcontrib><creatorcontrib>Thenard Olivier</creatorcontrib><creatorcontrib>Manish M Bharti</creatorcontrib><creatorcontrib>Vismay Vinod Walle</creatorcontrib><creatorcontrib>Ravindra Pradip Dhotre</creatorcontrib><title>Ball Valve</title><description>An aircraft fuel system ball valve (fig.2a,100) has an integrated valve housing 120 with a support portion (fig.2a,116), and a ball housing (fig.2a,115) with a first conduit 113 and an opposing aperture 122; a ball 112 received in the ball housing; and a second conduit 114. The second conduit and aperture have complimentary engagement features (such a snap-fit features or a bayonet fitting) so the second conduit may be removably attached. A seal may be provided on an inner surface of the aperture or an outer surface of an interface of the second conduit received in the aperture. The valve housing may be moulded from carbon reinforced polyether ether ketone (PEEK). Preferably, the engagement features are arranged around the periphery of the aperture and an end of second conduit. Snap-fit engagement features may have a resilient part which is deflected during assembly and engages an internal recess of the second conduit when assembled; an aperture in the housing is aligned with the snap-fit features to allow disassembly. Bayonet connections may utilise a sprung pin as a latch to maintain alignment of the second conduit and the housing.</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>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZOBySszJUQhLzClL5WFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8e5ORqZmFsbGZo7GhFUAAC7lG7g</recordid><startdate>20190515</startdate><enddate>20190515</enddate><creator>Guruprasad Ramesh Pujar</creator><creator>Thenard Olivier</creator><creator>Manish M Bharti</creator><creator>Vismay Vinod Walle</creator><creator>Ravindra Pradip Dhotre</creator><scope>EVB</scope></search><sort><creationdate>20190515</creationdate><title>Ball Valve</title><author>Guruprasad Ramesh Pujar ; Thenard Olivier ; Manish M Bharti ; Vismay Vinod Walle ; Ravindra Pradip Dhotre</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2568336A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2019</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>Guruprasad Ramesh Pujar</creatorcontrib><creatorcontrib>Thenard Olivier</creatorcontrib><creatorcontrib>Manish M Bharti</creatorcontrib><creatorcontrib>Vismay Vinod Walle</creatorcontrib><creatorcontrib>Ravindra Pradip Dhotre</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Guruprasad Ramesh Pujar</au><au>Thenard Olivier</au><au>Manish M Bharti</au><au>Vismay Vinod Walle</au><au>Ravindra Pradip Dhotre</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Ball Valve</title><date>2019-05-15</date><risdate>2019</risdate><abstract>An aircraft fuel system ball valve (fig.2a,100) has an integrated valve housing 120 with a support portion (fig.2a,116), and a ball housing (fig.2a,115) with a first conduit 113 and an opposing aperture 122; a ball 112 received in the ball housing; and a second conduit 114. The second conduit and aperture have complimentary engagement features (such a snap-fit features or a bayonet fitting) so the second conduit may be removably attached. A seal may be provided on an inner surface of the aperture or an outer surface of an interface of the second conduit received in the aperture. The valve housing may be moulded from carbon reinforced polyether ether ketone (PEEK). Preferably, the engagement features are arranged around the periphery of the aperture and an end of second conduit. Snap-fit engagement features may have a resilient part which is deflected during assembly and engages an internal recess of the second conduit when assembled; an aperture in the housing is aligned with the snap-fit features to allow disassembly. Bayonet connections may utilise a sprung pin as a latch to maintain alignment of the second conduit and the housing.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| 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 | Ball Valve |
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