Changeover valve
A changeover valve for a tandem fan type of engine is located in a duct (4) between fan stages (54,56) at either end. The valve arrangement has a butterfly flap valve (2) to selectively obstruct flow along the cut, a drop-down chute (32) to eject front fan flow and secondary inlet means (10) to indu...
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| creator | ROBERT CHARLES TONKS |
| description | A changeover valve for a tandem fan type of engine is located in a duct (4) between fan stages (54,56) at either end. The valve arrangement has a butterfly flap valve (2) to selectively obstruct flow along the cut, a drop-down chute (32) to eject front fan flow and secondary inlet means (10) to induct air to the second fan stage (54) to supply the core engine. The secondary inlet means (10) comprises drop-in doors (11) hinged to pivot (50) into the duct (4) behind the flap valve (2). A tertiary airflow in a space (20) defined by the duct (4) and an engine nacelle (14) is admitted to the region at the second fan entry face which is shadowed by the secondary inlet doors (11). |
| format | Patent |
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The valve arrangement has a butterfly flap valve (2) to selectively obstruct flow along the cut, a drop-down chute (32) to eject front fan flow and secondary inlet means (10) to induct air to the second fan stage (54) to supply the core engine. The secondary inlet means (10) comprises drop-in doors (11) hinged to pivot (50) into the duct (4) behind the flap valve (2). A tertiary airflow in a space (20) defined by the duct (4) and an engine nacelle (14) is admitted to the region at the second fan entry face which is shadowed by the secondary inlet doors (11).</description><edition>5</edition><language>eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>1994</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=19940928&DB=EPODOC&CC=GB&NR=2261918B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19940928&DB=EPODOC&CC=GB&NR=2261918B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ROBERT CHARLES TONKS</creatorcontrib><title>Changeover valve</title><description>A changeover valve for a tandem fan type of engine is located in a duct (4) between fan stages (54,56) at either end. The valve arrangement has a butterfly flap valve (2) to selectively obstruct flow along the cut, a drop-down chute (32) to eject front fan flow and secondary inlet means (10) to induct air to the second fan stage (54) to supply the core engine. The secondary inlet means (10) comprises drop-in doors (11) hinged to pivot (50) into the duct (4) behind the flap valve (2). A tertiary airflow in a space (20) defined by the duct (4) and an engine nacelle (14) is admitted to the region at the second fan entry face which is shadowed by the secondary inlet doors (11).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1994</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBBwzkjMS0_NL0stUihLzClL5WFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8e5ORkZmhpaGFk7GhFUAADFQHl8</recordid><startdate>19940928</startdate><enddate>19940928</enddate><creator>ROBERT CHARLES TONKS</creator><scope>EVB</scope></search><sort><creationdate>19940928</creationdate><title>Changeover valve</title><author>ROBERT CHARLES TONKS</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2261918B3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1994</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ROBERT CHARLES TONKS</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ROBERT CHARLES TONKS</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Changeover valve</title><date>1994-09-28</date><risdate>1994</risdate><abstract>A changeover valve for a tandem fan type of engine is located in a duct (4) between fan stages (54,56) at either end. The valve arrangement has a butterfly flap valve (2) to selectively obstruct flow along the cut, a drop-down chute (32) to eject front fan flow and secondary inlet means (10) to induct air to the second fan stage (54) to supply the core engine. The secondary inlet means (10) comprises drop-in doors (11) hinged to pivot (50) into the duct (4) behind the flap valve (2). A tertiary airflow in a space (20) defined by the duct (4) and an engine nacelle (14) is admitted to the region at the second fan entry face which is shadowed by the secondary inlet doors (11).</abstract><edition>5</edition><oa>free_for_read</oa></addata></record> |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | Changeover valve |
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