LIGHTWEIGHT CABIN PRESSURE THRUST RECOVERY OUTFLOW VALVE
An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.
Gespeichert in:
| Hauptverfasser: | , , , , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | |
|---|---|
| container_issue | |
| container_start_page | |
| container_title | |
| container_volume | |
| creator | KANG ALBERT MILLER BETH PRODROMIDES KEVIN FUHRMANN BARRETT HORNER DARRELL YADAV GOVIND SCHROEDER KARL GENTILE DAVID P MEYER ROSS F |
| description | An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US2014134936A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US2014134936A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US2014134936A13</originalsourceid><addsrcrecordid>eNrjZLDw8XT3CAl3BZEKzo5Onn4KAUGuwcGhQa4KIR5BocEhCkGuzv5hrkGRCv6hIW4-_uEKYY4-Ya48DKxpiTnFqbxQmptB2c01xNlDN7UgPz61uCAxOTUvtSQ-NNjIwNDE0NjE0tjM0dCYOFUAQ_wp8g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>LIGHTWEIGHT CABIN PRESSURE THRUST RECOVERY OUTFLOW VALVE</title><source>esp@cenet</source><creator>KANG ALBERT ; MILLER BETH ; PRODROMIDES KEVIN ; FUHRMANN BARRETT ; HORNER DARRELL ; YADAV GOVIND ; SCHROEDER KARL ; GENTILE DAVID P ; MEYER ROSS F</creator><creatorcontrib>KANG ALBERT ; MILLER BETH ; PRODROMIDES KEVIN ; FUHRMANN BARRETT ; HORNER DARRELL ; YADAV GOVIND ; SCHROEDER KARL ; GENTILE DAVID P ; MEYER ROSS F</creatorcontrib><description>An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.</description><language>eng</language><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; RANGES ; TRANSPORTING ; VENTILATING ; WEAPONS</subject><creationdate>2014</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=20140515&DB=EPODOC&CC=US&NR=2014134936A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140515&DB=EPODOC&CC=US&NR=2014134936A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KANG ALBERT</creatorcontrib><creatorcontrib>MILLER BETH</creatorcontrib><creatorcontrib>PRODROMIDES KEVIN</creatorcontrib><creatorcontrib>FUHRMANN BARRETT</creatorcontrib><creatorcontrib>HORNER DARRELL</creatorcontrib><creatorcontrib>YADAV GOVIND</creatorcontrib><creatorcontrib>SCHROEDER KARL</creatorcontrib><creatorcontrib>GENTILE DAVID P</creatorcontrib><creatorcontrib>MEYER ROSS F</creatorcontrib><title>LIGHTWEIGHT CABIN PRESSURE THRUST RECOVERY OUTFLOW VALVE</title><description>An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.</description><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>RANGES</subject><subject>TRANSPORTING</subject><subject>VENTILATING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLDw8XT3CAl3BZEKzo5Onn4KAUGuwcGhQa4KIR5BocEhCkGuzv5hrkGRCv6hIW4-_uEKYY4-Ya48DKxpiTnFqbxQmptB2c01xNlDN7UgPz61uCAxOTUvtSQ-NNjIwNDE0NjE0tjM0dCYOFUAQ_wp8g</recordid><startdate>20140515</startdate><enddate>20140515</enddate><creator>KANG ALBERT</creator><creator>MILLER BETH</creator><creator>PRODROMIDES KEVIN</creator><creator>FUHRMANN BARRETT</creator><creator>HORNER DARRELL</creator><creator>YADAV GOVIND</creator><creator>SCHROEDER KARL</creator><creator>GENTILE DAVID P</creator><creator>MEYER ROSS F</creator><scope>EVB</scope></search><sort><creationdate>20140515</creationdate><title>LIGHTWEIGHT CABIN PRESSURE THRUST RECOVERY OUTFLOW VALVE</title><author>KANG ALBERT ; MILLER BETH ; PRODROMIDES KEVIN ; FUHRMANN BARRETT ; HORNER DARRELL ; YADAV GOVIND ; SCHROEDER KARL ; GENTILE DAVID P ; MEYER ROSS F</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2014134936A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2014</creationdate><topic>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>RANGES</topic><topic>TRANSPORTING</topic><topic>VENTILATING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>KANG ALBERT</creatorcontrib><creatorcontrib>MILLER BETH</creatorcontrib><creatorcontrib>PRODROMIDES KEVIN</creatorcontrib><creatorcontrib>FUHRMANN BARRETT</creatorcontrib><creatorcontrib>HORNER DARRELL</creatorcontrib><creatorcontrib>YADAV GOVIND</creatorcontrib><creatorcontrib>SCHROEDER KARL</creatorcontrib><creatorcontrib>GENTILE DAVID P</creatorcontrib><creatorcontrib>MEYER ROSS F</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KANG ALBERT</au><au>MILLER BETH</au><au>PRODROMIDES KEVIN</au><au>FUHRMANN BARRETT</au><au>HORNER DARRELL</au><au>YADAV GOVIND</au><au>SCHROEDER KARL</au><au>GENTILE DAVID P</au><au>MEYER ROSS F</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>LIGHTWEIGHT CABIN PRESSURE THRUST RECOVERY OUTFLOW VALVE</title><date>2014-05-15</date><risdate>2014</risdate><abstract>An aircraft cabin pressure control system outflow thrust recovery valve includes a frame, a valve element, and actuation hardware. The frame, valve element, and at least a portion of the actuation hardware are made of composite material. The actuation hardware is disposed external to the frame.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng |
| recordid | cdi_epo_espacenet_US2014134936A1 |
| source | esp@cenet |
| subjects | AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS RANGES TRANSPORTING VENTILATING WEAPONS |
| title | LIGHTWEIGHT CABIN PRESSURE THRUST RECOVERY OUTFLOW VALVE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-13T00%3A59%3A09IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=KANG%20ALBERT&rft.date=2014-05-15&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS2014134936A1%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |