FAN NACELLE TRAILING EDGE
A fan nacelle (104), a gas turbine engine cell assembly (190), and an aircraft are provided. The fan nacelle (104) includes a fan duct skin (110) arranged in a fan duct (112) to direct airflow from the fan of a Turbofan engine toward a fan nozzle (122). An exterior skin (114) of the fan nacelle dire...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | eng ; fre ; ger |
| 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 | HOWE, Sean P |
| description | A fan nacelle (104), a gas turbine engine cell assembly (190), and an aircraft are provided. The fan nacelle (104) includes a fan duct skin (110) arranged in a fan duct (112) to direct airflow from the fan of a Turbofan engine toward a fan nozzle (122). An exterior skin (114) of the fan nacelle directs air flow around an exterior of the engine. The fan duct skin (110) and the exterior skin (114) terminate at a trailing edge (108), and a trailing edge portion of the exterior skin is one of parallel to and diverging from a trailing edge portion of the fan duct skin in an aft direction. In certain aspects, the trailing edge portion of the exterior skin is actuatable or inflatable to selectively divert from the trailing edge portion of the fan duct skin. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3318494A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3318494A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3318494A13</originalsourceid><addsrcrecordid>eNrjZJB0c_RT8HN0dvXxcVUICXL09PH0c1dwdXF35WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxsaGFiaWJo6GxkQoAQCyRB9A</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>FAN NACELLE TRAILING EDGE</title><source>esp@cenet</source><creator>HOWE, Sean P</creator><creatorcontrib>HOWE, Sean P</creatorcontrib><description>A fan nacelle (104), a gas turbine engine cell assembly (190), and an aircraft are provided. The fan nacelle (104) includes a fan duct skin (110) arranged in a fan duct (112) to direct airflow from the fan of a Turbofan engine toward a fan nozzle (122). An exterior skin (114) of the fan nacelle directs air flow around an exterior of the engine. The fan duct skin (110) and the exterior skin (114) terminate at a trailing edge (108), and a trailing edge portion of the exterior skin is one of parallel to and diverging from a trailing edge portion of the fan duct skin in an aft direction. In certain aspects, the trailing edge portion of the exterior skin is actuatable or inflatable to selectively divert from the trailing edge portion of the fan duct skin.</description><language>eng ; fre ; ger</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>2018</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=20180509&DB=EPODOC&CC=EP&NR=3318494A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180509&DB=EPODOC&CC=EP&NR=3318494A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HOWE, Sean P</creatorcontrib><title>FAN NACELLE TRAILING EDGE</title><description>A fan nacelle (104), a gas turbine engine cell assembly (190), and an aircraft are provided. The fan nacelle (104) includes a fan duct skin (110) arranged in a fan duct (112) to direct airflow from the fan of a Turbofan engine toward a fan nozzle (122). An exterior skin (114) of the fan nacelle directs air flow around an exterior of the engine. The fan duct skin (110) and the exterior skin (114) terminate at a trailing edge (108), and a trailing edge portion of the exterior skin is one of parallel to and diverging from a trailing edge portion of the fan duct skin in an aft direction. In certain aspects, the trailing edge portion of the exterior skin is actuatable or inflatable to selectively divert from the trailing edge portion of the fan duct skin.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJB0c_RT8HN0dvXxcVUICXL09PH0c1dwdXF35WFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BxsaGFiaWJo6GxkQoAQCyRB9A</recordid><startdate>20180509</startdate><enddate>20180509</enddate><creator>HOWE, Sean P</creator><scope>EVB</scope></search><sort><creationdate>20180509</creationdate><title>FAN NACELLE TRAILING EDGE</title><author>HOWE, Sean P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3318494A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</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>HOWE, Sean P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HOWE, Sean P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>FAN NACELLE TRAILING EDGE</title><date>2018-05-09</date><risdate>2018</risdate><abstract>A fan nacelle (104), a gas turbine engine cell assembly (190), and an aircraft are provided. The fan nacelle (104) includes a fan duct skin (110) arranged in a fan duct (112) to direct airflow from the fan of a Turbofan engine toward a fan nozzle (122). An exterior skin (114) of the fan nacelle directs air flow around an exterior of the engine. The fan duct skin (110) and the exterior skin (114) terminate at a trailing edge (108), and a trailing edge portion of the exterior skin is one of parallel to and diverging from a trailing edge portion of the fan duct skin in an aft direction. In certain aspects, the trailing edge portion of the exterior skin is actuatable or inflatable to selectively divert from the trailing edge portion of the fan duct skin.</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; fre ; ger |
| recordid | cdi_epo_espacenet_EP3318494A1 |
| source | esp@cenet |
| 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 | FAN NACELLE TRAILING EDGE |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-19T15%3A36%3A10IST&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=HOWE,%20Sean%20P&rft.date=2018-05-09&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3318494A1%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 |