NACELLE FOR AN AIRCRAFT AFT FAN

An aircraft (10) is provided including a fuselage (12) extending between a forward end (16) and an aft end (18). An aft engine is mounted to the fuselage (12) at the aft end of the fuselage (18). The aft engine includes a nacelle (306) having a forward section. An airflow duct (344) is also provided...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: WOOD, Trevor Howard, RAMAKRISHNAN, Kishore
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 WOOD, Trevor Howard
RAMAKRISHNAN, Kishore
description An aircraft (10) is provided including a fuselage (12) extending between a forward end (16) and an aft end (18). An aft engine is mounted to the fuselage (12) at the aft end of the fuselage (18). The aft engine includes a nacelle (306) having a forward section. An airflow duct (344) is also provided extending at least partially through the nacelle (306) and including an opening on the forward section of the nacelle (330). The opening is configured for providing an airflow to, or receiving an airflow from, the forward section of the nacelle (306) to increase an amount of, e.g., boundary layer airflow received within the aft engine during operation of the aircraft (10), to guide the flow of boundary layer airflow into the engine more smoothly, or to reduce a distortion on the engine.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP4292939A2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP4292939A2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP4292939A23</originalsourceid><addsrcrecordid>eNrjZJD3c3R29fFxVXDzD1Jw9FNw9AxyDnJ0C1EAYTdHPx4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGJkaWRpbOloZEyEEgBd6yDC</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>NACELLE FOR AN AIRCRAFT AFT FAN</title><source>esp@cenet</source><creator>WOOD, Trevor Howard ; RAMAKRISHNAN, Kishore</creator><creatorcontrib>WOOD, Trevor Howard ; RAMAKRISHNAN, Kishore</creatorcontrib><description>An aircraft (10) is provided including a fuselage (12) extending between a forward end (16) and an aft end (18). An aft engine is mounted to the fuselage (12) at the aft end of the fuselage (18). The aft engine includes a nacelle (306) having a forward section. An airflow duct (344) is also provided extending at least partially through the nacelle (306) and including an opening on the forward section of the nacelle (330). The opening is configured for providing an airflow to, or receiving an airflow from, the forward section of the nacelle (306) to increase an amount of, e.g., boundary layer airflow received within the aft engine during operation of the aircraft (10), to guide the flow of boundary layer airflow into the engine more smoothly, or to reduce a distortion on the engine.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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&amp;date=20231220&amp;DB=EPODOC&amp;CC=EP&amp;NR=4292939A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20231220&amp;DB=EPODOC&amp;CC=EP&amp;NR=4292939A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WOOD, Trevor Howard</creatorcontrib><creatorcontrib>RAMAKRISHNAN, Kishore</creatorcontrib><title>NACELLE FOR AN AIRCRAFT AFT FAN</title><description>An aircraft (10) is provided including a fuselage (12) extending between a forward end (16) and an aft end (18). An aft engine is mounted to the fuselage (12) at the aft end of the fuselage (18). The aft engine includes a nacelle (306) having a forward section. An airflow duct (344) is also provided extending at least partially through the nacelle (306) and including an opening on the forward section of the nacelle (330). The opening is configured for providing an airflow to, or receiving an airflow from, the forward section of the nacelle (306) to increase an amount of, e.g., boundary layer airflow received within the aft engine during operation of the aircraft (10), to guide the flow of boundary layer airflow into the engine more smoothly, or to reduce a distortion on the engine.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJD3c3R29fFxVXDzD1Jw9FNw9AxyDnJ0C1EAYTdHPx4G1rTEnOJUXijNzaDg5hri7KGbWpAfn1pckJicmpdaEu8aYGJkaWRpbOloZEyEEgBd6yDC</recordid><startdate>20231220</startdate><enddate>20231220</enddate><creator>WOOD, Trevor Howard</creator><creator>RAMAKRISHNAN, Kishore</creator><scope>EVB</scope></search><sort><creationdate>20231220</creationdate><title>NACELLE FOR AN AIRCRAFT AFT FAN</title><author>WOOD, Trevor Howard ; RAMAKRISHNAN, Kishore</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP4292939A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>WOOD, Trevor Howard</creatorcontrib><creatorcontrib>RAMAKRISHNAN, Kishore</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WOOD, Trevor Howard</au><au>RAMAKRISHNAN, Kishore</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>NACELLE FOR AN AIRCRAFT AFT FAN</title><date>2023-12-20</date><risdate>2023</risdate><abstract>An aircraft (10) is provided including a fuselage (12) extending between a forward end (16) and an aft end (18). An aft engine is mounted to the fuselage (12) at the aft end of the fuselage (18). The aft engine includes a nacelle (306) having a forward section. An airflow duct (344) is also provided extending at least partially through the nacelle (306) and including an opening on the forward section of the nacelle (330). The opening is configured for providing an airflow to, or receiving an airflow from, the forward section of the nacelle (306) to increase an amount of, e.g., boundary layer airflow received within the aft engine during operation of the aircraft (10), to guide the flow of boundary layer airflow into the engine more smoothly, or to reduce a distortion on the engine.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP4292939A2
source esp@cenet
subjects AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title NACELLE FOR AN AIRCRAFT AFT FAN
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T10%3A46%3A16IST&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=WOOD,%20Trevor%20Howard&rft.date=2023-12-20&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP4292939A2%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