Aircraft flap assembly

Aircraft flap assembly

A flap assembly attached to the undersurface of a wing of an aircraft. The size of the flap has been precisely designed in view of the size of the wing of the aircraft and also precisely located relative to the wing of the aircraft so that the flap can be used as an air brake to substantially slow t...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: NAHAS, ROGER A
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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 NAHAS
ROGER A
description A flap assembly attached to the undersurface of a wing of an aircraft. The size of the flap has been precisely designed in view of the size of the wing of the aircraft and also precisely located relative to the wing of the aircraft so that the flap can be used as an air brake to substantially slow the speed of the aircraft when landing without loss of lift thereby utilizing substantially less runway during landing. Also, the flap assembly can be deployed to increase lift for the purpose of utilizing substantially less runway during take-off.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US4881703A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US4881703A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US4881703A3</originalsourceid><addsrcrecordid>eNrjZBBzzCxKLkpMK1FIy0ksUEgsLk7NTcqp5GFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8aHBJhYWhuYGxo7GhFUAAB2UINQ</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Aircraft flap assembly</title><source>esp@cenet</source><creator>NAHAS; ROGER A</creator><creatorcontrib>NAHAS; ROGER A</creatorcontrib><description>A flap assembly attached to the undersurface of a wing of an aircraft. The size of the flap has been precisely designed in view of the size of the wing of the aircraft and also precisely located relative to the wing of the aircraft so that the flap can be used as an air brake to substantially slow the speed of the aircraft when landing without loss of lift thereby utilizing substantially less runway during landing. Also, the flap assembly can be deployed to increase lift for the purpose of utilizing substantially less runway during take-off.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>1989</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=19891121&amp;DB=EPODOC&amp;CC=US&amp;NR=4881703A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=19891121&amp;DB=EPODOC&amp;CC=US&amp;NR=4881703A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NAHAS; ROGER A</creatorcontrib><title>Aircraft flap assembly</title><description>A flap assembly attached to the undersurface of a wing of an aircraft. The size of the flap has been precisely designed in view of the size of the wing of the aircraft and also precisely located relative to the wing of the aircraft so that the flap can be used as an air brake to substantially slow the speed of the aircraft when landing without loss of lift thereby utilizing substantially less runway during landing. Also, the flap assembly can be deployed to increase lift for the purpose of utilizing substantially less runway during take-off.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1989</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBBzzCxKLkpMK1FIy0ksUEgsLk7NTcqp5GFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8aHBJhYWhuYGxo7GhFUAAB2UINQ</recordid><startdate>19891121</startdate><enddate>19891121</enddate><creator>NAHAS; ROGER A</creator><scope>EVB</scope></search><sort><creationdate>19891121</creationdate><title>Aircraft flap assembly</title><author>NAHAS; ROGER A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US4881703A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1989</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>NAHAS; ROGER A</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>NAHAS; ROGER A</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Aircraft flap assembly</title><date>1989-11-21</date><risdate>1989</risdate><abstract>A flap assembly attached to the undersurface of a wing of an aircraft. The size of the flap has been precisely designed in view of the size of the wing of the aircraft and also precisely located relative to the wing of the aircraft so that the flap can be used as an air brake to substantially slow the speed of the aircraft when landing without loss of lift thereby utilizing substantially less runway during landing. Also, the flap assembly can be deployed to increase lift for the purpose of utilizing substantially less runway during take-off.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US4881703A
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Aircraft flap assembly
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2024-12-28T03%3A00%3A33IST&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=NAHAS;%20ROGER%20A&rft.date=1989-11-21&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS4881703A%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