TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY
An aircraft (101) including a nacelle (200) disposed at a fixed location relative a wing member (109); a proprotor housing (202) coupled to the nacelle (200), the proprotor housing (202) configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door (204)...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
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 | SMITH, Clegg REINHART, Michael E WILLIAMS, Jeffrey M ROSS, Brent C PRAVANH, Nick |
description | An aircraft (101) including a nacelle (200) disposed at a fixed location relative a wing member (109); a proprotor housing (202) coupled to the nacelle (200), the proprotor housing (202) configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door (204) pivotably coupled to the proprotor housing (202); and a linkage (213) to connect the door (204) and the nacelle (200), the linkage (213) configured to move with the door (204) from a closed position when the proprotor housing (202) is in a horizontal orientation to an open position when the proprotor housing (202) is in a non-horizontal orientation. In some embodiments, there can be a hinge member (208) for hingedly coupling the door (204) to the proprotor and/or nacelle (200). In other embodiments, the door (204) includes a flexure portion (704m, 704n). In some embodiments, the nacelle (200) includes a plurality of doors (804). In other embodiments, proprotor includes a forward portion and a stationary aft portion; wherein the forward portion is configured to selectively pivot. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP3626612A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP3626612A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP3626612A13</originalsourceid><addsrcrecordid>eNrjZNAL8fQJCfIP8Q9ScPQMcg5ydAtRAHIdQzz93BUCgvwDoHLBwa6-Tj6RPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2MzIzMzQyNHQmAglAN1EJe8</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY</title><source>esp@cenet</source><creator>SMITH, Clegg ; REINHART, Michael E ; WILLIAMS, Jeffrey M ; ROSS, Brent C ; PRAVANH, Nick</creator><creatorcontrib>SMITH, Clegg ; REINHART, Michael E ; WILLIAMS, Jeffrey M ; ROSS, Brent C ; PRAVANH, Nick</creatorcontrib><description>An aircraft (101) including a nacelle (200) disposed at a fixed location relative a wing member (109); a proprotor housing (202) coupled to the nacelle (200), the proprotor housing (202) configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door (204) pivotably coupled to the proprotor housing (202); and a linkage (213) to connect the door (204) and the nacelle (200), the linkage (213) configured to move with the door (204) from a closed position when the proprotor housing (202) is in a horizontal orientation to an open position when the proprotor housing (202) is in a non-horizontal orientation. In some embodiments, there can be a hinge member (208) for hingedly coupling the door (204) to the proprotor and/or nacelle (200). In other embodiments, the door (204) includes a flexure portion (704m, 704n). In some embodiments, the nacelle (200) includes a plurality of doors (804). In other embodiments, proprotor includes a forward portion and a stationary aft portion; wherein the forward portion is configured to selectively pivot.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; HELICOPTERS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2020</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=20200325&DB=EPODOC&CC=EP&NR=3626612A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76419</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200325&DB=EPODOC&CC=EP&NR=3626612A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SMITH, Clegg</creatorcontrib><creatorcontrib>REINHART, Michael E</creatorcontrib><creatorcontrib>WILLIAMS, Jeffrey M</creatorcontrib><creatorcontrib>ROSS, Brent C</creatorcontrib><creatorcontrib>PRAVANH, Nick</creatorcontrib><title>TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY</title><description>An aircraft (101) including a nacelle (200) disposed at a fixed location relative a wing member (109); a proprotor housing (202) coupled to the nacelle (200), the proprotor housing (202) configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door (204) pivotably coupled to the proprotor housing (202); and a linkage (213) to connect the door (204) and the nacelle (200), the linkage (213) configured to move with the door (204) from a closed position when the proprotor housing (202) is in a horizontal orientation to an open position when the proprotor housing (202) is in a non-horizontal orientation. In some embodiments, there can be a hinge member (208) for hingedly coupling the door (204) to the proprotor and/or nacelle (200). In other embodiments, the door (204) includes a flexure portion (704m, 704n). In some embodiments, the nacelle (200) includes a plurality of doors (804). In other embodiments, proprotor includes a forward portion and a stationary aft portion; wherein the forward portion is configured to selectively pivot.</description><subject>AEROPLANES</subject><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>HELICOPTERS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNAL8fQJCfIP8Q9ScPQMcg5ydAtRAHIdQzz93BUCgvwDoHLBwa6-Tj6RPAysaYk5xam8UJqbQcHNNcTZQze1ID8-tbggMTk1L7Uk3jXA2MzIzMzQyNHQmAglAN1EJe8</recordid><startdate>20200325</startdate><enddate>20200325</enddate><creator>SMITH, Clegg</creator><creator>REINHART, Michael E</creator><creator>WILLIAMS, Jeffrey M</creator><creator>ROSS, Brent C</creator><creator>PRAVANH, Nick</creator><scope>EVB</scope></search><sort><creationdate>20200325</creationdate><title>TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY</title><author>SMITH, Clegg ; REINHART, Michael E ; WILLIAMS, Jeffrey M ; ROSS, Brent C ; PRAVANH, Nick</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3626612A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2020</creationdate><topic>AEROPLANES</topic><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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>SMITH, Clegg</creatorcontrib><creatorcontrib>REINHART, Michael E</creatorcontrib><creatorcontrib>WILLIAMS, Jeffrey M</creatorcontrib><creatorcontrib>ROSS, Brent C</creatorcontrib><creatorcontrib>PRAVANH, Nick</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SMITH, Clegg</au><au>REINHART, Michael E</au><au>WILLIAMS, Jeffrey M</au><au>ROSS, Brent C</au><au>PRAVANH, Nick</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY</title><date>2020-03-25</date><risdate>2020</risdate><abstract>An aircraft (101) including a nacelle (200) disposed at a fixed location relative a wing member (109); a proprotor housing (202) coupled to the nacelle (200), the proprotor housing (202) configured to selectively rotate between a horizontal orientation and a non-horizontal orientation; a door (204) pivotably coupled to the proprotor housing (202); and a linkage (213) to connect the door (204) and the nacelle (200), the linkage (213) configured to move with the door (204) from a closed position when the proprotor housing (202) is in a horizontal orientation to an open position when the proprotor housing (202) is in a non-horizontal orientation. In some embodiments, there can be a hinge member (208) for hingedly coupling the door (204) to the proprotor and/or nacelle (200). In other embodiments, the door (204) includes a flexure portion (704m, 704n). In some embodiments, the nacelle (200) includes a plurality of doors (804). In other embodiments, proprotor includes a forward portion and a stationary aft portion; wherein the forward portion is configured to selectively pivot.</abstract><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng ; fre ; ger |
recordid | cdi_epo_espacenet_EP3626612A1 |
source | esp@cenet |
subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
title | TILTROTOR AIRCRAFT ROTATING PROPROTOR ASSEMBLY |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-07T23%3A30%3A56IST&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=SMITH,%20Clegg&rft.date=2020-03-25&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP3626612A1%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 |