Composite rotor system using two race track style cantilevered yokes

A hub system comprises at least one yoke, at least one shear bearing, and at least one mast adapter. The at least one mast adapter is configured to support the at least one yoke and the at least one shear bearing, and the at least one yoke has a flapping hinge that is non-coincident with a flapping...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Wardlaw, Robert Patrick, Sutton, Drew Alan, Maresh, Andrew, Stamps, Frank Bradley, Haldeman, Andrew, Tisdale, Patrick Ryan
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 Wardlaw, Robert Patrick
Sutton, Drew Alan
Maresh, Andrew
Stamps, Frank Bradley
Haldeman, Andrew
Tisdale, Patrick Ryan
description A hub system comprises at least one yoke, at least one shear bearing, and at least one mast adapter. The at least one mast adapter is configured to support the at least one yoke and the at least one shear bearing, and the at least one yoke has a flapping hinge that is non-coincident with a flapping hinge of the at least one shear bearing. Another hub system comprises a stacked yoke and a mast adapter. The mast adapter is configured to transfer rotation from a rotor mast to the hub system to rotate the hub system about a central axis of rotation. The mast adapter is further configured to support the stacked yoke such that each yoke in the stacked yoke is configured to accommodate at least some amount of rotation about an axis that is perpendicular to or about perpendicular to the central axis of rotation.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_US10086934B2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>US10086934B2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_US10086934B23</originalsourceid><addsrcrecordid>eNrjZHBxzs8tyC_OLElVKMovyS9SKK4sLknNVSgtzsxLVygpz1coSkxOVSgBktkKxSWVOakKyYl5JZk5qWWpRakpCpX52anFPAysaYk5xam8UJqbQdHNNcTZQze1ID8-tbgAaEJeakl8aLChgYGFmaWxiZORMTFqAAG1M40</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Composite rotor system using two race track style cantilevered yokes</title><source>esp@cenet</source><creator>Wardlaw, Robert Patrick ; Sutton, Drew Alan ; Maresh, Andrew ; Stamps, Frank Bradley ; Haldeman, Andrew ; Tisdale, Patrick Ryan</creator><creatorcontrib>Wardlaw, Robert Patrick ; Sutton, Drew Alan ; Maresh, Andrew ; Stamps, Frank Bradley ; Haldeman, Andrew ; Tisdale, Patrick Ryan</creatorcontrib><description>A hub system comprises at least one yoke, at least one shear bearing, and at least one mast adapter. The at least one mast adapter is configured to support the at least one yoke and the at least one shear bearing, and the at least one yoke has a flapping hinge that is non-coincident with a flapping hinge of the at least one shear bearing. Another hub system comprises a stacked yoke and a mast adapter. The mast adapter is configured to transfer rotation from a rotor mast to the hub system to rotate the hub system about a central axis of rotation. The mast adapter is further configured to support the stacked yoke such that each yoke in the stacked yoke is configured to accommodate at least some amount of rotation about an axis that is perpendicular to or about perpendicular to the central axis of rotation.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</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&amp;date=20181002&amp;DB=EPODOC&amp;CC=US&amp;NR=10086934B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20181002&amp;DB=EPODOC&amp;CC=US&amp;NR=10086934B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Wardlaw, Robert Patrick</creatorcontrib><creatorcontrib>Sutton, Drew Alan</creatorcontrib><creatorcontrib>Maresh, Andrew</creatorcontrib><creatorcontrib>Stamps, Frank Bradley</creatorcontrib><creatorcontrib>Haldeman, Andrew</creatorcontrib><creatorcontrib>Tisdale, Patrick Ryan</creatorcontrib><title>Composite rotor system using two race track style cantilevered yokes</title><description>A hub system comprises at least one yoke, at least one shear bearing, and at least one mast adapter. The at least one mast adapter is configured to support the at least one yoke and the at least one shear bearing, and the at least one yoke has a flapping hinge that is non-coincident with a flapping hinge of the at least one shear bearing. Another hub system comprises a stacked yoke and a mast adapter. The mast adapter is configured to transfer rotation from a rotor mast to the hub system to rotate the hub system about a central axis of rotation. The mast adapter is further configured to support the stacked yoke such that each yoke in the stacked yoke is configured to accommodate at least some amount of rotation about an axis that is perpendicular to or about perpendicular to the central axis of rotation.</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>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZHBxzs8tyC_OLElVKMovyS9SKK4sLknNVSgtzsxLVygpz1coSkxOVSgBktkKxSWVOakKyYl5JZk5qWWpRakpCpX52anFPAysaYk5xam8UJqbQdHNNcTZQze1ID8-tbgAaEJeakl8aLChgYGFmaWxiZORMTFqAAG1M40</recordid><startdate>20181002</startdate><enddate>20181002</enddate><creator>Wardlaw, Robert Patrick</creator><creator>Sutton, Drew Alan</creator><creator>Maresh, Andrew</creator><creator>Stamps, Frank Bradley</creator><creator>Haldeman, Andrew</creator><creator>Tisdale, Patrick Ryan</creator><scope>EVB</scope></search><sort><creationdate>20181002</creationdate><title>Composite rotor system using two race track style cantilevered yokes</title><author>Wardlaw, Robert Patrick ; Sutton, Drew Alan ; Maresh, Andrew ; Stamps, Frank Bradley ; Haldeman, Andrew ; Tisdale, Patrick Ryan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US10086934B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</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>Wardlaw, Robert Patrick</creatorcontrib><creatorcontrib>Sutton, Drew Alan</creatorcontrib><creatorcontrib>Maresh, Andrew</creatorcontrib><creatorcontrib>Stamps, Frank Bradley</creatorcontrib><creatorcontrib>Haldeman, Andrew</creatorcontrib><creatorcontrib>Tisdale, Patrick Ryan</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Wardlaw, Robert Patrick</au><au>Sutton, Drew Alan</au><au>Maresh, Andrew</au><au>Stamps, Frank Bradley</au><au>Haldeman, Andrew</au><au>Tisdale, Patrick Ryan</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Composite rotor system using two race track style cantilevered yokes</title><date>2018-10-02</date><risdate>2018</risdate><abstract>A hub system comprises at least one yoke, at least one shear bearing, and at least one mast adapter. The at least one mast adapter is configured to support the at least one yoke and the at least one shear bearing, and the at least one yoke has a flapping hinge that is non-coincident with a flapping hinge of the at least one shear bearing. Another hub system comprises a stacked yoke and a mast adapter. The mast adapter is configured to transfer rotation from a rotor mast to the hub system to rotate the hub system about a central axis of rotation. The mast adapter is further configured to support the stacked yoke such that each yoke in the stacked yoke is configured to accommodate at least some amount of rotation about an axis that is perpendicular to or about perpendicular to the central axis of rotation.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_epo_espacenet_US10086934B2
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title Composite rotor system using two race track style cantilevered yokes
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-20T06%3A22%3A44IST&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=Wardlaw,%20Robert%20Patrick&rft.date=2018-10-02&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EUS10086934B2%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