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...
Gespeichert in:
Hauptverfasser: | , , , , , |
---|---|
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&date=20181002&DB=EPODOC&CC=US&NR=10086934B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181002&DB=EPODOC&CC=US&NR=10086934B2$$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 |