Rotor blade and structural system for coupling the rotor blade in a rotor hub

The rotor hub (103) can include a rotor yoke (109); a grip member (119) having an inboard portion, an upper extension (137), and a lower extension (139); and a rotor blade (105) having a root end (705) coupled to the upper extension and the lower extension of the grip member with a first bolt (129),...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	MCCULLOUGH, JOHN R, WIINIKKA, MARK A, SELF, ROBERT A, GREEN, NATHAN P
Format:	Patent
Sprache:	eng ; fre ; ger
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	MCCULLOUGH, JOHN R WIINIKKA, MARK A SELF, ROBERT A GREEN, NATHAN P
description	The rotor hub (103) can include a rotor yoke (109); a grip member (119) having an inboard portion, an upper extension (137), and a lower extension (139); and a rotor blade (105) having a root end (705) coupled to the upper extension and the lower extension of the grip member with a first bolt (129), a second bolt (131), and a third bolt (133). The first bolt (129) is located on a spanwise axis of the rotor blade (105). The second bolt (131) is offset from the spanwise axis by a first chordwise distance (C1) and is offset from the first bolt (129) by a first spanwise distance (D1). The third bolt (133) is offset from the spanwise axis by a second chordwise distance (C2) and is offset from the first bolt (129) by a second spanwise distance.
format	Patent
fullrecord	<record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2848524B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2848524B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2848524B13</originalsourceid><addsrcrecordid>eNrjZPANyi_JL1JIyklMSVVIzEtRKC4pKk0uKS1KzFEoriwuSc1VSAPKJ-eXFuRk5qUrlGSkKhQhacnMU0iECmSUJvEwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXACMLEwtTIxMnQ2MilAAAV6g1gw</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Rotor blade and structural system for coupling the rotor blade in a rotor hub</title><source>esp@cenet</source><creator>MCCULLOUGH, JOHN R ; WIINIKKA, MARK A ; SELF, ROBERT A ; GREEN, NATHAN P</creator><creatorcontrib>MCCULLOUGH, JOHN R ; WIINIKKA, MARK A ; SELF, ROBERT A ; GREEN, NATHAN P</creatorcontrib><description>The rotor hub (103) can include a rotor yoke (109); a grip member (119) having an inboard portion, an upper extension (137), and a lower extension (139); and a rotor blade (105) having a root end (705) coupled to the upper extension and the lower extension of the grip member with a first bolt (129), a second bolt (131), and a third bolt (133). The first bolt (129) is located on a spanwise axis of the rotor blade (105). The second bolt (131) is offset from the spanwise axis by a first chordwise distance (C1) and is offset from the first bolt (129) by a first spanwise distance (D1). The third bolt (133) is offset from the spanwise axis by a second chordwise distance (C2) and is offset from the first bolt (129) by a second spanwise distance.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2015</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=20150923&DB=EPODOC&CC=EP&NR=2848524B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25551,76302</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150923&DB=EPODOC&CC=EP&NR=2848524B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MCCULLOUGH, JOHN R</creatorcontrib><creatorcontrib>WIINIKKA, MARK A</creatorcontrib><creatorcontrib>SELF, ROBERT A</creatorcontrib><creatorcontrib>GREEN, NATHAN P</creatorcontrib><title>Rotor blade and structural system for coupling the rotor blade in a rotor hub</title><description>The rotor hub (103) can include a rotor yoke (109); a grip member (119) having an inboard portion, an upper extension (137), and a lower extension (139); and a rotor blade (105) having a root end (705) coupled to the upper extension and the lower extension of the grip member with a first bolt (129), a second bolt (131), and a third bolt (133). The first bolt (129) is located on a spanwise axis of the rotor blade (105). The second bolt (131) is offset from the spanwise axis by a first chordwise distance (C1) and is offset from the first bolt (129) by a first spanwise distance (D1). The third bolt (133) is offset from the spanwise axis by a second chordwise distance (C2) and is offset from the first bolt (129) by a second spanwise distance.</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>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPANyi_JL1JIyklMSVVIzEtRKC4pKk0uKS1KzFEoriwuSc1VSAPKJ-eXFuRk5qUrlGSkKhQhacnMU0iECmSUJvEwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUknjXACMLEwtTIxMnQ2MilAAAV6g1gw</recordid><startdate>20150923</startdate><enddate>20150923</enddate><creator>MCCULLOUGH, JOHN R</creator><creator>WIINIKKA, MARK A</creator><creator>SELF, ROBERT A</creator><creator>GREEN, NATHAN P</creator><scope>EVB</scope></search><sort><creationdate>20150923</creationdate><title>Rotor blade and structural system for coupling the rotor blade in a rotor hub</title><author>MCCULLOUGH, JOHN R ; WIINIKKA, MARK A ; SELF, ROBERT A ; GREEN, NATHAN P</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2848524B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2015</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>MCCULLOUGH, JOHN R</creatorcontrib><creatorcontrib>WIINIKKA, MARK A</creatorcontrib><creatorcontrib>SELF, ROBERT A</creatorcontrib><creatorcontrib>GREEN, NATHAN P</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MCCULLOUGH, JOHN R</au><au>WIINIKKA, MARK A</au><au>SELF, ROBERT A</au><au>GREEN, NATHAN P</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Rotor blade and structural system for coupling the rotor blade in a rotor hub</title><date>2015-09-23</date><risdate>2015</risdate><abstract>The rotor hub (103) can include a rotor yoke (109); a grip member (119) having an inboard portion, an upper extension (137), and a lower extension (139); and a rotor blade (105) having a root end (705) coupled to the upper extension and the lower extension of the grip member with a first bolt (129), a second bolt (131), and a third bolt (133). The first bolt (129) is located on a spanwise axis of the rotor blade (105). The second bolt (131) is offset from the spanwise axis by a first chordwise distance (C1) and is offset from the first bolt (129) by a first spanwise distance (D1). The third bolt (133) is offset from the spanwise axis by a second chordwise distance (C2) and is offset from the first bolt (129) by a second spanwise distance.</abstract><oa>free_for_read</oa></addata></record>
fulltext	fulltext_linktorsrc
identifier
ispartof
issn
language	eng ; fre ; ger
recordid	cdi_epo_espacenet_EP2848524B1
source	esp@cenet
subjects	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
title	Rotor blade and structural system for coupling the rotor blade in a rotor hub
url	https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T16%3A41%3A57IST&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=MCCULLOUGH,%20JOHN%20R&rft.date=2015-09-23&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2848524B1%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