TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER

TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER

The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the plate so as to respond to a retainer plate disbond.

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: MEYER, LEON M, LAY, RICHARD C, SCHMALING, DAVID N
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 MEYER, LEON M
LAY, RICHARD C
SCHMALING, DAVID N
description The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the plate so as to respond to a retainer plate disbond.
format Patent
fullrecord <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2367719A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2367719A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2367719A13</originalsourceid><addsrcrecordid>eNqNyrEKwjAQANAsDqL-w_2AQy1YHC_tWQ8uiSS3dCqlnJNoof4_Ln6A01ve1vWKLJCTpgxesCPAUih4GQBjByRYNAXK3IInzBx7KENRChCScoogHFgp793mMT1XO_zcObiStrejLe_R1mWa7WWfke6n-tw01QWr-o_yBYLwLEg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER</title><source>esp@cenet</source><creator>MEYER, LEON M ; LAY, RICHARD C ; SCHMALING, DAVID N</creator><creatorcontrib>MEYER, LEON M ; LAY, RICHARD C ; SCHMALING, DAVID N</creatorcontrib><description>The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the plate so as to respond to a retainer plate disbond.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2011</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=20110928&amp;DB=EPODOC&amp;CC=EP&amp;NR=2367719A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25551,76302</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20110928&amp;DB=EPODOC&amp;CC=EP&amp;NR=2367719A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MEYER, LEON M</creatorcontrib><creatorcontrib>LAY, RICHARD C</creatorcontrib><creatorcontrib>SCHMALING, DAVID N</creatorcontrib><title>TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER</title><description>The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the plate so as to respond to a retainer plate disbond.</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>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyrEKwjAQANAsDqL-w_2AQy1YHC_tWQ8uiSS3dCqlnJNoof4_Ln6A01ve1vWKLJCTpgxesCPAUih4GQBjByRYNAXK3IInzBx7KENRChCScoogHFgp793mMT1XO_zcObiStrejLe_R1mWa7WWfke6n-tw01QWr-o_yBYLwLEg</recordid><startdate>20110928</startdate><enddate>20110928</enddate><creator>MEYER, LEON M</creator><creator>LAY, RICHARD C</creator><creator>SCHMALING, DAVID N</creator><scope>EVB</scope></search><sort><creationdate>20110928</creationdate><title>TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER</title><author>MEYER, LEON M ; LAY, RICHARD C ; SCHMALING, DAVID N</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2367719A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2011</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>MEYER, LEON M</creatorcontrib><creatorcontrib>LAY, RICHARD C</creatorcontrib><creatorcontrib>SCHMALING, DAVID N</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MEYER, LEON M</au><au>LAY, RICHARD C</au><au>SCHMALING, DAVID N</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER</title><date>2011-09-28</date><risdate>2011</risdate><abstract>The invention relates to a backing plate used for an elastomeric bearing system, the backing plate comprising a plate which defines an at least partial annulus about an axis, a motion limiter and a redundant pivot which extend from the plate so as to respond to a retainer plate disbond.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng ; fre ; ger
recordid cdi_epo_espacenet_EP2367719A1
source esp@cenet
subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title TAIL ROTOR BLADE ASSEMBLY AND ELASTOMERIC BEARING SYSTEM MOTION LIMITER
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-15T22%3A14%3A38IST&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=MEYER,%20LEON%20M&rft.date=2011-09-28&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EEP2367719A1%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