Device for attaching an aircraft engine and aircraft comprising at least one such device

Device for attaching an aircraft engine and aircraft comprising at least one such device

An attachment device for an aircraft engine that includes a rigid structure and an attachment mechanism of the engine to the rigid structure. The attachment mechanism includes a device reacting to thrust forces generated by the engine, the reacting device including two link rods mechanically connect...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Combes, Stephane, Rovatti, Didier
Format: Patent
Sprache:eng
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 Combes, Stephane
Rovatti, Didier
description An attachment device for an aircraft engine that includes a rigid structure and an attachment mechanism of the engine to the rigid structure. The attachment mechanism includes a device reacting to thrust forces generated by the engine, the reacting device including two link rods mechanically connected to a balance beam at a rear end by a first mechanical connection, a main fitting fixed to the rigid structure to which the balance beam is mechanically connected, and two additional fittings fixed to the rigid structure to which the link rods are mechanically connected with play. The mechanical connections between the balance beam and the main fitting and between the link rods and the additional fittings each include a pin orthogonal to a mid-plane of transmission of the forces.
format Patent
fullrecord <record><control><sourceid>uspatents_EFH</sourceid><recordid>TN_cdi_uspatents_grants_08146856</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>08146856</sourcerecordid><originalsourceid>FETCH-uspatents_grants_081468563</originalsourceid><addsrcrecordid>eNrjZIhwSS3LTE5VSMsvUkgsKUlMzsjMS1dIzFNIzCxKLkpMK1FIzUvPzEsFCqUgxJLzcwuKMovBSksUclITi0sU8oGKikuTMxRSwCbyMLCmJeYUp_JCaW4GBTfXEGcP3dLigsSS1LyS4vj0okQQZWBhaGJmYWpmTIQSABTROsE</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Device for attaching an aircraft engine and aircraft comprising at least one such device</title><source>USPTO Issued Patents</source><creator>Combes, Stephane ; Rovatti, Didier</creator><creatorcontrib>Combes, Stephane ; Rovatti, Didier ; Airbus Operations SAS</creatorcontrib><description>An attachment device for an aircraft engine that includes a rigid structure and an attachment mechanism of the engine to the rigid structure. The attachment mechanism includes a device reacting to thrust forces generated by the engine, the reacting device including two link rods mechanically connected to a balance beam at a rear end by a first mechanical connection, a main fitting fixed to the rigid structure to which the balance beam is mechanically connected, and two additional fittings fixed to the rigid structure to which the link rods are mechanically connected with play. The mechanical connections between the balance beam and the main fitting and between the link rods and the additional fittings each include a pin orthogonal to a mid-plane of transmission of the forces.</description><language>eng</language><creationdate>2012</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8146856$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,776,798,881,64012</link.rule.ids><linktorsrc>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8146856$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Combes, Stephane</creatorcontrib><creatorcontrib>Rovatti, Didier</creatorcontrib><creatorcontrib>Airbus Operations SAS</creatorcontrib><title>Device for attaching an aircraft engine and aircraft comprising at least one such device</title><description>An attachment device for an aircraft engine that includes a rigid structure and an attachment mechanism of the engine to the rigid structure. The attachment mechanism includes a device reacting to thrust forces generated by the engine, the reacting device including two link rods mechanically connected to a balance beam at a rear end by a first mechanical connection, a main fitting fixed to the rigid structure to which the balance beam is mechanically connected, and two additional fittings fixed to the rigid structure to which the link rods are mechanically connected with play. The mechanical connections between the balance beam and the main fitting and between the link rods and the additional fittings each include a pin orthogonal to a mid-plane of transmission of the forces.</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2012</creationdate><recordtype>patent</recordtype><sourceid>EFH</sourceid><recordid>eNrjZIhwSS3LTE5VSMsvUkgsKUlMzsjMS1dIzFNIzCxKLkpMK1FIzUvPzEsFCqUgxJLzcwuKMovBSksUclITi0sU8oGKikuTMxRSwCbyMLCmJeYUp_JCaW4GBTfXEGcP3dLigsSS1LyS4vj0okQQZWBhaGJmYWpmTIQSABTROsE</recordid><startdate>20120403</startdate><enddate>20120403</enddate><creator>Combes, Stephane</creator><creator>Rovatti, Didier</creator><scope>EFH</scope></search><sort><creationdate>20120403</creationdate><title>Device for attaching an aircraft engine and aircraft comprising at least one such device</title><author>Combes, Stephane ; Rovatti, Didier</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_grants_081468563</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2012</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Combes, Stephane</creatorcontrib><creatorcontrib>Rovatti, Didier</creatorcontrib><creatorcontrib>Airbus Operations SAS</creatorcontrib><collection>USPTO Issued Patents</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Combes, Stephane</au><au>Rovatti, Didier</au><aucorp>Airbus Operations SAS</aucorp><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Device for attaching an aircraft engine and aircraft comprising at least one such device</title><date>2012-04-03</date><risdate>2012</risdate><abstract>An attachment device for an aircraft engine that includes a rigid structure and an attachment mechanism of the engine to the rigid structure. The attachment mechanism includes a device reacting to thrust forces generated by the engine, the reacting device including two link rods mechanically connected to a balance beam at a rear end by a first mechanical connection, a main fitting fixed to the rigid structure to which the balance beam is mechanically connected, and two additional fittings fixed to the rigid structure to which the link rods are mechanically connected with play. The mechanical connections between the balance beam and the main fitting and between the link rods and the additional fittings each include a pin orthogonal to a mid-plane of transmission of the forces.</abstract><oa>free_for_read</oa></addata></record>
fulltext fulltext_linktorsrc
identifier
ispartof
issn
language eng
recordid cdi_uspatents_grants_08146856
source USPTO Issued Patents
title Device for attaching an aircraft engine and aircraft comprising at least one such device
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-09T10%3A35%3A00IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-uspatents_EFH&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=Combes,%20Stephane&rft.aucorp=Airbus%20Operations%20SAS&rft.date=2012-04-03&rft_id=info:doi/&rft_dat=%3Cuspatents_EFH%3E08146856%3C/uspatents_EFH%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