AIRCRAFT ENGINE MOUNT COMPRISING AT LEAST ONE TRANSVERSE NUT AND AIRCRAFT COMPRISING THE SAID ENGINE MOUNT

An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a thr...

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Hauptverfasser:	GROSSEAU Nicolas, MUTIN Antoine, BOUCHET Eric, JOURNADE Frederic
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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creator	GROSSEAU Nicolas MUTIN Antoine BOUCHET Eric JOURNADE Frederic
description	An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.
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The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.</description><language>eng</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; 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=20180111&DB=EPODOC&CC=US&NR=2018009543A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180111&DB=EPODOC&CC=US&NR=2018009543A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GROSSEAU Nicolas</creatorcontrib><creatorcontrib>MUTIN Antoine</creatorcontrib><creatorcontrib>BOUCHET Eric</creatorcontrib><creatorcontrib>JOURNADE Frederic</creatorcontrib><title>AIRCRAFT ENGINE MOUNT COMPRISING AT LEAST ONE TRANSVERSE NUT AND AIRCRAFT COMPRISING THE SAID ENGINE MOUNT</title><description>An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2018</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZMhy9AxyDnJ0C1Fw9XP39HNV8PUP9QtRcPb3DQjyDPb0c1dwDFHwcXUMDlHwB8qGBDn6BYe5BgW7KviFhig4-rkowA1A0hPi4aoQ7OjpgmIoDwNrWmJOcSovlOZmUHZzDXH20E0tyI9PLS5ITE7NSy2JDw02MjC0MDCwNDUxdjQ0Jk4VAGKINw4</recordid><startdate>20180111</startdate><enddate>20180111</enddate><creator>GROSSEAU Nicolas</creator><creator>MUTIN Antoine</creator><creator>BOUCHET Eric</creator><creator>JOURNADE Frederic</creator><scope>EVB</scope></search><sort><creationdate>20180111</creationdate><title>AIRCRAFT ENGINE MOUNT COMPRISING AT LEAST ONE TRANSVERSE NUT AND AIRCRAFT COMPRISING THE SAID ENGINE MOUNT</title><author>GROSSEAU Nicolas ; MUTIN Antoine ; BOUCHET Eric ; JOURNADE Frederic</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US2018009543A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2018</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>GROSSEAU Nicolas</creatorcontrib><creatorcontrib>MUTIN Antoine</creatorcontrib><creatorcontrib>BOUCHET Eric</creatorcontrib><creatorcontrib>JOURNADE Frederic</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GROSSEAU Nicolas</au><au>MUTIN Antoine</au><au>BOUCHET Eric</au><au>JOURNADE Frederic</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT ENGINE MOUNT COMPRISING AT LEAST ONE TRANSVERSE NUT AND AIRCRAFT COMPRISING THE SAID ENGINE MOUNT</title><date>2018-01-11</date><risdate>2018</risdate><abstract>An aircraft engine mount which comprises first and second parts connected by connecting elements and wherein one of the two connected parts comprises at least one transverse hole opening onto an access face of the part and into which there open at least two passage holes each intended to house a threaded shank of one of the connecting elements. The engine mount comprises a transverse nut which comprises at least two bodies joined together each having a tapped hole configured to engage with one of the threaded shanks.</abstract><oa>free_for_read</oa></addata></record>
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subjects	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
title	AIRCRAFT ENGINE MOUNT COMPRISING AT LEAST ONE TRANSVERSE NUT AND AIRCRAFT COMPRISING THE SAID ENGINE MOUNT
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