Engine assembly for aircraft comprising an engine and a mounting device for such an engine
The invention relates to an aircraft engine assembly (1) including an engine (6) and an engine mounting device (4), the mounting device being designed to be inserted between a wing of the aircraft and the engine, and comprising a rigid structure (8) and means of mounting the engine onto the rigid st...
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| creator | KOENIG NICOLAS DIOCHON LIONEL EL HAMMAMI SAMIR DUMAS JEAN-BAPTISTE LE LOUVETEL-POILLY JULIE |
| description | The invention relates to an aircraft engine assembly (1) including an engine (6) and an engine mounting device (4), the mounting device being designed to be inserted between a wing of the aircraft and the engine, and comprising a rigid structure (8) and means of mounting the engine onto the rigid structure, the mounting means comprising a forward fastener (10) and an aft fastener (12). According to the invention, the aft fastener comprises two aft half-fasteners (12a) that will each resist at least the forces applied along a longitudinal direction (X) of the engine, and the two aft half-fasteners are arranged so that a horizontal plane (P) passing through a longitudinal axis (5) of the engine passes through each of them. |
| format | Patent |
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According to the invention, the aft fastener comprises two aft half-fasteners (12a) that will each resist at least the forces applied along a longitudinal direction (X) of the engine, and the two aft half-fasteners are arranged so that a horizontal plane (P) passing through a longitudinal axis (5) of the engine passes through each of them.</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>2010</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=20100316&DB=EPODOC&CC=US&NR=7677493B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20100316&DB=EPODOC&CC=US&NR=7677493B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KOENIG NICOLAS</creatorcontrib><creatorcontrib>DIOCHON LIONEL</creatorcontrib><creatorcontrib>EL HAMMAMI SAMIR</creatorcontrib><creatorcontrib>DUMAS JEAN-BAPTISTE</creatorcontrib><creatorcontrib>LE LOUVETEL-POILLY JULIE</creatorcontrib><title>Engine assembly for aircraft comprising an engine and a mounting device for such an engine</title><description>The invention relates to an aircraft engine assembly (1) including an engine (6) and an engine mounting device (4), the mounting device being designed to be inserted between a wing of the aircraft and the engine, and comprising a rigid structure (8) and means of mounting the engine onto the rigid structure, the mounting means comprising a forward fastener (10) and an aft fastener (12). According to the invention, the aft fastener comprises two aft half-fasteners (12a) that will each resist at least the forces applied along a longitudinal direction (X) of the engine, and the two aft half-fasteners are arranged so that a horizontal plane (P) passing through a longitudinal axis (5) of the engine passes through each of them.</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>2010</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIhyzUvPzEtVSCwuTs1NyqlUSMsvUkjMLEouSkwrUUjOzy0oyizOzEtXSMxTSIUqzUtRSFTIzS_NKwFJpKSWZSangvUVlyZnIBTyMLCmJeYUp_JCaW4GBTfXEGcP3dSC_PjU4oLE5NS81JL40GBzM3NzE0tjJyNjIpQAAIJ2OmY</recordid><startdate>20100316</startdate><enddate>20100316</enddate><creator>KOENIG NICOLAS</creator><creator>DIOCHON LIONEL</creator><creator>EL HAMMAMI SAMIR</creator><creator>DUMAS JEAN-BAPTISTE</creator><creator>LE LOUVETEL-POILLY JULIE</creator><scope>EVB</scope></search><sort><creationdate>20100316</creationdate><title>Engine assembly for aircraft comprising an engine and a mounting device for such an engine</title><author>KOENIG NICOLAS ; DIOCHON LIONEL ; EL HAMMAMI SAMIR ; DUMAS JEAN-BAPTISTE ; LE LOUVETEL-POILLY JULIE</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US7677493B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2010</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>KOENIG NICOLAS</creatorcontrib><creatorcontrib>DIOCHON LIONEL</creatorcontrib><creatorcontrib>EL HAMMAMI SAMIR</creatorcontrib><creatorcontrib>DUMAS JEAN-BAPTISTE</creatorcontrib><creatorcontrib>LE LOUVETEL-POILLY JULIE</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KOENIG NICOLAS</au><au>DIOCHON LIONEL</au><au>EL HAMMAMI SAMIR</au><au>DUMAS JEAN-BAPTISTE</au><au>LE LOUVETEL-POILLY JULIE</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Engine assembly for aircraft comprising an engine and a mounting device for such an engine</title><date>2010-03-16</date><risdate>2010</risdate><abstract>The invention relates to an aircraft engine assembly (1) including an engine (6) and an engine mounting device (4), the mounting device being designed to be inserted between a wing of the aircraft and the engine, and comprising a rigid structure (8) and means of mounting the engine onto the rigid structure, the mounting means comprising a forward fastener (10) and an aft fastener (12). According to the invention, the aft fastener comprises two aft half-fasteners (12a) that will each resist at least the forces applied along a longitudinal direction (X) of the engine, and the two aft half-fasteners are arranged so that a horizontal plane (P) passing through a longitudinal axis (5) of the engine passes through each of them.</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 | Engine assembly for aircraft comprising an engine and a mounting device for such an engine |
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