AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ENGINE AND A MOUNT FOR SAID ENGINE
The invention relates to an aircraft engine assembly (1) comprising an engine (2) and an engine mount (4), this engine mount including firstly a rigid structure (10) comprising a box (24) and secondly a mounting system (11) positioned between the engine and the rigid structure, this mounting system...
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| creator | LAFONT, LAURENT JOURNADE, FREDERIC |
| description | The invention relates to an aircraft engine assembly (1) comprising an engine (2) and an engine mount (4), this engine mount including firstly a rigid structure (10) comprising a box (24) and secondly a mounting system (11) positioned between the engine and the rigid structure, this mounting system notably comprising an aft attachment (8), the assembly also being provided with a thermal protection system (58) for the box, comprising a preferably ventilated duct (60) forming a heat barrier and extending between this box and the engine. According to the invention, the duct extends rearward beyond the aft engine attachment.
L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un moteur (2) et un mât d'accrochage (4), ce mât comportant d'une part une structure rigide (10) comprenant un caisson (24) et d'autre part un système de montage (11) interposé entre le moteur et la structure rigide, ce système de montage comportant notamment une attache arrière (8), l'ensemble étant en outre pourvu d'un système de protection thermique (58) du caisson comportant un conduit (60) de préférence ventilé et formant une barrière thermique et s'étendant entre ce caisson et le moteur. Selon l'invention, le conduit s'étend vers l'arrière au-delà de l'attache moteur arrière. |
| format | Patent |
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L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un moteur (2) et un mât d'accrochage (4), ce mât comportant d'une part une structure rigide (10) comprenant un caisson (24) et d'autre part un système de montage (11) interposé entre le moteur et la structure rigide, ce système de montage comportant notamment une attache arrière (8), l'ensemble étant en outre pourvu d'un système de protection thermique (58) du caisson comportant un conduit (60) de préférence ventilé et formant une barrière thermique et s'étendant entre ce caisson et le moteur. Selon l'invention, le conduit s'étend vers l'arrière au-delà de l'attache moteur arrière.</description><language>eng ; fre</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>2013</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=20131112&DB=EPODOC&CC=CA&NR=2624002C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20131112&DB=EPODOC&CC=CA&NR=2624002C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LAFONT, LAURENT</creatorcontrib><creatorcontrib>JOURNADE, FREDERIC</creatorcontrib><title>AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ENGINE AND A MOUNT FOR SAID ENGINE</title><description>The invention relates to an aircraft engine assembly (1) comprising an engine (2) and an engine mount (4), this engine mount including firstly a rigid structure (10) comprising a box (24) and secondly a mounting system (11) positioned between the engine and the rigid structure, this mounting system notably comprising an aft attachment (8), the assembly also being provided with a thermal protection system (58) for the box, comprising a preferably ventilated duct (60) forming a heat barrier and extending between this box and the engine. According to the invention, the duct extends rearward beyond the aft engine attachment.
L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un moteur (2) et un mât d'accrochage (4), ce mât comportant d'une part une structure rigide (10) comprenant un caisson (24) et d'autre part un système de montage (11) interposé entre le moteur et la structure rigide, ce système de montage comportant notamment une attache arrière (8), l'ensemble étant en outre pourvu d'un système de protection thermique (58) du caisson comportant un conduit (60) de préférence ventilé et formant une barrière thermique et s'étendant entre ce caisson et le moteur. Selon l'invention, le conduit s'étend vers l'arrière au-delà de l'attache moteur arrière.</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>2013</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPB09AxyDnJ0C1Fw9XP39HNVcAwOdvV18olUcPb3DQjyDPb0c1dw9IPL-rkoOCr4-of6hSi4-QcpBDt6ukDleBhY0xJzilN5oTQ3g7yba4izh25qQX58anFBYnJqXmpJvLOjkZmRiYGBkbMxYRUASmwrnQ</recordid><startdate>20131112</startdate><enddate>20131112</enddate><creator>LAFONT, LAURENT</creator><creator>JOURNADE, FREDERIC</creator><scope>EVB</scope></search><sort><creationdate>20131112</creationdate><title>AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ENGINE AND A MOUNT FOR SAID ENGINE</title><author>LAFONT, LAURENT ; JOURNADE, FREDERIC</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2624002C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2013</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>LAFONT, LAURENT</creatorcontrib><creatorcontrib>JOURNADE, FREDERIC</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LAFONT, LAURENT</au><au>JOURNADE, FREDERIC</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>AIRCRAFT ENGINE ASSEMBLY COMPRISING AN ENGINE AND A MOUNT FOR SAID ENGINE</title><date>2013-11-12</date><risdate>2013</risdate><abstract>The invention relates to an aircraft engine assembly (1) comprising an engine (2) and an engine mount (4), this engine mount including firstly a rigid structure (10) comprising a box (24) and secondly a mounting system (11) positioned between the engine and the rigid structure, this mounting system notably comprising an aft attachment (8), the assembly also being provided with a thermal protection system (58) for the box, comprising a preferably ventilated duct (60) forming a heat barrier and extending between this box and the engine. According to the invention, the duct extends rearward beyond the aft engine attachment.
L'invention se rapporte à un ensemble moteur (1) pour aéronef comprenant un moteur (2) et un mât d'accrochage (4), ce mât comportant d'une part une structure rigide (10) comprenant un caisson (24) et d'autre part un système de montage (11) interposé entre le moteur et la structure rigide, ce système de montage comportant notamment une attache arrière (8), l'ensemble étant en outre pourvu d'un système de protection thermique (58) du caisson comportant un conduit (60) de préférence ventilé et formant une barrière thermique et s'étendant entre ce caisson et le moteur. Selon l'invention, le conduit s'étend vers l'arrière au-delà de l'attache moteur arrière.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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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 ASSEMBLY COMPRISING AN ENGINE AND A MOUNT FOR SAID ENGINE |
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