SUSPENSION D'UN TURBOREACTEUR A UN AERONEF
The suspension has a front attachment (10) with a beam transversal with respect to an axis connected to an external ferrule of an intermediate case (3) by two rods of the front attachment. A rear attachment (11) has two rods connected to another external ferrule of an exhaust case (8). A thrust tran...
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| creator | LEFORT GUILLAUME CHOUARD PIERRE ALAIN JEAN MARIE TROHEL MATHIEU JEAN PIERRE FAUVELET BENOIT MARC MICHEL |
| description | The suspension has a front attachment (10) with a beam transversal with respect to an axis connected to an external ferrule of an intermediate case (3) by two rods of the front attachment. A rear attachment (11) has two rods connected to another external ferrule of an exhaust case (8). A thrust transmission rod (12) connects the hub of the case (3) to the rear attachment. A plane formed by the rods of front attachment and the transmission rod are convergent in a point on the axis of a motor or near the axis. |
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A rear attachment (11) has two rods connected to another external ferrule of an exhaust case (8). A thrust transmission rod (12) connects the hub of the case (3) to the rear attachment. 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A plane formed by the rods of front attachment and the transmission rod are convergent in a point on the axis of a motor or near the axis.</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>eNrjZNAKDg0OcPUL9vT3U3BRD_VTCAkNcvIPcnV0DnENDVJwVAAKOboG-fu5uvEwsKYl5hSn8kJpbgYFN9cQZw_d1IL8-NTigsTk1LzUkni3ICNLI1MDQzMnQ2MilAAAEK0kQw</recordid><startdate>20100618</startdate><enddate>20100618</enddate><creator>LEFORT GUILLAUME</creator><creator>CHOUARD PIERRE ALAIN JEAN MARIE</creator><creator>TROHEL MATHIEU JEAN PIERRE</creator><creator>FAUVELET BENOIT MARC MICHEL</creator><scope>EVB</scope></search><sort><creationdate>20100618</creationdate><title>SUSPENSION D'UN TURBOREACTEUR A UN AERONEF</title><author>LEFORT GUILLAUME ; CHOUARD PIERRE ALAIN JEAN MARIE ; TROHEL MATHIEU JEAN PIERRE ; FAUVELET BENOIT MARC MICHEL</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2925016B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</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>LEFORT GUILLAUME</creatorcontrib><creatorcontrib>CHOUARD PIERRE ALAIN JEAN MARIE</creatorcontrib><creatorcontrib>TROHEL MATHIEU JEAN PIERRE</creatorcontrib><creatorcontrib>FAUVELET BENOIT MARC MICHEL</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>LEFORT GUILLAUME</au><au>CHOUARD PIERRE ALAIN JEAN MARIE</au><au>TROHEL MATHIEU JEAN PIERRE</au><au>FAUVELET BENOIT MARC MICHEL</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SUSPENSION D'UN TURBOREACTEUR A UN AERONEF</title><date>2010-06-18</date><risdate>2010</risdate><abstract>The suspension has a front attachment (10) with a beam transversal with respect to an axis connected to an external ferrule of an intermediate case (3) by two rods of the front attachment. A rear attachment (11) has two rods connected to another external ferrule of an exhaust case (8). A thrust transmission rod (12) connects the hub of the case (3) to the rear attachment. A plane formed by the rods of front attachment and the transmission rod are convergent in a point on the axis of a motor or near the axis.</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 | SUSPENSION D'UN TURBOREACTEUR A UN AERONEF |
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