Three-point shackle with vibration-filtering capacity and aircraft engine attachment provided with such a shackle
The link (124) has a first orifice (132a) and a second orifice (132b) to connect the link to an aircraft pylon. A third orifice (132c) connects the link to an aircraft engine. The third orifice is offset relative to a plane passing simultaneously through an axis (134a) of the first orifice and throu...
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| creator | TERRAL, ROMAIN BROCHARD, WOLFGANG |
| description | The link (124) has a first orifice (132a) and a second orifice (132b) to connect the link to an aircraft pylon. A third orifice (132c) connects the link to an aircraft engine. The third orifice is offset relative to a plane passing simultaneously through an axis (134a) of the first orifice and through an axis (134b) of the second orifice. A straight line segment (S) extending from the axis of the first orifice to an axis (134c) of the third orifice crosses a region (R) external to the link when the link is seen in section in any plane orthogonal to the axes of the first and second orifices. Independent claims are also included for the following: (1) an engine mount of an aircraft (2) a propulsion system for an aircraft.
Manille à trois points (124) pour attache moteur d'aéronef, comprenant :
- un premier orifice (132a) et un deuxième orifice (132b), tous deux destinés à relier la manille (124) à un mât d'aéronef, et
- un troisième orifice (132c), destiné à relier la manille (124) à un moteur d'aéronef. Le troisième orifice (132c) est écarté par rapport à un plan (P) passant simultanément par un axe (134a) du premier orifice (132a) et par un axe (134b) du deuxième orifice (132b). Lorsque la manille est vue en section selon un plan orthogonal aux axes (134a, 134b), un segment de droite (S) allant de l'axe (134b) du deuxième orifice jusqu'à un axe (134c) du troisième orifice traverse une région (R) extérieure à la manille. Cette conformation confère à la manille une souplesse lui permettant de filtrer les vibrations transversales entre un moteur et un mât d'aéronef. |
| format | Patent |
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Manille à trois points (124) pour attache moteur d'aéronef, comprenant :
- un premier orifice (132a) et un deuxième orifice (132b), tous deux destinés à relier la manille (124) à un mât d'aéronef, et
- un troisième orifice (132c), destiné à relier la manille (124) à un moteur d'aéronef. Le troisième orifice (132c) est écarté par rapport à un plan (P) passant simultanément par un axe (134a) du premier orifice (132a) et par un axe (134b) du deuxième orifice (132b). Lorsque la manille est vue en section selon un plan orthogonal aux axes (134a, 134b), un segment de droite (S) allant de l'axe (134b) du deuxième orifice jusqu'à un axe (134c) du troisième orifice traverse une région (R) extérieure à la manille. Cette conformation confère à la manille une souplesse lui permettant de filtrer les vibrations transversales entre un moteur et un mât d'aéronef.</description><language>eng ; fre ; ger</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>2014</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=20140716&DB=EPODOC&CC=EP&NR=2754612A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140716&DB=EPODOC&CC=EP&NR=2754612A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TERRAL, ROMAIN</creatorcontrib><creatorcontrib>BROCHARD, WOLFGANG</creatorcontrib><title>Three-point shackle with vibration-filtering capacity and aircraft engine attachment provided with such a shackle</title><description>The link (124) has a first orifice (132a) and a second orifice (132b) to connect the link to an aircraft pylon. A third orifice (132c) connects the link to an aircraft engine. The third orifice is offset relative to a plane passing simultaneously through an axis (134a) of the first orifice and through an axis (134b) of the second orifice. A straight line segment (S) extending from the axis of the first orifice to an axis (134c) of the third orifice crosses a region (R) external to the link when the link is seen in section in any plane orthogonal to the axes of the first and second orifices. Independent claims are also included for the following: (1) an engine mount of an aircraft (2) a propulsion system for an aircraft.
Manille à trois points (124) pour attache moteur d'aéronef, comprenant :
- un premier orifice (132a) et un deuxième orifice (132b), tous deux destinés à relier la manille (124) à un mât d'aéronef, et
- un troisième orifice (132c), destiné à relier la manille (124) à un moteur d'aéronef. Le troisième orifice (132c) est écarté par rapport à un plan (P) passant simultanément par un axe (134a) du premier orifice (132a) et par un axe (134b) du deuxième orifice (132b). Lorsque la manille est vue en section selon un plan orthogonal aux axes (134a, 134b), un segment de droite (S) allant de l'axe (134b) du deuxième orifice jusqu'à un axe (134c) du troisième orifice traverse une région (R) extérieure à la manille. Cette conformation confère à la manille une souplesse lui permettant de filtrer les vibrations transversales entre un moteur et un mât d'aéronef.</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>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNzbsOwjAMheEuDAh4B79AhpbbjFARI0P3yqRuY7U4ITFFvD2VgJ3pLL--M8_ulYtEJngWheTQ9gPBk9XByNeIyl5My4NSZOnAYkDL-gKUBpCjjdgqkHQsBKiK1t1ogkL0IzfUfKT0sA7wpy-zWYtDotV3Fxmcyup4NhR8TWk6ICGty0ux3252eXHI138kb2BCQ68</recordid><startdate>20140716</startdate><enddate>20140716</enddate><creator>TERRAL, ROMAIN</creator><creator>BROCHARD, WOLFGANG</creator><scope>EVB</scope></search><sort><creationdate>20140716</creationdate><title>Three-point shackle with vibration-filtering capacity and aircraft engine attachment provided with such a shackle</title><author>TERRAL, ROMAIN ; BROCHARD, WOLFGANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2754612A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2014</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>TERRAL, ROMAIN</creatorcontrib><creatorcontrib>BROCHARD, WOLFGANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TERRAL, ROMAIN</au><au>BROCHARD, WOLFGANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Three-point shackle with vibration-filtering capacity and aircraft engine attachment provided with such a shackle</title><date>2014-07-16</date><risdate>2014</risdate><abstract>The link (124) has a first orifice (132a) and a second orifice (132b) to connect the link to an aircraft pylon. A third orifice (132c) connects the link to an aircraft engine. The third orifice is offset relative to a plane passing simultaneously through an axis (134a) of the first orifice and through an axis (134b) of the second orifice. A straight line segment (S) extending from the axis of the first orifice to an axis (134c) of the third orifice crosses a region (R) external to the link when the link is seen in section in any plane orthogonal to the axes of the first and second orifices. Independent claims are also included for the following: (1) an engine mount of an aircraft (2) a propulsion system for an aircraft.
Manille à trois points (124) pour attache moteur d'aéronef, comprenant :
- un premier orifice (132a) et un deuxième orifice (132b), tous deux destinés à relier la manille (124) à un mât d'aéronef, et
- un troisième orifice (132c), destiné à relier la manille (124) à un moteur d'aéronef. Le troisième orifice (132c) est écarté par rapport à un plan (P) passant simultanément par un axe (134a) du premier orifice (132a) et par un axe (134b) du deuxième orifice (132b). Lorsque la manille est vue en section selon un plan orthogonal aux axes (134a, 134b), un segment de droite (S) allant de l'axe (134b) du deuxième orifice jusqu'à un axe (134c) du troisième orifice traverse une région (R) extérieure à la manille. Cette conformation confère à la manille une souplesse lui permettant de filtrer les vibrations transversales entre un moteur et un mât d'aéronef.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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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 | Three-point shackle with vibration-filtering capacity and aircraft engine attachment provided with such a shackle |
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