An engine attachment pylon

The present invention provides and engine attachment pylon 17 for mounting an aircraft engine 11 to an aircraft structure while minimising vibrations induced into the engine attachment pylon during flight and operation of the engine. The engine attachment pylon according to the present invention com...

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1. Verfasser:	ANTYPAS, JEROME
Format:	Patent
Sprache:	eng ; fre ; ger
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	ANTYPAS, JEROME
description	The present invention provides and engine attachment pylon 17 for mounting an aircraft engine 11 to an aircraft structure while minimising vibrations induced into the engine attachment pylon during flight and operation of the engine. The engine attachment pylon according to the present invention comprises a rigid box like structure 19 housing a resonator 29 which is tuned to attenuate tension and compression vibrations, experienced by the engine attachment pylon 17. The engine attachment pylon 17 is primarily used in combination within another identical engine attachment pylon 18, both being linked together on a vertical plane (P) within the fuselage by a hinge like junction 28, and each engine attachment pylon 17, 18 being raised approximately 30° from the horizontal (y) axis of the fuselage 10.
format	Patent
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The engine attachment pylon according to the present invention comprises a rigid box like structure 19 housing a resonator 29 which is tuned to attenuate tension and compression vibrations, experienced by the engine attachment pylon 17. The engine attachment pylon 17 is primarily used in combination within another identical engine attachment pylon 18, both being linked together on a vertical plane (P) within the fuselage by a hinge like junction 28, and each engine attachment pylon 17, 18 being raised approximately 30° from the horizontal (y) axis of the fuselage 10.</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=20140402&DB=EPODOC&CC=EP&NR=2631180B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140402&DB=EPODOC&CC=EP&NR=2631180B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ANTYPAS, JEROME</creatorcontrib><title>An engine attachment pylon</title><description>The present invention provides and engine attachment pylon 17 for mounting an aircraft engine 11 to an aircraft structure while minimising vibrations induced into the engine attachment pylon during flight and operation of the engine. 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The engine attachment pylon 17 is primarily used in combination within another identical engine attachment pylon 18, both being linked together on a vertical plane (P) within the fuselage by a hinge like junction 28, and each engine attachment pylon 17, 18 being raised approximately 30° from the horizontal (y) axis of the fuselage 10.</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>eNrjZJByzFNIzUvPzEtVSCwpSUzOyE3NK1EoqMzJz-NhYE1LzClO5YXS3AwKbq4hzh66qQX58anFBYnJqXmpJfGuAUZmxoaGFgZOhsZEKAEA9d8idQ</recordid><startdate>20140402</startdate><enddate>20140402</enddate><creator>ANTYPAS, JEROME</creator><scope>EVB</scope></search><sort><creationdate>20140402</creationdate><title>An engine attachment pylon</title><author>ANTYPAS, JEROME</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2631180B13</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>ANTYPAS, JEROME</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ANTYPAS, JEROME</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>An engine attachment pylon</title><date>2014-04-02</date><risdate>2014</risdate><abstract>The present invention provides and engine attachment pylon 17 for mounting an aircraft engine 11 to an aircraft structure while minimising vibrations induced into the engine attachment pylon during flight and operation of the engine. The engine attachment pylon according to the present invention comprises a rigid box like structure 19 housing a resonator 29 which is tuned to attenuate tension and compression vibrations, experienced by the engine attachment pylon 17. The engine attachment pylon 17 is primarily used in combination within another identical engine attachment pylon 18, both being linked together on a vertical plane (P) within the fuselage by a hinge like junction 28, and each engine attachment pylon 17, 18 being raised approximately 30° from the horizontal (y) axis of the fuselage 10.</abstract><oa>free_for_read</oa></addata></record>
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language	eng ; fre ; ger
recordid	cdi_epo_espacenet_EP2631180B1
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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	An engine attachment pylon
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