SCHUBUMKEHRVORRICHTUNG FUER EIN STRAHLTRIEBWERK, AUSGERUESTET MIT UMKEHRKLAPPEN MIT STRAHLLEITDUESEN

A tilting door (107) of a thrust reverser for the secondary flow of a double-flow jet engine comprises an outer panel (9), the outer surface of which is connected to the outer profile of the nacelle (4) and fixed rear part (3) of the reverser and an inner panel (111), the inner surface (111a) of whi...

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Hauptverfasser:	VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR, STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR, HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR
Format:	Patent
Sprache:	ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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creator	VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR
description	A tilting door (107) of a thrust reverser for the secondary flow of a double-flow jet engine comprises an outer panel (9), the outer surface of which is connected to the outer profile of the nacelle (4) and fixed rear part (3) of the reverser and an inner panel (111), the inner surface (111a) of which coincides, in direct thrust, with the theoretical surface delimiting the line of the secondary flow. Between the said inner panel (111) and outer panel (9) is formed a passage (20) having an orifice (21, 22) at each end on the inside of the door and, in the thrust reversal mode, forming a mini-nozzle via which passes part (15b) of the reversed flow (15a) of which it ensures the best possible deflection.
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Between the said inner panel (111) and outer panel (9) is formed a passage (20) having an orifice (21, 22) at each end on the inside of the door and, in the thrust reversal mode, forming a mini-nozzle via which passes part (15b) of the reversed flow (15a) of which it ensures the best possible deflection.</description><edition>5</edition><language>ger</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>1993</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=19930325&DB=EPODOC&CC=DE&NR=68902727T2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19930325&DB=EPODOC&CC=DE&NR=68902727T2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR</creatorcontrib><creatorcontrib>STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR</creatorcontrib><creatorcontrib>HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR</creatorcontrib><title>SCHUBUMKEHRVORRICHTUNG FUER EIN STRAHLTRIEBWERK, AUSGERUESTET MIT UMKEHRKLAPPEN MIT STRAHLLEITDUESEN</title><description>A tilting door (107) of a thrust reverser for the secondary flow of a double-flow jet engine comprises an outer panel (9), the outer surface of which is connected to the outer profile of the nacelle (4) and fixed rear part (3) of the reverser and an inner panel (111), the inner surface (111a) of which coincides, in direct thrust, with the theoretical surface delimiting the line of the secondary flow. Between the said inner panel (111) and outer panel (9) is formed a passage (20) having an orifice (21, 22) at each end on the inside of the door and, in the thrust reversal mode, forming a mini-nozzle via which passes part (15b) of the reversed flow (15a) of which it ensures the best possible deflection.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1993</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNi00KwjAUBrNxIeodgmsFqWB12Z-vTWgay8uLLkvRuBIt1PujWA_gamCYmYqry5RPfV1B0elIpDPF3pay8CAJbaVjSpRh0kjPoGolE-9KkIdjsKw1y3GuTNI0sF8zPgaa808HOxeTW3cfwuLHmVgW4EytQ_9sw9B3l_AIrzbHbn_YRHEUM0fbv6I3ZtQ2gA</recordid><startdate>19930325</startdate><enddate>19930325</enddate><creator>VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR</creator><creator>STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR</creator><creator>HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR</creator><scope>EVB</scope></search><sort><creationdate>19930325</creationdate><title>SCHUBUMKEHRVORRICHTUNG FUER EIN STRAHLTRIEBWERK, AUSGERUESTET MIT UMKEHRKLAPPEN MIT STRAHLLEITDUESEN</title><author>VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR ; STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR ; HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE68902727TT23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>1993</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR</creatorcontrib><creatorcontrib>STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR</creatorcontrib><creatorcontrib>HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>VAUCHEL, GUY BERNARD, F-76610 LE HAVRE, FR</au><au>STANDISH, ROBERT, F-78120 GAZERAN RAMBOUILLET, FR</au><au>HOGIE, JEAN PAUL RENE ANDRE, F-76600 LE HAVRE, FR</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SCHUBUMKEHRVORRICHTUNG FUER EIN STRAHLTRIEBWERK, AUSGERUESTET MIT UMKEHRKLAPPEN MIT STRAHLLEITDUESEN</title><date>1993-03-25</date><risdate>1993</risdate><abstract>A tilting door (107) of a thrust reverser for the secondary flow of a double-flow jet engine comprises an outer panel (9), the outer surface of which is connected to the outer profile of the nacelle (4) and fixed rear part (3) of the reverser and an inner panel (111), the inner surface (111a) of which coincides, in direct thrust, with the theoretical surface delimiting the line of the secondary flow. Between the said inner panel (111) and outer panel (9) is formed a passage (20) having an orifice (21, 22) at each end on the inside of the door and, in the thrust reversal mode, forming a mini-nozzle via which passes part (15b) of the reversed flow (15a) of which it ensures the best possible deflection.</abstract><edition>5</edition><oa>free_for_read</oa></addata></record>
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subjects	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
title	SCHUBUMKEHRVORRICHTUNG FUER EIN STRAHLTRIEBWERK, AUSGERUESTET MIT UMKEHRKLAPPEN MIT STRAHLLEITDUESEN
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