METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT
An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thr...
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| creator | ILIOPOULOS, ALEXANDROS RICHER, ALAIN KULCZYK, MARCIN REGNAULT, LAURENT |
| description | An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.
L'invention concerne un aéronef (10) contenant un axe de référence s'étendant le long d'au moins une partie de l'aéronef, et un système de propulsion ayant un élément de vecteur de poussée (43) définissant généralement une direction de poussée du moteur de réacteur à double flux (18), l'élément de vecteur de poussée (43) s'étendant par rapport à un axe de vecteur de poussée, le moteur de réacteur à double flux (18) étant placé sur l'aéronef avec l'élément de vecteur de poussée (43) orienté par rapport à l'axe de référence de l'aéronef. |
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L'invention concerne un aéronef (10) contenant un axe de référence s'étendant le long d'au moins une partie de l'aéronef, et un système de propulsion ayant un élément de vecteur de poussée (43) définissant généralement une direction de poussée du moteur de réacteur à double flux (18), l'élément de vecteur de poussée (43) s'étendant par rapport à un axe de vecteur de poussée, le moteur de réacteur à double flux (18) étant placé sur l'aéronef avec l'élément de vecteur de poussée (43) orienté par rapport à l'axe de référence de l'aéronef.</description><language>eng ; fre</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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=20231017&DB=EPODOC&CC=CA&NR=2985967C$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231017&DB=EPODOC&CC=CA&NR=2985967C$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ILIOPOULOS, ALEXANDROS</creatorcontrib><creatorcontrib>RICHER, ALAIN</creatorcontrib><creatorcontrib>KULCZYK, MARCIN</creatorcontrib><creatorcontrib>REGNAULT, LAURENT</creatorcontrib><title>METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT</title><description>An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.
L'invention concerne un aéronef (10) contenant un axe de référence s'étendant le long d'au moins une partie de l'aéronef, et un système de propulsion ayant un élément de vecteur de poussée (43) définissant généralement une direction de poussée du moteur de réacteur à double flux (18), l'élément de vecteur de poussée (43) s'étendant par rapport à un axe de vecteur de poussée, le moteur de réacteur à double flux (18) étant placé sur l'aéronef avec l'élément de vecteur de poussée (43) orienté par rapport à l'axe de référence de l'aéronef.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZIj1dQ3x8HdRcPRzUQiODA5x9VVw8w9ScPTxdPfz9HNXCAjyDwj1Cfb094NJg1SGuXp4Ovu4Kng4hoEUBYc6eyCrBOv2dfUL4WFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8c6ORpYWppZm5s7GhFUAAEhCMiw</recordid><startdate>20231017</startdate><enddate>20231017</enddate><creator>ILIOPOULOS, ALEXANDROS</creator><creator>RICHER, ALAIN</creator><creator>KULCZYK, MARCIN</creator><creator>REGNAULT, LAURENT</creator><scope>EVB</scope></search><sort><creationdate>20231017</creationdate><title>METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT</title><author>ILIOPOULOS, ALEXANDROS ; RICHER, ALAIN ; KULCZYK, MARCIN ; REGNAULT, LAURENT</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CA2985967C3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2023</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>ILIOPOULOS, ALEXANDROS</creatorcontrib><creatorcontrib>RICHER, ALAIN</creatorcontrib><creatorcontrib>KULCZYK, MARCIN</creatorcontrib><creatorcontrib>REGNAULT, LAURENT</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ILIOPOULOS, ALEXANDROS</au><au>RICHER, ALAIN</au><au>KULCZYK, MARCIN</au><au>REGNAULT, LAURENT</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT</title><date>2023-10-17</date><risdate>2023</risdate><abstract>An aircraft (10) is described as including a reference axis extending along at least a portion of the aircraft, and a propulsion system having a thrust vector feature (43) defining generally a direction of thrust of the turbofan engine (18), the thrust vector feature (43) extending relative to a thrust vector axis, where the turbofan engine (18) is disposed on the aircraft with the thrust vector feature (43) oriented with respect to the reference axis of the aircraft.
L'invention concerne un aéronef (10) contenant un axe de référence s'étendant le long d'au moins une partie de l'aéronef, et un système de propulsion ayant un élément de vecteur de poussée (43) définissant généralement une direction de poussée du moteur de réacteur à double flux (18), l'élément de vecteur de poussée (43) s'étendant par rapport à un axe de vecteur de poussée, le moteur de réacteur à double flux (18) étant placé sur l'aéronef avec l'élément de vecteur de poussée (43) orienté par rapport à l'axe de référence de l'aéronef.</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 DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | METHOD AND SYSTEM FOR ALIGNING PROPULSION SYSTEM AND VEHICLE HAVING SUCH PROPULSION ALIGNMENT |
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