Turboprop aircraft with engine pods mounted on the main wing tips, comprises rotating front sections enabling very short/vertical take off capability
The aircraft comprises of engine pods (6) mounted on the extreme wing tips. The engine pods house a turboprop engine that drives an oversized propeller assembly, the circumference of which is represented by the circle and line (9). The front section of the pod to which the propeller is attached can...
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| creator | MAGRE ERIC BALAYN FREDERIC |
| description | The aircraft comprises of engine pods (6) mounted on the extreme wing tips. The engine pods house a turboprop engine that drives an oversized propeller assembly, the circumference of which is represented by the circle and line (9). The front section of the pod to which the propeller is attached can be tilted whilst the aircraft is on the ground. As the aircraft takes of and attain normal horizontal flight, the propellers can be rotated to a normal operating position driving the aircraft in horizontal flight.
L'aéronef convertible (1) à rotors (9) basculants comprend deux ailes fixes (5) à flèche nulle sur lesquelles un arbre d'interconnexion (13) est rectiligne et parallèle à l'axe de basculement (X-X), mais décalé de cet axe, sensiblement perpendiculaire à un axe longitudinal de symétrie (A-A) de l'aéronef (1), dont le centre de gravité en mode hélicoptère est sensiblement dans un plan vertical passant par 1'axe de basculement (X-X), et en mode avion est sensiblement contenu dans ou à proximité d'un autre plan vertical passant par la ligne droite des foyers aérodynamiques des ailes (5). |
| format | Patent |
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L'aéronef convertible (1) à rotors (9) basculants comprend deux ailes fixes (5) à flèche nulle sur lesquelles un arbre d'interconnexion (13) est rectiligne et parallèle à l'axe de basculement (X-X), mais décalé de cet axe, sensiblement perpendiculaire à un axe longitudinal de symétrie (A-A) de l'aéronef (1), dont le centre de gravité en mode hélicoptère est sensiblement dans un plan vertical passant par 1'axe de basculement (X-X), et en mode avion est sensiblement contenu dans ou à proximité d'un autre plan vertical passant par la ligne droite des foyers aérodynamiques des ailes (5).</description><edition>7</edition><language>eng ; fre</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2000</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=20000929&DB=EPODOC&CC=FR&NR=2791319A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,309,782,887,25573,76557</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20000929&DB=EPODOC&CC=FR&NR=2791319A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>MAGRE ERIC</creatorcontrib><creatorcontrib>BALAYN FREDERIC</creatorcontrib><title>Turboprop aircraft with engine pods mounted on the main wing tips, comprises rotating front sections enabling very short/vertical take off capability</title><description>The aircraft comprises of engine pods (6) mounted on the extreme wing tips. The engine pods house a turboprop engine that drives an oversized propeller assembly, the circumference of which is represented by the circle and line (9). The front section of the pod to which the propeller is attached can be tilted whilst the aircraft is on the ground. As the aircraft takes of and attain normal horizontal flight, the propellers can be rotated to a normal operating position driving the aircraft in horizontal flight.
L'aéronef convertible (1) à rotors (9) basculants comprend deux ailes fixes (5) à flèche nulle sur lesquelles un arbre d'interconnexion (13) est rectiligne et parallèle à l'axe de basculement (X-X), mais décalé de cet axe, sensiblement perpendiculaire à un axe longitudinal de symétrie (A-A) de l'aéronef (1), dont le centre de gravité en mode hélicoptère est sensiblement dans un plan vertical passant par 1'axe de basculement (X-X), et en mode avion est sensiblement contenu dans ou à proximité d'un autre plan vertical passant par la ligne droite des foyers aérodynamiques des ailes (5).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2000</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjEFKA1EQRGfjQtQ71AEMMmYhWYokuJbsQ89P_0zjTPenu6PkIN7XCXgAV1XUe9Rt97M_-2DNrYHEi1NNfEuOYD2JMpodA7OdNfkIU-TImEl0kfSElBaPKDY3l-CAW1JeQXXTRHBJMY3ljIbpun-xXxCjeT4tNaXQhKRPhtWKQo0GmSQv991NpSn44S_vOuy2-7f3FTc7cDQqrJyH3cfzy6Zf95vXfv0P5RciYVGa</recordid><startdate>20000929</startdate><enddate>20000929</enddate><creator>MAGRE ERIC</creator><creator>BALAYN FREDERIC</creator><scope>EVB</scope></search><sort><creationdate>20000929</creationdate><title>Turboprop aircraft with engine pods mounted on the main wing tips, comprises rotating front sections enabling very short/vertical take off capability</title><author>MAGRE ERIC ; BALAYN FREDERIC</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR2791319A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre</language><creationdate>2000</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>MAGRE ERIC</creatorcontrib><creatorcontrib>BALAYN FREDERIC</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>MAGRE ERIC</au><au>BALAYN FREDERIC</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Turboprop aircraft with engine pods mounted on the main wing tips, comprises rotating front sections enabling very short/vertical take off capability</title><date>2000-09-29</date><risdate>2000</risdate><abstract>The aircraft comprises of engine pods (6) mounted on the extreme wing tips. The engine pods house a turboprop engine that drives an oversized propeller assembly, the circumference of which is represented by the circle and line (9). The front section of the pod to which the propeller is attached can be tilted whilst the aircraft is on the ground. As the aircraft takes of and attain normal horizontal flight, the propellers can be rotated to a normal operating position driving the aircraft in horizontal flight.
L'aéronef convertible (1) à rotors (9) basculants comprend deux ailes fixes (5) à flèche nulle sur lesquelles un arbre d'interconnexion (13) est rectiligne et parallèle à l'axe de basculement (X-X), mais décalé de cet axe, sensiblement perpendiculaire à un axe longitudinal de symétrie (A-A) de l'aéronef (1), dont le centre de gravité en mode hélicoptère est sensiblement dans un plan vertical passant par 1'axe de basculement (X-X), et en mode avion est sensiblement contenu dans ou à proximité d'un autre plan vertical passant par la ligne droite des foyers aérodynamiques des ailes (5).</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Turboprop aircraft with engine pods mounted on the main wing tips, comprises rotating front sections enabling very short/vertical take off capability |
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