Aircraft fuselage section
The invention refers to an aircraft fuselage frame (2) that comprises a central element (3) adapted to be located within the perimeter of the fuselage, and two lateral extensions (4) projecting outside the perimeter of the fuselage from both sides of the central element (3) that are a portion of a l...
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| creator | Goya Abaurrea, Pablo Gillemaut, Julien Blanc, Jonathan Bouchet, Eric Colmagro, Jérôme Liñares Mendoza, Sandra Folch Cortés, Diego Martino González, Esteban Pascual Fuertes, Ángel |
| description | The invention refers to an aircraft fuselage frame (2) that comprises a central element (3) adapted to be located within the perimeter of the fuselage, and two lateral extensions (4) projecting outside the perimeter of the fuselage from both sides of the central element (3) that are a portion of a longitudinal structure of a lifting surface (1). Additionally the central element (3) and the two lateral extensions (4) being configured as an integrated piece. |
| format | Patent |
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Additionally the central element (3) and the two lateral extensions (4) being configured as an integrated piece.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Aircraft fuselage section |
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