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Aircraft e.g. twin-beam twin-engine aircraft, has cockpit mounted rotationally around longeron in order to allow temporary rotation of cockpit toward bottom by voluntary action of pilot in order to retract nose for sight of pilot
Aircraft e.g. twin-beam twin-engine aircraft, has cockpit mounted rotationally around longeron in order to allow temporary rotation of cockpit toward bottom by voluntary action of pilot in order to retract nose for sight of pilot
The aircraft has two wings (3) supported by a traversing longeron (4). A cockpit (5) includes a nose (6) projecting forward, and is separated from a fuselage (1). The cockpit is mounted rotationally around the longeron in order to allow temporary rotation of the cockpit toward bottom by voluntary action of a pilot using actuation units in order to retract the nose for sight of the pilot. A wheel (18) of a landing gear is located at a front part of the cockpit. The wings are equidistance from each other. The cockpit is placed in an intermediate position between the wings. The actuation units are jacks, wheels and endless screws.
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