Abstract: A vehicle having a door slidably mounted on a shell. The vehicle includes at least one assistance device, comprising both a winder carrying a strap and a receptacle, the winder including a brake for braking unwinding of the strap from the winder, one of the winder and receptacle being fastened to the shell and one of the winder and receptacle being fastened to the door, the strap carrying a latchplate suitable for being reversibly attached to the receptacle.

Abstract: An aircraft provided with a wing and a winch device. The winch device is provided with a hoist device that includes a storage drum and a motor member for winding a suspension member around the storage drum and for unwinding said suspension member off the storage drum. The hoist device is surrounded at least in part by a fairing of the winning, said hoist device being arranged in an inside volume of the wing at least in a position referred to as the “streamlined” position.

Abstract: A vehicle having a door slidably mounted on a shell. The vehicle includes at least one assistance device, comprising both a winder carrying a strap and a receptacle, the winder including a brake for braking unwinding of the strap from the winder, one of the winder and receptacle being fastened to the shell and one of the winder and receptacle being fastened to the door, the strap carrying a latchplate suitable for being reversibly attached to the receptacle.

Abstract: An aircraft provided with a wing and a winch device. The winch device is provided with a hoist device that includes a storage drum and a motor member for winding a suspension member around the storage drum and for unwinding said suspension member off the storage drum. The hoist device is surrounded at least in part by a fairing of the winning, said hoist device being arranged in an inside volume of the wing at least in a position referred to as the “streamlined” position.

Abstract: An undercarriage (6) provided with an undercarriage leg (10) and a shock absorber (20), said undercarriage (6) including an actuator-shock absorber (30), said undercarriage leg (10) comprising both a first element (11) carrying contact means (13) and a second element (12), which elements are hinged to each other. The undercarriage (6) includes pivot means (40) enabling said undercarriage leg (10) to pivot firstly in a first direction (S1) in order to retract said undercarriage leg (10) into said housing (4) under drive from said actuator-shock absorber (30), and secondly, during an emergency landing, in a second direction (S2) opposite to the first direction (S1) in order to move said undercarriage leg (10) away from said housing (4) while stressing said actuator-shock absorber (30).

Abstract: An instrument panel for a rotorcraft having two pilot seats, said instrument panel being arranged under an anti-glare shield (4) and including display means (2), at least some of the display means (2) being suitable for acting as communications means, said display means (2) comprising a first set (5) of display means (2) arranged on the instrument panel, and a second set (6) of display means (2) arranged on the instrument panel, wherein the instrument panel includes, symmetrically relative to a longitudinal axis, a central dashboard (3), and at least two lateral dashboards arranged on either side of the central dashboard (3), the dashboards being mutually parallel and presenting a forward longitudinal offset from one dashboard to the next starting from the central dashboard (3).

Abstract: An undercarriage (6) provided with an undercarriage leg (10) and a shock absorber (20), said undercarriage (6) including an actuator-shock absorber (30), said undercarriage leg (10) comprising both a first element (11) carrying contact means (13) and a second element (12), which elements are hinged to each other. The undercarriage (6) includes pivot means (40) enabling said undercarriage leg (10) to pivot firstly in a first direction (S1) in order to retract said undercarriage leg (10) into said housing (4) under drive from said actuator-shock absorber (30), and secondly, during an emergency landing, in a second direction (S2) opposite to the first direction (S1) in order to move said undercarriage leg (10) away from said housing (4) while stressing said actuator-shock absorber (30).

Abstract: An instrument panel for a rotorcraft having two pilot seats, said instrument panel being arranged under an anti-glare shield (4) and including display means (2), at least some of the display means (2) being suitable for acting as communications means, said display means (2) comprising a first set (5) of display means (2) arranged on the instrument panel, and a second set (6) of display means (2) arranged on the instrument panel, wherein the instrument panel includes, symmetrically relative to a longitudinal axis, a central dashboard (3), and at least two lateral dashboards arranged on either side of the central dashboard (3), the dashboards being mutually parallel and presenting a forward longitudinal offset from one dashboard to the next starting from the central dashboard (3).