Aircraft provided with a winch device
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.
1. An aircraft comprising:
a wing extending longitudinally from a streamlined leading edge towards a streamlined trailing edge,
the aircraft being provided with a winch device,
the winch device being provided with a hoist device including a storage drum,
the winch device being provided with a suspension member extending from a first end to a second end that is free and that projects from the hoist device,
the hoist device including a motor member for winding the suspension member around the storage drum and for unwinding the suspension member off the storage drum,
the hoist device being at least partially surrounded by a fairing of the wing,
the hoist device being arranged in an inside volume of the wing in a streamlined position,
wherein the winch device includes a movable arm carried by a hinge,
the hinge giving the movable arm at least one degree of freedom to move in rotation about an axis of rotation relative to the wing,
the hoist device being carried by the movable arm, and
the movable arm and the fairing being movable together between the streamlined position and an extended position.
2. The aircraft according to claim 1 , wherein the fairing is a fuselage fairing of the wing.
3. The aircraft according to claim 1 , wherein the hoist device is arranged in one of the streamlined edges of the wing, the fairing is a portion of the streamlined edge containing the hoist device.
4. The aircraft according to claim 3 , wherein the wing carries a propeller arranged longitudinally beside one of the streamlined edges, and the hoist device is arranged in the other streamlined edge.
5. The aircraft according to claim 3 , wherein the streamlined edge containing the hoist device comprises in succession a root segment, the fairing, and then an end segment.
6. The aircraft according to claim 1 , wherein the suspension member passes through the fairing.
7. The aircraft according to claim 1 , wherein, in the streamlined position, the fairing closes the inside volume, and, in the extended position, the fairing opens the inside volume to a medium outside the aircraft.
8. The aircraft according to claim 1 , wherein the winch device includes a motor-driven system connected to the movable arm to move the movable arm in rotation about the axis of rotation.
9. The aircraft according to claim 1 , wherein the aircraft includes a fuselage provided with at least one frame and a skin fastened to the frame, and the hinge is fastened to the frame.
10. The aircraft according to claim 1 , wherein the hinge is fastened to a member of the wing.
11. The aircraft according to claim 5 , wherein the root segment includes at least one movable flap and a movement system, the movement system co-operating with the flap to move the flap between a closed position and an open position, the flap in the closed position impeding movement of the movable arm, and not impeding the movement when in the open position.
12. The aircraft according to claim 1 , wherein the wing includes at least one deflector for deflecting a stream of air that might impact against the winch device.
13. The aircraft according to claim 1 , wherein the aircraft is an aircraft suitable for performing hovering flight.
14. An aircraft comprising:
a wing extending longitudinally from a streamlined leading edge towards a streamlined trailing edge,
a winch provided with a hoist including a storage drum,
the winch provided with a suspension member extending from a first end to a second end that is free and that projects from the hoist,
the hoist including a motor for winding the suspension member around the storage drum and for unwinding the suspension member off the storage drum,
the hoist being at least partially surrounded by a fairing of the wing,
the hoist disposed in an inside volume of the wing in a streamlined position,
wherein the winch includes a movable arm carried by a hinge,
the hinge giving the movable arm at least one degree of freedom to move in rotation about an axis of rotation relative to the wing,
the hoist being carried by the movable arm, and
the movable arm and the fairing being movable together between the streamlined position and an extended position.
15. The aircraft according to claim 14 , wherein the fairing is a fuselage fairing of the wing.
16. The aircraft according to claim 14 , wherein the hoist is disposed in one of the streamlined edges of the wing, the fairing is a portion of the streamlined edge containing the hoist.
17. The aircraft according to claim 16 , wherein the wing carries a propeller arranged longitudinally beside one of the streamlined edges, and the hoist is disposed in the other streamlined edge.
18. The aircraft according to claim 16 , wherein the streamlined edge containing the hoist comprises in succession a root segment, the fairing, and then an end segment.
19. The aircraft according to claim 14 , wherein the suspension member passes through the fairing.
20. The aircraft according to claim 14 , wherein, in the streamlined position, the fairing closes the inside volume, and, in the extended position, the fairing opens the inside volume to a medium outside the aircraft.