Device for folding/unfolding a tail boom of a rotorcraft, an associated rotorcraft, and a corresponding folding/unfolding method

Patent metadata

Field	Value
Publication number	US-2016332719-A1
Application number	US-201615083568-A
Country	US
Kind code	A1
Filing date	Mar 29, 2016
Priority date	Mar 31, 2015
Publication date	Nov 17, 2016
Grant date	—

Abstract

A folding/unfolding device for folding/unfolding a tail boom, the device being arranged in association with a rear power transmission shaft of a tail rotor of the rotorcraft, the folding/unfolding device comprising pivot means enabling a movable portion of the tail boom to move in pivoting relative to a stationary portion of the tail boom, the relative pivoting movement being performed between two distinct extreme positions, namely an unfolded, working position enabling the rear power transmission shaft to transmit driving torque to the tail rotor, and a folded, rest position enabling the overall length of the rotorcraft to be reduced. According to the invention, the folding/unfolding device includes motor-driven decoupling/coupling means for mechanically decoupling/coupling together two portions of a single rear power transmission shaft before/after the relative pivoting movement of the movable portion of the tail boom relative to the stationary portion.

First claim

What is claimed is:

1 . A folding/unfolding device for folding/unfolding a tail boom of a rotorcraft, the folding/unfolding device being arranged on the tail boom in association with a rear power transmission shaft upstream from a rear power transmission gearbox and downstream from a main power transmission gearbox mechanically connected to at least one engine of the rotorcraft, the rear power transmission shaft being suitable for transmitting driving torque and for driving a tail rotor of the rotorcraft in rotation, the folding/unfolding device comprising:
mechanical decoupling/coupling means between two portions of the single rear power transmission shaft and arranged specifically upstream and downstream from the folding/unfolding device; and pivot means enabling a movable portion of the tail boom to move in pivoting relative to a stationary portion of the tail boom, the relative pivoting movement being performed between two distinct extreme positions, namely an unfolded, working position enabling the rear power transmission shaft to transmit driving torque to the tail rotor, and a folded, rest position enabling the overall length of the rotorcraft to be reduced while the engine, the rear power transmission shaft, and the tail rotor are all stopped; wherein the decoupling/coupling means are motor-driven and can be actuated independently of the pivot means firstly to mechanically decouple the two portions of the single rear power transmission shaft prior to the relative pivoting movement corresponding to folding the movable portion relative to the stationary portion of the tail boom, and secondly to mechanically couple together the two portions of the single rear power transmission shaft after the relative pivoting movement corresponding to unfolding the movable portion relative to the stationary portion of the tail boom.

2 . A device according to claim 1 , wherein the folding/unfolding device includes unlocking/locking means for the unfolded, working position of the movable portion of the tail boom relative to the stationary portion of the tail boom.

3 . A device according to claim 2 , wherein the decoupling/coupling means and the unlocking/locking means are actuated by a common actuator.

4 . A device according to claim 3 , wherein the decoupling/coupling means include first resilient return means stressed in compression and having free ends bearing respectively on a frame of the stationary portion and on a plane face of a jaw clutch that is movable in translation along a direction parallel to a longitudinal direction of the rear power transmission shaft, and the unlocking/locking means include second resilient return means stressed in compression and having free ends bearing respectively on the frame of the stationary portion and on a plane face of a rod of the unlocking/locking means.

5 . A device according to claim 4 , wherein the first resilient return means enable a first return force to be exerted on the jaw clutch, and the second resilient return means enable a second return force to be exerted on the rod of the unlocking/locking means, the first return force being less than the second return force.

6 . A device according to claim 3 , wherein the folding/unfolding device includes a mechanical connection member enabling the decoupling/coupling means and the unlocking/locking means to be actuated simultaneously with the common actuator.

7 . A device according to claim 4 , wherein the mechanical connection member includes at least one link, at least one crank having at least one degree of freedom to move in rotation relative to the frame, and a pusher enabling a thrust force to be exerted on the plane face of the jaw clutch, the free ends of the link being in ball-joint connection respectively with a free end of the rod and with a free end of a lever arm of the crank, the mechanical connection member enabling the common actuator to move the movable jaw clutch in translation along a direction parallel to the longitudinal direction of the rear power transmission shaft.

8 . A device according to claim 6 , wherein the mechanical connection member includes at least one projection suitable for controlling the movement in translation of a jaw clutch, the projection being arranged in a slideway connection with a frame of the stationary portion of the tail boom and including a free end that is arranged in annular linear connection with a free end of a rod, the rod being arranged in a helical connection with the frame to transform the movement in translation of at least one finger of the actuator into a combined movement in rotation and in translation of the rod relative to the frame.

9 . A device according to claim 2 , wherein the decoupling/coupling means include a first actuator, and the unlocking/locking means include a second actuator distinct from the first actuator.

10 . A device according to claim 1 , wherein the pivot means have a pivot axis inclined at a predetermined angle α relative to a plane P perpendicular to a longitudinal direction of the rear power transmission shaft, the predetermined angle α lying in the range 20 degrees to 30 degrees.

11 . A rotorcraft having a tail rotor arranged on a tail boom, the tail rotor being driven in rotation by means of at least one engine and a rear power transmission shaft, and the tail boom including a movable portion movable in pivoting relative to a stationary portion between two distinct extreme positions, namely an unfolded, working position enabling the rear folding/unfolding to transmit driving torque to the tail rotor, and a folded, rest position enabling the overall length of the rotorcraft to be reduce when the engine, the rear power transmission shaft and the tail rotor are all stopped, wherein the rotorcraft includes a folding/unfolding device for a tail boom according to claim 1 .

12 . A folding/unfolding method for folding/unfolding a tail boom of a rotorcraft including at least one tail rotor, the tail rotor being driven in rotation by means of at least one engine and at least one rear power transmission shaft, the folding/unfolding method being performed when the at least one engine, the rear power transmission shaft, and the tail rotor are all stopped, the folding/unfolding method comprising:
a first step consisting in mechanically decoupling two portions of a single rear power transmission shaft; an unlocking, second step for unlocking a movable portion of the tail boom when in an unfolded, working position relative to a stationary portion of the tail boom, the unfolded, working position of the movable portion enabling the rear power transmission shaft to transmit driving torque to the tail rotor; a folding, third step of folding the movable portion relative to the stationary portion, the folding corresponding to moving the movable portion in relative pivoting through an angle between two distinct extreme positions, namely the unfolded, working position and a folded, rest position enabling the overall length of the rotorcraft to be reduced; an unfolding, fourth step of unfolding the movable portion relative to the stationary portion, the unfolding corresponding to a relative pivoting movement, through an angle of the movable portion between two distinct extreme positions, namely the folded, rest position and the unfolded, working position; a fifth step consisting in mechanically coupling together the two portions of the single rear power transmission shaft; and a locking, sixth step of locking the movable portion of the tail boom in the unfolded, working position relative to the stationary portion of the tail boom; wherein: the first step and the third step are performed independently of each other,

Assignees

• Airbus Helicopters

Inventors

• Maltinti Maxime
• Poggioli Florian

Classifications

• B64C27/82

  characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft · CPC title

• B64C1/30 Primary

  Parts of fuselage relatively movable to reduce overall dimensions of aircraft · CPC title

• B64C27/08

  with two or more rotors · CPC title

• B64C1/063

  Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms · CPC title

• B64C27/06

  with single rotor · CPC title