METHOD AND APPARATUS FOR FOLDING/UNFOLDING THE BLADES OF A ROTARY-WING AIRCRAFT ROTOR

• US 20040026564A1
• Filed: 02/27/2003
• Published: 02/12/2004
• Est. Priority Date: 03/11/2002
• Status: Active Grant

• Current Assignee: Airbus Helicopters
• Original Assignee: Eurocopter
• Inventors: Romani, Michel, Cayol, Marcel
• Granted Patent: US 6,695,253 B1
• Time in Patent Office: Days
• US Class Current: 244/17.11
• CPC Class Codes: B64C 27/50 Blades foldable to facilitate stowage of aircraft

Abstract

To fold/unfold blades of a rotor, at least one variable-length linear actuator is removably attached to two blades locked in the flight position. A first blade is unlocked, and the actuator is actuated to vary its length and bear against the other blade which remains locked. This causes the first blade to pivot about its pivot axis and move to a folded position where it is again locked. The other blade is then unlocked and the actuator once again actuated but this time bearing against the first blade. In this way the other blade pivots into the folded position where it is again locked. The two locked folded blades may be connected to each other by a link rod. Rotors with three blades, four blades, five and six blades can be folded/unfolded with only two actuators.

Claims

1. A method of folding/unfolding at least one blade of a multi-bladed rotor of a rotary-wing aircraft, with at least a first blade being connected to a hub of the rotor by a coupling comprising a pivotal connection defining a pivot axis and a releasable connection, release of which allows its blade to be pivoted about its pivot axis between an unfolded position and a folded position, the method comprising steps:

(a) removably attaching at least one variable-length linear actuator to the first blade and a second blade, each locked in a fixed position with respect to the hub which is itself locked stationary;

(b) releasing the first blade from its fixed position with respect to the hub;

(c) actuating the linear actuator to vary its length and bear against the second blade, thereby pivoting the first blade about its pivot axis to a new position with respect to the hub; and

(d) locking the first blade in the new position.

2. A method according to claim 1, wherein the second blade is connected to the hub of the rotor in an analogous way to the first blade, and wherein the method further comprises after step (d) steps:

(e) releasing the second blade from its fixed position with respect to the rotor;

(f) actuating the linear actuator to vary its length and bear against the first blade, thereby pivoting the second blade about its pivot axis to a new position with respect to the hub; and

(g) locking the second blade in its new position.

3. A method according to claim 2, further comprising before step (f):

removably attaching a link rod to the first blade locked in its new position and to a third blade whose position is fixed with respect to the hub, whereby under subsequent actuation the linear actuator bears against the first and third blades together when the second blade pivots about its axis.

4. A method according to claim 2, wherein the multi-bladed rotor is a two-bladed rotor with the blades being foldable towards a rear part of the rotary-wing aircraft, and wherein the method further comprises:

locking the stationary rotor with the first and second blades aligned substantially transversely to a longitudinal axis of the rotary-wing aircraft; and

attaching pivotally the linear actuator to a forward part of one blade and a rearward part of the other blade such that the linear actuator extends rearwardly of a line passing through the pivot axes of the two blades, and such that the linear actuator is disposed rearwardly of the hub of the rotor.

5. A method according to claim 4, wherein the linear actuator is attached to the blades via two securing brackets, one projecting forwardly of a leading edge of one blade and another projecting rearwardly of a trailing edge of the other blade.

6. A method according to claim 1, wherein the multi-bladed rotor is a three-bladed rotor, with the blades being foldable towards a rear part of the rotary-wing aircraft, and with a third blade connected to and fixed in position with respect to the hub of the rotor in an analogous way to the first blade, and wherein the method further comprises:

locking the stationary rotor with the second blade aligned over the rear part of the rotary-wing aircraft;

removable attaching a variable-length linear actuator to the second and third blades;

releasing the third blade from its fixed position;

actuating the linear actuator to vary its length and pivot the third blade about its pivot axis to a new position with respect to the hub; and

locking the third blade in its new position.

7. A method according to claim 6, wherein the linear actuator between the first and second blades and the linear actuator between the third and second blades are attached substantially to a common attachment point on the second blade, the common attachment point being substantially aligned with a longitudinal axis of the second blade and radially outwardly of any pivot axis the second blade has relative to an axis of rotor rotation.

8. A method according to claim 2, wherein the multi-bladed rotor has at least four blades, with the blades being foldable towards a rear part of the rotary wing aircraft, and with a third blade and a fourth blade each connected to and fixed in position with respect to the hub of the rotor in an analogous way to the first blade, and wherein the method further comprises:

locking the stationary rotor with the first and second blades disposed on one side of the rotary-wing aircraft and the third and fourth blades disposed on an opposite side, with the first blade rearwardly of the second blade and the third blade rearwardly of the fourth blade;

carrying out steps (a) to (d) so that the new position of the first blade is over the rear part of the rotary wing aircraft;

repeating steps (a) to (d) for the third blade in place of the first blade so that the third blade is positioned adjacent the first blade;

carrying out steps (e) to (f) for the second blade so that the second blade is positioned adjacent the first blade;

repeating steps (e) to (f) for the fourth blade in place of the second blade so that the fourth blade is positioned adjacent the third blade.

9. A method according to claim 8, further comprising connecting the first blade to the third blade with a removable link when the first blade is in the new position and the third blade is positioned adjacent to it.

10. A method according to claim 8, wherein the stationary rotor is locked with one blade positioned over the rear part of the rotary wing aircraft when the multi-bladed rotor has an odd-number of blades.

11. A method according to claim 8, wherein the multi-bladed rotor has more than five blades, and wherein the method further comprises:

removing the linear actuator between the first and second blades once pivoted respectively to the new position over the rear part of the rotary wing aircraft and adjacent to the new position;

removably attaching the linear actuator between the second and a fifth blade connected to and fixed in position with respect to the hub of the rotor in an analogous way to the first blade;

and repeating steps (e) to (f) for the fifth blade in place of the second blade so that the fifth blade is positioned adjacent the second blade.

12. A method according to claim 1, wherein the first blade is locked in the folded position by attaching said blade to a rear part of the rotary wing aircraft by at least one attachment tool selected from the group consisting of a pole, a folding pole, strapping and a support.

13. Apparatus for folding/unfolding at least one blade of a multi-bladed rotor of a rotary-wing aircraft, with at least a first blade being connected to a hub of the rotor by a coupling comprising a pivotal connection defining a pivot axis and a releasable connection, release of which allows its blade to be pivoted about its pivot axis between an unfolded position and folded position, the apparatus comprising:

at least one variable length, removable linear actuator configured to be removably attached to two adjacent blades of the rotor and to exert forces in either direction along its longitudinal axis on two blades connected by the linear actuator; and

connectors for removably attaching the linear actuator to two adjacent blades, each connector comprising an end fitting integral with the linear actuator and an attachment device configured for attachment to one blade, the end fitting and the attachment device being releasably interconnectable.

14. Apparatus according to claim 13, comprising two substantially identical linear actuators, each having at each of its two longitudinal ends an end fitting for attaching removably to at least one attachment device configured for attachment to a blade.

15. Apparatus according to claim 13, further comprising at least one substantially rectilinear removable link rod configured for removable attachment to two blades via releasable connectors at opposed ends of the link rod.

16. Apparatus according to claim 13, wherein the at least one removable linear actuator comprises at least one double-acting linear jack comprising at least one rectilinear rod configured to move a either direction in a jack body into which said rod is partially inserted and drivable by a drive device housed in the body.

17. Apparatus according to claim 16, wherein said jack is one of mechanical and electromechanical with the body housing a mechanical drive device which is configured to multiply forces imparted to the rod.

18. Apparatus according to claim 17, wherein the mechanical drive device comprises at least one stage of reduction gearing comprising at least one input shaft configured to be driven from outside the jack by one of a mechanical or electromechanical device.

19. Apparatus according to claim 18, wherein the at least one reduction stage comprises gearing selected from the group consisting of a worm screw, a rack-and-pinion combination and a gearwheel-pinion combination.

20. Apparatus according to claim 18, wherein the mechanical drive device comprises a worm screw engaged with the rod which is tubular, the worm screw partially extended into the tubular rod, with the worm screw being rotatably driven by an output gearwheel of a pair of bevel gears, an input pinion of which is integral with the input shaft.

21. Apparatus according to claim 17, wherein the jack further comprises a manually operated mechanism for disengaging the rod from the mechanical drive device and allowing rapid adjustment of the jack to any desired length.

22. Apparatus according to claim 16, wherein the jack further comprises a shock absorber in series with at least one of the rod, the body and one end fitting of the jack.

23. Apparatus according to claim 13, wherein at least one connector for removably attaching the linear actuator to adjacent blades, comprises at least one ball joint for connecting at least one end fitting to its respective attachment device.

24. Apparatus according to claim 23, wherein the at least one ball joint comprises at least one swivel ball of at least one ball joint end fitting for cooperating with an attachment pin of its respective attachment device.

25. Apparatus according to claim 23, wherein the at least one ball joint comprises:

at least one swivel ball supported by the attachment device so that in use the swivel ball projects above a root portion of its blade; and

at least one sleeve of an elbow end fitting for removably attaching the linear actuator, the at least one sleeve being configured to fit and be releasably locked onto said swivel ball.

26. Apparatus according to claim 25, wherein the at least one swivel ball is supported by a support retained by at least one pin or screw in at least one insert of the attachment device which is integrated into a root portion of its blade.

27. Apparatus according to claim 25, wherein the at least one swivel ball is supported by a support integrated as an insert in a root portion of its blade.

28. Apparatus according to claim 23, wherein at least one attachment device comprises at least one attachment element fitted by a removable attachment into at least one insert integrated into a root portion of the blade.

29. Apparatus according to claim 23, wherein at least one attachment device is configured to be removably fitted to its respective blade.

30. Apparatus according to claim 29, wherein the at least one attachment device comprises a retaining collar supporting one of a swivel or a pin cooperating with a swivel ball, the retaining collar being removable and configured to grip part of a root portion of a blade and be locked thereto by snug fitting and by a spacer keeping the retaining collar radially spaced towards the outside of the pivot axis of the blade, about which the spacer is pivotable with the retaining collar and the blade.