Adjustment of track and balance of a multi-blade rotor

Patent metadata

Field	Value
Publication number	US-10870484-B2
Application number	US-201715704185-A
Country	US
Kind code	B2
Filing date	Sep 14, 2017
Priority date	Sep 15, 2016
Publication date	Dec 22, 2020
Grant date	Dec 22, 2020

Abstract

A multi-blade rotor of a rotary wing aircraft, the multi-blade rotor comprising at least one rotor blade that defines a pitch axis and that is provided with an associated pitch-control lever that is operatively coupled to a pitch link rod, the pitch link rod defining a longitudinal axis, wherein the associated pitch-control lever comprises an accommodation that is located on the longitudinal axis of the pitch link rod at a predetermined distance from the pitch axis of the at least one rotor blade, the pitch link rod being operatively coupled to the associated pitch-control lever at the accommodation of the associated pitch-control lever, wherein the predetermined distance is adjustable in order to enable adjustment of track and balance of the multi-blade rotor.

First claim

What is claimed is:

1. A multi-blade rotor of a rotary wing aircraft, the multi-blade rotor comprising at least one rotor blade that defines a pitch axis, the at least one rotor blade being provided with an associated pitch-control lever that is operatively coupled to a pitch link rod, the pitch link rod defining a longitudinal axis, wherein the associated pitch-control lever comprises an accommodation that is located on the longitudinal axis of the pitch link rod at a predetermined distance from the pitch axis of the at least one rotor blade, the pitch link rod being operatively coupled to the associated pitch-control lever at the accommodation of the associated pitch-control lever,
wherein the associated pitch-control lever has a pitch horn that forms and defines a bushing accommodation that extends through the pitch horn, the bushing accommodation being provided with an exchangeable bushing that provides the accommodation of the associated pitch-control lever so that the predetermined distance is adjustable in order to adjust the pitching angle of the corresponding blade and thereby adjust of track and balance of the multi-blade rotor independent from an adjustment of a length of the pitch link rod.

2. The multi-blade rotor of claim 1 ,
wherein the exchangeable bushing is arranged in a supplementary bushing that defines the bushing accommodation, the supplementary bushing being arranged in an associated accommodation provided in the associated pitch-control lever.

3. The multi-blade rotor of claim 1 ,
wherein the exchangeable bushing comprises an at least partly serrated inner contour.

4. The multi-blade rotor of claim 3 ,
wherein a connector with an at least partly serrated outer contour is arranged in the exchangeable bushing, the at least partly serrated outer contour matching the at least partly serrated inner contour of the exchangeable bushing, wherein the connector operatively couples the associated pitch-control lever to the pitch link rod.

5. The multi-blade rotor of claim 3 ,
wherein an insert with an at least partly serrated outer contour is arranged in the exchangeable bushing, the at least partly serrated outer contour matching the at least partly serrated inner contour of the exchangeable bushing, wherein the insert provides the accommodation of the associated pitch-control lever.

6. The multi-blade rotor of claim 1 ,
wherein the bushing accommodation is provided with a torque-transferring inner contour, and wherein the exchangeable bushing comprises a torque-transferring outer contour, the torque-transferring outer contour matching the torque-transferring inner contour, wherein the exchangeable bushing provides the accommodation of the associated pitch-control lever, the accommodation being arranged eccentrically on the exchangeable bushing.

7. The multi-blade rotor of claim 1 ,
wherein the bushing accommodation is provided with the exchangeable bushing that is at least partly arranged in the bushing accommodation and that provides the accommodation of the associated pitch-control lever, the accommodation of the associated pitch-control lever being arranged eccentrically on the exchangeable bushing.

8. The multi-blade rotor of claim 7 ,
wherein the exchangeable bushing comprises an elongated flange that is attached to the associated pitch-control lever by means of an associated fixation member, the elongated flange comprising an associated opening for arrangement of the associated fixation member and being releasable for enabling rotation of the exchangeable bushing in the bushing accommodation.

9. The multi-blade rotor of claim 8 ,
wherein the associated pitch-control lever comprises a plurality of openings that are adapted for receiving the associated fixation member.

10. The multi-blade rotor of claim 7 ,
wherein the exchangeable bushing comprises a semi-circular flange that is attached to the associated pitch-control lever by means of an associated fixation member, the semi-circular flange comprising a plurality of openings for a selective arrangement of the associated fixation member and being releasable for enabling rotation of the exchangeable bushing in the bushing accommodation.

11. The multi-blade rotor according to claim 10 ,
wherein the associated pitch-control lever comprises a single opening for receiving the associated fixation member.

12. The multi-blade rotor of claim 10 ,
wherein the plurality of openings is arranged on at least two separate arc-shaped arrangement patterns, wherein the associated pitch-control lever comprises a separate opening for each one of the at least two separate arc-shaped arrangement patterns, each separate opening being provided for selectively receiving the associated fixation member.

13. The multi-blade rotor of claim 1 ,
wherein the bushing accommodation is provided with the exchangeable bushing that is at least partly arranged in the bushing accommodation and that comprises an L-shaped flange, the accommodation of the associated pitch-control lever being arranged on the L-shaped flange that is attached to the associated pitch-control lever by means of an associated fixation member.

14. The multi-blade rotor of claim 1 ,
wherein the accommodation of the associated pitch-control lever is relocated by filling the accommodation with an associated filling material and recreating the accommodation at a distinct predetermined location on the associated pitch-control lever.

15. A multi-blade rotor of a rotary wing aircraft, the multi-blade rotor comprising:
a rotor blade that defines a pitch axis, the rotor blade having a pitch-control lever, the pitch-control lever with a pitch horn, the pitch horn forming and defining a bushing accommodation aperture that extends through the pitch horn;
an exchangeable bushing received within the bushing accommodation aperture such that an outer wall of the exchangeable bushing mates with an inner wall of the bushing accommodation aperture, the exchangeable bushing defining a bearing accommodation aperture therethrough;
a pitch link rod defining a longitudinal axis, the pitch link rod extending through the bearing accommodation aperture such that the pitch link rod is rotatably coupled to the pitch-control lever via the bearing accommodation aperture;
wherein the bearing accommodation aperture is located along the longitudinal axis of the pitch link rod such that the longitudinal axis intersects both the inner wall of the bushing accommodation aperture and an inner wall of the bearing accommodation aperture, and wherein the bearing accommodation aperture is located at a predetermined distance from the pitch axis of the rotor blade; and
wherein a pitching angle of the rotor blade is adjusted via setting the predetermined distance of the bearing accommodation aperture to thereby adjust a track and balance of the rotor blade independent from an adjustment of a length of the pitch link rod.

16. The multi-blade rotor of claim 15 wherein the bushing accommodation aperture is elongated; and
wherein the exchangeable bushing has an elongated outer contour sized to be received within the elongated bushing accommodation aperture.

17. The multi-blade rotor of claim 15 wherein the bearing accommodation aperture of the exchangeable bushing is elongated and is defined by a serrated inner contour; and
wherein the pitch link rod is connected to the pitch-control lever via a pitch link rod having a serrated outer contour, the serrated outer contour sized to mate with the serrated inner contour of the exchangeable bushing to locate the pitch link rod and set the predetermine

Assignees

• Airbus Helicopters Deutschland GmbH

Inventors

• Buesing Moritz

Classifications

• B64C27/008 Primary

  Rotors tracking or balancing devices · CPC title

• B64C27/605

  including swash plate, spider or cam mechanisms · CPC title

• B64C11/32

  mechanical · CPC title

• B64C27/32

  Rotors · CPC title

• B64C27/59 Primary

  mechanical · CPC title