Separation of collective and cyclic actuation

Patent metadata

Field	Value
Publication number	US-10836478-B2
Application number	US-201615246254-A
Country	US
Kind code	B2
Filing date	Aug 24, 2016
Priority date	Aug 24, 2015
Publication date	Nov 17, 2020
Grant date	Nov 17, 2020

Abstract

A rotor actuation system includes a swashplate assembly comprised of a stationary swashplate and a rotating swashplate operatively connected together for relative rotation about a rotor axis. A cyclic actuator is operatively connected to the stationary swashplate to tilt the swashplate assembly off axis from the rotor axis for cyclic control. A collective actuator is operatively connected to the swashplate assembly to move the swashplate axially along the rotor axis for collective control. The cyclic actuator and the collective actuator are operatively connected to the swashplate assembly to respectively actuate cyclic and collective control independent of one another.

First claim

What is claimed is:

1. A rotor actuation system comprising:
a counter rotating co-axial main rotor assembly including a lower rotor assembly and an upper rotor assembly;
a first swashplate assembly including a first stationary swashplate and a first rotatable swashplate operatively connected to the lower rotor assembly, the first stationary swashplate being operatively connected to the first rotatable swashplate, wherein the first rotatable swashplate is rotatable relative to the first stationary swashplate about a rotor axis;
a second swashplate assembly including a second stationary swashplate and a second rotatable swashplate operatively connected to the upper rotor assembly, the second stationary swashplate being operatively connected to the second rotatable swashplate, wherein the second rotatable swashplate is rotatable relative to the second stationary swashplate about the rotor axis;
two dual-stage mono-cyclic actuators, each of the two dual-stage mono-cyclic actuators operatively connected to a respective one of the first stationary swashplate and the second stationary swashplate to rotate the respective one of the first and second swashplate assemblies off axis from the rotor axis for cyclic control of one of the lower and upper rotor assemblies for roll and the other of the lower and upper rotor assemblies for pitch; and
a dual-stage hydraulic collective actuator including a plurality of compartments operatively connected to the swashplate assembly independent of the dual-stage mono-cyclic actuators, the dual-stage hydraulic collective actuator being operable to move the stationary swashplate axially along the rotor axis for collective control by selectively pressurizing select ones of the plurality of compartments, wherein the dual-stage mono-cyclic actuator and the dual-stage hydraulic collective actuator are operatively connected to the swashplate assembly to respectively actuate cyclic and collective control independent of one another.

2. The rotor actuation system as recited in claim 1 , further comprising a main rotor assembly operatively connected to the swashplate assembly for collective and cyclic control of the main rotor assembly.

3. The rotor actuation system as recited in claim 1 , further comprising:
a propulsor rotor assembly operatively connected to the rotating swashplate for collective and cyclic control of the propulsor rotor assembly; or
a tail rotor assembly operatively connected to the rotating swashplate for collective and cyclic control of the tail rotor assembly.

4. The rotor actuation system as recited in claim 1 , wherein the stationary swashplate is pinned to a slider for rotation about a cyclic rotation axis substantially perpendicular to the rotor axis.

5. The rotor actuation system as recited in claim 1 , further comprising:
a standpipe extending along the rotor axis; and
a slider translationally engaged to the standpipe, wherein the swashplate assembly is mounted to the slider, and wherein the dual-stage hydraulic collective actuator is operatively connected to the standpipe and the slider to actuate the standpipe and the slider axially relative to one another along the rotor axis for collective control.

6. The rotor actuation system as recited in claim 5 , wherein the dual-stage mono-cyclic actuator is mounted between the slider and the stationary swashplate to locally tilt the stationary swashplate and slider toward and away from a common axis.

7. The rotor actuation system as recited in claim 1 , further comprising a bearing element between the swashplate assembly and the rotor axis or slider, wherein the bearing element forms a pivot point for off axis rotation of the swashplate assembly relative to the rotor axis/slider.

8. The rotor actuation system as recited in claim 1 , wherein the dual-stage hydraulic collective actuator is a hydraulic actuator in an annular space between the standpipe and the slider.

9. The rotor actuation system as recited in claim 1 , wherein the dual-stage hydraulic collective actuator is mounted to the standpipe and slider externally.

10. The rotor actuation system as recited in claim 1 , wherein the dual-stage mono-cyclic actuator includes a plurality of actuator stages.

11. The rotor actuation system as recited in claim 1 , wherein the dual-stage hydraulic collective actuator includes a plurality of actuator stages.

12. The rotor actuation system as recited in claim 1 , wherein at least one of the dual-stage mono-cyclic and the dual-stage hydraulic collective actuator defines an actuator axis of motion that is angled relative to the rotor axis.

13. A control system for rotor actuation comprising:
a rotor actuation system as recited in claim 1 ; and
a controller operatively connected to the cyclic and collective actuators, wherein the controller is configured to receive command input and issue commands to the dual-stage cyclic and the dual-stage hydraulic collective actuator for independent actuation of collective and cyclic motion on the swashplate assembly based on the command input.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Halcom Lance

Classifications

• B64C27/64

  using fluid pressure, e.g. having fluid power amplification · CPC title

• B64C27/68

  using electrical energy, e.g. having electrical power amplification · CPC title

• B64C27/605 Primary

  including swash plate, spider or cam mechanisms · CPC title