Compact two axis gimbal for control stick

• US 9,126,676 B2
• Filed: 10/22/2012
• Issued: 09/08/2015
• Est. Priority Date: 10/28/2011
• Status: Active Grant

• Current Assignee: Woodward MPC, Inc.
• Original Assignee: Woodward MPC, Inc.
• Inventors: DeCraene, Matthew P., Kramer, Matthew, Thompson, Nathan, Petrou, Anton
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Green, Richard R
• Application Number:
  US13/657,294
• Publication Number:
  US 20130105634A1
• Time in Patent Office: 1,051 Days
• Field of Search: 244/223, 244/231, 244/237, 475/4
• US Class Current: 1/1
• CPC Class Codes: B64C 13/0421 control sticks for primary flight controls
• CPC Class Codes: B64C 13/46 with artificial feel
• CPC Class Codes: G05G 2009/04718 with cardan or gimbal type joint
• CPC Class Codes: G05G 5/03 Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a counterforce arrangements for indicating the position of the controlling member G05G1/015
• CPC Class Codes: G05G 9/047 the controlling member being movable by hand about orthogonal axes, e.g. joysticks for switches H01H25/04

Abstract

An electromechanical portion of the control stick includes a two-axis gimbal, with each axis including a mechanical gimbal structure supported by rolling element bearings, cam based centering mechanisms, linkages to connect a geared power-drive including a resolver commutated brushless DC motor and compound-planetary gearhead to provide active force feedback, and several electrically independent RVDT position sensors. The gearing architecture uses a fixed-cage, rotating internal gear arrangement on a planetary gearhead, which may be single or multi-stage. The output torque of the gearhead is provided by a feature on the outer housing of the rotating internal ring gear, allowing an axial placement of the entire power-drive in a more central location, reducing the moment load on the gearhead output cage bearings, and facilitating a compact drive arrangement of the gimbal using linkages. Additionally, a common power-drive can be used for both the roll and pitch axes.

Claims

1. A compact two-axis control stick comprising:

a pilot input device pivotable about a pitch axis and a roll axis;

a pitch force feedback drive including;

a pitch motor including an output shaft;

a pitch gear train including a pitch sun gear mounted to the output shaft of the pitch motor, a plurality of pitch planet gears mounted to a permanently fixed position pitch carrier, and a pitch ring gear, the plurality of pitch planet gears radially positioned between the pitch sun gear and the pitch ring gear;

a roll force feedback drive including;

a roll motor including an output shaft;

a roll gear train including a roll sun gear mounted to the output shaft of the roll motor, a plurality of roll planet gears mounted to a fixed position roll carrier, and a roll ring gear, the plurality of roll planet gears radially positioned between the roll sun gear and the roll ring gear; and

a pitch linkage operably coupling the pitch force feedback drive to the pilot input device, the pitch linkage being operably coupled to the pilot input device and the pitch ring gear such that rotation of the pitch ring gear causes rotation of the pilot input device about the pitch axis;

a roll linkage operably coupling the roll force feedback drive to the pilot input device, the roll linkage being operably coupled to the pilot input device and the roll ring gear such that rotation of the roll ring gear causes rotation of the pilot input device about the roll axis.

2. The control stick of claim 1, wherein the roll force feedback drive and the pitch force feedback drive are substantially identical.

3. The control stick of claim 1, wherein the pitch motor output shaft rotates about a rotational axis that is parallel to the pitch axis and the roll motor output shaft rotates about a rotational axis that is parallel to the roll axis, the rotational axes of the pitch motor output shaft and the roll motor output shaft being general perpendicular to one another.

4. The control stick of claim 1, further comprising:

a pitch centering mechanism acting on the pilot input device to bias the pilot input device to a pitch home position when the pilot input device is rotated about the pitch axis away from the pitch home position; and

a roll centering mechanism acting on the pilot input device to bias the pilot input device to a roll home position when the pilot input device is rotated about the roll axis away from the roll home position.

5. The control stick of claim 1, further comprising a base frame to which the pilot input device is operably pivotably mounted for rotation about the pitch and roll axes, the fixed position pitch carrier defining a rotational axis for each of the plurality of pitch planet gears, the fixed position pitch carrier having a fixed position relative to the base frame and maintaining the rotational axes of the plurality of pitch planet gears in a fixed position relative to the base frame;

and

the fixed position roll carrier defining a rotational axis for each of the plurality of roll planet gears, the fixed position roll carrier having a fixed position relative to the base frame and maintaining the rotational axes of the plurality of roll planet gears in a fixed position relative to the base frame.

6. The control stick of claim 1, wherein the pitch ring gear includes a radially outward extending attachment feature, the pitch linkage pivotally operably connected to the radially outward extending attachment feature of the pitch ring gear proximate a first end of the pitch linkage and the pitch linkage is pivotally operably connected to the pilot input device proximate a second end of the pitch linkage;

and

wherein the roll ring gear includes a radially outward extending attachment feature, the roll linkage pivotally operably connected to the radially outward extending attachment feature of the roll ring gear proximate a first end of the roll linkage and the roll linkage is pivotally operably connected to the pilot input device proximate a second end of the roll linkage.

7. The control stick of claim 6, wherein the pitch ring gear has a first end adjacent the pitch motor and a second end, opposite the first end, the second end is spaced away from the pitch motor with the first end positioned axially between the second end and the pitch motor along an axis defined by the pitch motor output shaft, the radially outward extending attachment feature of the pitch ring gear does not extend axially outward beyond the second end;

and

wherein the roll ring gear has a first end adjacent the roll motor and a second end, opposite the first end, the second end is spaced away from the roll motor with the first end positioned axially between the second end and the roll motor along an axis defined by the roll motor output shaft, the radially outward extending attachment feature of the roll ring gear does not extend axially outward beyond the second end.

8. The control stick of claim 6, further comprising a pair of axially spaced apart gearhead carrier bearings radially supporting the pitch ring gear for rotation, the radially outward extending attachment feature of the pitch ring gear is positioned axially adjacent one of the gearhead carrier bearings;

and

a pair of axially spaced apart gearhead carrier bearings radially supporting the roll ring gear for rotation, the radially outward extending attachment feature of the roll ring gear positioned axially adjacent one of the gearhead carrier bearings.

9. The control stick of claim 8, wherein the radially outward extending attachment feature of the pitch ring gear has a single leg that extends radially outward and the pitch linkage is operably connected on a side of the leg;

and

wherein the radially outward extending attachment feature of the roll ring gear has a single leg that extends radially outward and the roll linkage is operably connected on a side of the leg.

10. The control stick of claim 9, wherein the pitch linkage is connected on a pitch motor side of the leg of the pitch ring gear such that it is substantially in line with the roll axis of rotation;

and

wherein the roll linkage is connected on a side of the leg opposite the roll motor with the roll linkage positioned axially between the pair of gear head carrier bearings.

11. A method of providing force feedback to a pilot input device comprising:

sensing a displacement of the pilot input device about a pitch axis;

providing pitch force feedback to bias the pilot input device back toward a pitch home position using a pitch force feedback drive operably connected to the pilot input device with a pitch linkage, the pitch force feedback drive including;

a pitch motor including an output shaft; and

a pitch gear train including a pitch sun gear mounted to the output shaft of the pitch motor, a plurality of pitch planet gears mounted to a permanently fixed position pitch carrier, and a pitch ring gear, the plurality of pitch planet gears radially positioned between the pitch sun gear and the pitch ring gear, the pitch linkage operably coupled to the pitch ring gear;

sensing a displacement of the pilot input device about a roll axis; and

providing roll force feedback to bias the pilot input device back toward a roll home position using a roll force feedback drive operably connected to the pilot input device with a roll linkage, the roll force feedback drive including;

a roll motor including an output shaft; and

a roll gear train including a roll sun gear mounted to the output shaft of the roll motor, a plurality of roll planet gears mounted to a fixed position roll carrier, and a roll ring gear, the plurality of roll planet gears radially positioned between the roll sun gear and the roll ring gear, the roll linkage operably coupled to the roll ring gear.

12. The method of claim 11, wherein the pitch ring gear includes a radially outward extending attachment feature, the pitch linkage pivotally connected to the radially outward extending attachment feature of the pitch ring gear proximate a first end of the pitch linkage and the pitch linkage is pivotally connected to the pilot input device proximate a second end of the pitch linkage;

and

wherein the roll ring gear includes a radially outward extending attachment feature, the roll linkage pivotally connected to the radially outward extending attachment feature of the roll ring gear proximate a first end of the roll linkage and the roll linkage is pivotally connected to the pilot input device proximate a second end of the roll linkage.

13. The method of claim 12, wherein the pitch ring gear has a first end adjacent the pitch motor and a second end, opposite the first end, the second end is spaced away from the pitch motor with the first end positioned axially between the second end and the pitch motor along an axis defined by the pitch motor output shaft, the radially outward extending attachment feature of the pitch ring gear being positioned inward from the second end of the pitch ring gear towards the pitch motor;

and

wherein the roll ring gear has a first end adjacent the roll motor and a second end, opposite the first end, the second end is spaced away from the roll motor with the first end positioned axially between the second end and the roll motor along an axis defined by the roll motor output shaft, the radially outward extending attachment feature of the roll ring gear being positioned inward from the second end of the roll ring gear towards the roll motor.

14. The method of claim 13, further comprising a pair of axially spaced apart gearhead carrier bearings radially supporting the pitch ring gear for rotation, the radially outward extending attachment feature of the pitch ring gear is positioned axially adjacent the gearhead carrier bearing axially closest the pitch motor;

and

a pair of axially spaced apart gearhead carrier bearings radially supporting the roll ring gear for rotation, the radially outward extending attachment feature of the roll ring gear is positioned axially adjacent the gearhead carrier bearing axially closest the pitch motor.

15. An apparatus for providing force feedback to a pilot input device comprising:

a force feedback drive including;

a motor including an output shaft; and

a gear train including a sun gear mounted to the output shaft of the motor, a plurality of planet gears mounted to a fixed position carrier, the fixed position carrier being fixed during all phases of operation, and a ring gear, the plurality of planet gears radially positioned between the sun gear and the ring gear; and

a linkage configured to operably couple the force feedback drive to the pilot input device, the linkage is configured to be operably coupled to the pilot input device, the linkage being operably coupled to the ring gear such that rotation of the pitch ring gear causes motion of the linkage.

16. The apparatus of claim 15, wherein the fixed position carrier defines a rotational axis for each of the plurality of planet gears, the fixed position carrier having a fixed position relative to motor and maintaining the rotational axes of the plurality of planet gears in a fixed position relative to the motor.

17. The apparatus of claim 15, wherein the ring gear includes a radially outward extending attachment feature, the linkage pivotally connected to the radially outward extending attachment feature of the ring gear proximate a first end of the linkage.

18. The apparatus of claim 17, wherein the ring gear has a first end adjacent the motor and a second end, opposite the first end, the second end is spaced away from the motor with the first end positioned axially between the second end and the motor along an axis defined by the motor output shaft, the radially outward extending attachment feature not extending axially beyond the second end of the ring gear in a direction extending away from the motor.

19. The apparatus of claim 17, further comprising a pair of axially spaced apart gearhead carrier bearings rotatably supporting the ring gear for rotation, the radially outward extending attachment feature being substantially axially centered relative to the gearhead carrier bearings.

20. The control stick of claim 19, wherein the radially outward extending attachment feature of the ring gear has a single leg that extends radially outward and the linkage is connected to a side of the leg but does not extend axially beyond an end of the ring gear opposite the motor.