Helicopter collective stick of the displacement type occupying a minimum space envelope yet whose grip generates an arc of large radius

• US 5,156,363 A
• Filed: 02/28/1991
• Issued: 10/20/1992
• Est. Priority Date: 02/28/1991
• Status: Expired due to Fees

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Rozak, James N., Cizewski, Steven C., Lange, William F.
• Primary Examiner(s): Peters, Jr., Joseph F.
• Assistant Examiner(s): Ellis, Christopher P.
• Application Number:
  US07/661,940
• Time in Patent Office: 600 Days
• Field of Search: 244/223, 244/229, 244/222, 244/232, 244/75 R, 244/220, 244/236, 244/234, 244/17.13, 74/479, 74/480 R
• US Class Current: 244/223
• CPC Class Codes: B64C 27/56 characterised by the control initiating means, e.g. manually actuated

Abstract

A helicopter collective control stick having a pilot grip positioned by a linkage assembly whose kinematics permits the control stick to occupy a small envelope and to have the pilot grip motion to be about a large radius. Our collective stick includes a biasing member to balance the control stick and linkage in the mid collective position and which provides a force gradient when the control stick is moved from the mid collective or trimmed position. Further, our collective stick is operable in concert with the full authority side arm controller to operate in either a tracking or a command mode.

Claims

1. A helicopter collective pitch control stick of the displacement type which occupies a minimum space envelope and whose pilot grip motion generates a large radius arc comprising:

a. a pilot grip member;

b. a linkage assembly connected to and operable by the pilot grip member and comprising;

1) a first link having first and second ends, and with its first end pivotally connected to a fixed station;

2) a second link having first and second ends, and with its second end integrally connected to the pilot grip member;

3) a third link having first and second ends, and having its first end pivotally connected to the first end of the second link and its second end pivotally connected to the first link at a selected station between the first link'"'"'s first and second ends; and

4) a fourth link extending substantially parallel to the third link and having first and second ends and having its first end pivotally connected to the second link at a selected station between the first and second ends of the second link, and having its second end pivotally connected to the second end of the first link;

said links being of selected length and the pivot connections between said links being selectively positioned so that the pilot grip member and the link assembly occupy a small space envelope and so that the motion of the pilot grip member generates an arc of large radius;

c. a positioning means connected to said linkage assembly and operable to cause motion of the linkage assembly to selectively position the pilot grip member.

2. A helicopter control stick as in claim 1 and including biasing means operatively connected to the linkage assembly and biased to maintain the pilot grip member in its mid-collective pitch position thereby negating the weight and inertia of the linkage mechanism and the grip member, and further to provide increasing resistance as the pilot moves the collective stick from its mid-collective or trimmed position so as to provide the pilot feel for the amount of collective pitch being called for by the control stick.

3. A helicopter control stick as in claim 2 wherein the biasing means are preloaded coil springs operatively connected to the linkage assembly.

4. A helicopter control stick as in claim 3 and including stop members operatively associated with the linkage assembly and operable to prevent motion of the linkage assembly and the grip member beyond a selected lowest collective pitch position and a selected highest collective pitch position.

6. A helicopter control stick according to claim 1 and further including a force/displacement type side arm controller operable to produce collective pitch, cyclic pitch, and helicopter yaw command signal in the fly-by-wire mode, electronic control means connecting said side arm controller to said collective stick and operable to place the collective stick in a tracking mode in which the position of the collective stick is an indicator of the collective pitch command generated by the side arm controller and so that the tracking collective stick provides displacement feedback to the pilot.

7. A helicopter control stick as in claim 6 and including means to disengage the collective stick from the control of the side arm controller to permit pilot operation of the collective stick.

8. A helicopter control stick according to claim 6 wherein the connecting means includes an input crank member connected to the linkage assembly, and

a. electric motor operatively connected to the crank to cause rotation thereof in either a clockwise or counterclockwise direction, and

b. means to drive the motor as a function of the side arm controller collective pitch command to thereby place the collective stick in said tracking mode.

9. A helicopter control stick according to claim 8 wherein said motor drive means includes a motor driven gear operatively connected to said motor to be driven in either a clockwise or counterclockwise direction thereby, a drive gear operatively connected to the input crank to cause the crank to rotate in either a clockwise or counterclockwise direction, an idler gear connected to a rotational variable displacement transducer (RVDT) operable to transmit a collective gear position signal to the electronic control, a member engaging each of said gears so that rotation of the motor driven gear by the electric motor will position the input crank and therefore the collective stick, and also send at least one collective stick position signal back to the electronic control means.

10. A helicopter control stick according to claim 9 wherein said gear engaging means is a continuous chain, and including means to control the tension of said chain.

11. A helicopter control stick according to claim 8 and including pilot operable means to prevent the motor from driving the linkage assembly and grip member so as to place the collective pitch stick in manual mode with the motor operative to provide electric damping to control stick motion.

12. A helicopter control stick according to claim 8 and including a pilot operated trim command operable to cause the motor drive means to maintain the trimmed collective stick position to maintain a fixed collective pitch and so that motor torque provides resistance when the pilot attempts to move the collective stick from the trimmed position.

5. A helicopter control stick according to claim wherein the positioning means is an input crank, and including mechanical means for positioning said input crank to control said collective pitch control stick position, or to provide a signal of collective pitch control stick position.

13. An operator control stick of the displacement type which occupies a minimum space envelope and whose grip motion generates a large radius arc comprising:

a. an operator grip member; and

b. a linkage assembly connected to and operable by the grip member and comprising;

1) a first link having first and second ends, and with its first end pivotally connected to a fixed station;

2) a second link having first and second ends, and with its second end integrally connected to the grip member;

3) a third link having first and second ends, and having its first end pivotally connected to the first end of the second link and its second end pivotally connected to the first link at a selected station between the first link'"'"'s first and second ends; and

4) a fourth link extending substantially parallel to the third link and having first and second ends and having its first end pivotally connected to the second link at a selected station between the first and second ends of the second link, and having its second end pivotally connected to the second end of the first link;

said links being of selected length and the pivot connections between said links being selectively positioned so that the grip member and the link assembly occupy a small space envelope and so that the motion of the grip member generates an arc of large radius.

14. A control stick according to claim 13 and further including means connected to said linkage assembly and operable to either cause motion of the linkage assembly to selectively position the grip member, or generate a grip member position indicator signal.

15. A control stick as in claim 13 and including biasing means operatively connected to the linkage assembly and biased to maintain the operator grip member in its mid position thereby negating the weight and inertia of the linkage mechanism and the grip member, and further to provide increasing resistance as the operator moves the control stick from its mid position so as to provide the operator feel for the amount of change being called for by the control stick.

16. A control stick as in claim 15 wherein the biasing means are preloaded coil springs operatively connected to the linkage assembly.

17. A control stick according to claim 15 and wherein the linkage assembly motion causing means is an input crank, and an electric motor operable to rotate such input crank to thereby actuate said linkage assembly to move said control stick so that the operator grip member generates a large radius arc.

18. A helicopter control stick according to claim 15 and wherein said linkage assembly motion causing means is an input crank, and mechanical means to either impart motion to said input crank to cause said linkage assembly to move said control stick, or to serve as a position indicator of control stick position.