Free play chatter suppression

Patent metadata

Field	Value
Publication number	US-12234015-B2
Application number	US-202318338463-A
Country	US
Kind code	B2
Filing date	Jun 21, 2023
Priority date	Jun 21, 2023
Publication date	Feb 25, 2025
Grant date	Feb 25, 2025

Abstract

An apparatus and method for suppressing free play chatter of a control surface of an aircraft. The free play chatter suppression apparatus includes a containment vessel connected to a control surface of an aircraft. A lossy material is contained within the containment vessel. A body is positioned within the lossy material. The deceleration of the body by the lossy fluid is transmitted to the control surface to dampen vibrations of the control surface.

First claim

What is claimed is:

1. An apparatus configured to suppress free play chatter, wherein the apparatus comprises:
a containment vessel mounted to a pivot axis of a control surface of an aircraft, wherein the containment vessel is configured to move with the control surface as the control surface pivots about the pivot axis;
a lossy material contained within the containment vessel; and
a body positioned within the lossy material.

2. The apparatus of claim 1 , wherein the containment vessel is positioned within a volume defined by the control surface of the aircraft.

3. The apparatus of claim 1 , wherein the-body within the lossy material is suspended within the lossy material without any direct connection between the body and the containment vessel.

4. The apparatus of claim 3 , wherein the pivot axis is grounded to a structural component of the aircraft.

5. The apparatus of claim 1 , wherein the control surface of the aircraft is selected from at least one of a flap, an elevator, a rudder, and a ruddervator.

6. The apparatus of claim 1 , further comprising an actuator having a geared transmission, the actuator connected to the control surface, wherein the geared transmission includes discontinuities that result in free play of the control surface.

7. The apparatus of claim 1 , wherein the lossy material is tunable.

8. The apparatus of claim 1 , wherein the lossy material is a viscous or viscoelastic material.

9. The apparatus of claim 1 , wherein the lossy material has a bulk modulus in a range of 1 to 2 GPa.

10. The apparatus of claim 1 , wherein a ratio of a mass of the control surface to a mass of the body is in a range of 10 to 50.

11. The apparatus of claim 1 , further comprising a connector connected to the body and the containment vessel within the lossy material.

12. The apparatus of claim 1 , wherein the body is suspended within the lossy material with no direct connection to the containment vessel.

13. A system configured to suppress free play chatter of a control surface of an aircraft, wherein the system comprises:
the control surface of the aircraft;
an actuator having a geared transmission, the actuator connected to the control surface;
a containment vessel mounted to a pivot axis of the control surface of the aircraft, wherein the containment vessel is configured to move with the control surface as the control surface pivots about the pivot axis;
a lossy material contained within the containment vessel; and
a body suspended within the lossy material.

14. The system of claim 13 , wherein the containment vessel is positioned within a volume defined by the control surface of the aircraft.

15. The system of claim 13 , wherein the control surface is directly connected to the pivot axis.

16. The system of claim 13 , wherein the containment vessel moves with movement of the control surface.

17. A method for suppressing free play chatter of a control surface of an aircraft, the method comprising:
mounting an actuator to the aircraft, wherein the actuator has at least one of a geared transmission or a linkage;
connecting the control surface of the aircraft to the actuator, wherein the control surface includes a pivot axis;
mounting a containment vessel to the pivot axis of the control surface;
moving the containment vessel with the control surface while pivoting the control surface about the pivot axis;
placing a lossy material within the containment vessel; and
positioning a body within the lossy material.

18. The method of claim 17 , wherein the containment vessel is positioned within a volume defined by the control surface of the aircraft.

19. The method of claim 17 , wherein the containment vessel is directly connected to the pivot axis.

20. The method of claim 17 , wherein positioning the body within the lossy material comprises suspending the body within the lossy material without any direct connection between the body and the containment vessel.

Assignees

• Boeing Co

Inventors

• Griffin Steven F
• Endsley Zackary L

Classifications

• F16F1/36

  made of rubber or other material having high internal friction, {e.g. thermoplastic elastomers (spring units consisting of several springs F16F3/08)} · CPC title

• F16F7/112

  on fluid springs · CPC title

• F16F7/108

  on plastics springs · CPC title

• F16F7/10

  using inertia effect (F16F13/108, F16F13/22, F16F15/10, F16F15/22 take precedence; stabilising vehicle bodies by means of movable masses B62D37/04; protection of buildings against vibrations or shocks by mass dampers E04H9/0215; arrangements or devices for damping mechanical oscillations of power lines H02G7/14) · CPC title

• B64C9/02 Primary

  Mounting or supporting thereof · CPC title