Counterbalance unit

Patent metadata

Field	Value
Publication number	US-10114406-B2
Application number	US-201414901750-A
Country	US
Kind code	B2
Filing date	Jun 27, 2014
Priority date	Jul 1, 2013
Publication date	Oct 30, 2018
Grant date	Oct 30, 2018

Abstract

A vibration damping counterbalance unit for an inceptor apparatus having a wall defining a cavity; and a plurality of vibration damping masses housed within the cavity.

First claim

The invention claimed is:

1. An inceptor apparatus for an aircraft, the apparatus comprising:
a control stick having a grip portion at one end of the control stick; and
a vibration damping counterbalance unit operatively coupled to an end of the control stick opposite the end having the grip portion, the vibration damping counterbalance unit including a wall defining a cavity, and a plurality of vibration damping masses housed within the cavity,
wherein the control stick is configured to pivot about a point between each end of the control stick.

2. The inceptor apparatus as claimed in claim 1 , wherein the cavity is configured such that the vibration damping masses are free to move in any direction relative to the cavity wall and each other.

3. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping masses are substantially spherical.

4. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping masses comprise a metal having a density of at least 15 g/cm 3 .

5. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping masses have a vickers hardness of at least 2600 MPa.

6. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping masses substantially comprise a tungsten alloy.

7. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping masses have a diameter of at least 2.0 mm but no greater than about 5.0 mm.

8. The inceptor apparatus as claimed in claim 1 , wherein a diameter of at least one of the vibration damping masses is a function of a counterbalance mass, a density of vibration mass material forming at least one of the vibration damping masses, a vibration damping counterbalance unit envelope, and a free space volume in the cavity.

9. The inceptor apparatus as claimed in claim 1 , wherein only one cavity houses the vibration damping masses.

10. The inceptor apparatus as claimed in claim 1 , further comprising at least one internal dividing wall to define at least one additional cavity to house vibration damping masses.

11. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping counterbalance unit is removeably fixed to the control stick.

12. The inceptor apparatus as claimed in claim 1 , wherein the control stick is pivotably mounted such that it may move in at least one of a first direction and second direction, the second direction being at right angles to the first direction.

13. The inceptor apparatus as claimed in claim 1 , wherein free space volume in the cavity is at least 15% of the volume of the cavity.

14. The inceptor apparatus as claimed in claim 1 , wherein the cavity includes an internal dividing wall defining at least one additional cavity to house vibration damping masses.

15. The inceptor apparatus as claimed in claim 1 , wherein the vibration damping counterbalance unit is removeably fixed to the control stick.

Assignees

• Bae Systems Plc

Inventors

• White Nicholas James
• Wasson Robert Maxwell

Classifications

• B64C13/10

  comprising warning devices · CPC title

• G05G9/047

  the controlling member being movable by hand about orthogonal axes, e.g. joysticks {(for switches H01H25/04)} · CPC title

• G05G25/02 Primary

  Inhibiting the generation or transmission of noise {(suppression of noise or vibrations in selector apparatus for gearings F16H59/0208)} · CPC title

• F16F7/015

  the particles being spherical, cylindrical or the like · CPC title

• B64C13/0421

  control sticks for primary flight controls · CPC title