Cantilever assemblies and methods of providing damping for cantilever assemblies

Patent metadata

Field	Value
Publication number	US-11353085-B2
Application number	US-201916459209-A
Country	US
Kind code	B2
Filing date	Jul 1, 2019
Priority date	Jul 1, 2019
Publication date	Jun 7, 2022
Grant date	Jun 7, 2022

Abstract

An example cantilever assembly includes a cantilever including an anchor configured to be coupled to a support, a tip, and an arm positioned between the anchor and the tip, a hollow conductive tube positioned at the tip of the cantilever, and a magnet suspended inside the hollow conductive tube with a first spring and a second spring. The first spring and the second spring are positioned at a first end and a second end of the hollow conductive tube respectively, and the magnet is positioned between the first spring and the second spring. The magnet is configured to move coaxially inside the hollow conductive tube as permitted by the first spring and the second spring, and the magnet suspended inside the hollow conductive tube operates as a tuned mass damper (TMD) to limit a resonant response of the cantilever assembly.

First claim

What is claimed is:

1. A cantilever assembly comprising:
a cantilever including an anchor configured to be coupled to a support, a tip, and an arm positioned between the anchor and the tip;
a hollow conductive tube positioned at the tip of the cantilever; and
a magnet suspended inside the hollow conductive tube with a first spring and a second spring, wherein the first spring and the second spring are positioned at a first end and a second end of the hollow conductive tube respectively, and the magnet is positioned between the first spring and the second spring, and wherein the magnet is configured to move coaxially inside the hollow conductive tube as permitted by the first spring and the second spring, wherein the magnet suspended inside the hollow conductive tube operates as a tuned mass damper (TMD) to limit a resonant response of the cantilever assembly,
wherein the tip of the cantilever comprises:
a first structural support extending partially around a first side of the hollow conductive tube; and
a second structural support extending partially around a second side of the hollow conductive tube.

2. The cantilever assembly of claim 1 , wherein the first structural support and the second structural support extend partially around portions of the hollow conductive tube such that a surface of the hollow conductive tube is exposed.

3. The cantilever assembly of claim 1 , wherein the tip of the cantilever comprises:
an opening into which the hollow conductive tube is positioned.

4. The cantilever assembly of claim 1 , wherein the arm of the cantilever has a thickness that tapers from the tip to the anchor.

5. The cantilever assembly of claim 1 , wherein the arm of the cantilever has a width that tapers from the anchor to the tip.

6. The cantilever assembly of claim 1 , wherein the arm of the cantilever comprises:
a first piezoelectric element positioned on a first side of the arm; and
a second piezoelectric element positioned on a second side of the arm, wherein the second side of the arm is opposite the first side of the arm.

7. The cantilever assembly of claim 6 , wherein the first piezoelectric element and the second piezoelectric element are operable as an acoustic sensor.

8. The cantilever assembly of claim 6 , wherein the first piezoelectric element and the second piezoelectric element are positioned on a top portion of the arm and on the first side and second side of the arm, respectively, wherein the second piezoelectric element is positioned to be offset from the first piezoelectric element such that the second piezoelectric element is positioned to be closer to the anchor than the first piezoelectric element.

9. The cantilever assembly of claim 1 , wherein a changing magnetic field produced by motion of the magnet relative to the hollow conductive tube generates eddy currents in the hollow conductive tube that produce an electromagnetic force opposing movement of the magnet.

10. The cantilever assembly of claim 9 , wherein the magnet acts as a mass of the TMD so that the electromagnetic force opposing movement of the magnet is a damping force.

11. The cantilever assembly of claim 9 , wherein a magnitude of the electromagnetic force is based on a magnetic field strength, magnet velocity relative to the hollow conductive tube, geometry of the hollow conductive tube, and conductivity of the hollow conductive tube, all of which remain substantially constant across operating temperatures.

12. The cantilever assembly of claim 1 , further comprising:
a first spacer positioned between the first spring and the magnet; and
a second spacer positioned between the second spring and the magnet,
wherein the magnet is coupled to the first spring via the first spacer and to the second spring via the second spacer.

13. A vector sensor assembly comprising:
a housing;
a printed circuit board in the housing; and
a plurality of cantilever assemblies positioned in the housing and coupled to the printed circuit board, wherein each of the plurality of cantilever assemblies comprises:
a cantilever including an anchor configured to be coupled to a support, a tip, and an arm positioned between the anchor and the tip;
a hollow conductive tube positioned at the tip of the cantilever; and
a magnet suspended inside the hollow conductive tube with a first spring and a second spring, wherein the first spring and the second spring are positioned at a first end and a second end of the hollow conductive tube respectively, and the magnet is positioned between the first spring and the second spring, and wherein the magnet is configured to move coaxially inside the hollow conductive tube as permitted by the first spring and the second spring, wherein the magnet suspended inside the hollow conductive tube operates as a tuned mass damper (TMD) to limit a resonant response of the cantilever assembly,
wherein the tip of the cantilever comprises:
a first structural support extending partially around a first side of the hollow conductive tube; and
a second structural support extending partially around a second side of the hollow conductive tube.

14. The vector sensor assembly of claim 13 , wherein the plurality of cantilever assemblies are arranged vertically in the housing and oriented orthogonal to each other to provide directional acoustic sensing functionality.

15. The vector sensor assembly of claim 13 , wherein the arm of the plurality of cantilever assemblies comprises:
a first piezoelectric element positioned on a first side of the arm; and
a second piezoelectric element positioned on a second side of the arm, wherein the second side of the arm is opposite the first side of the arm,
wherein the first piezoelectric element and the second piezoelectric element are operable as an acoustic sensor.

16. The vector sensor assembly of claim 15 , wherein the first piezoelectric element and the second piezoelectric element are positioned on a top portion of the arm and on the first side and second side of the arm, respectively, wherein the second piezoelectric element is positioned to be offset from the first piezoelectric element such that the second piezoelectric element is positioned to be closer to the anchor than the first piezoelectric element.

17. A method of providing damping for a cantilever assembly, the method comprising:
positioning a hollow conductive tube at a tip of a cantilever, wherein the cantilever includes an anchor configured to be coupled to a support, the tip, and an arm positioned between the anchor and the tip, wherein the tip of the cantilever comprises a first structural support extending partially around a first side of the hollow conductive tube and a second structural support extending partially around a second side of the hollow conductive tube;
suspending a magnet inside the hollow conductive tube with a first spring and a second spring;
positioning the first spring and the second spring at a first end and a second end of the hollow conductive tube respectively, wherein the magnet is positioned between the first spring and the second spring, and wherein the magnet is configured to move coaxially inside the hollow conductive tube as permitted by the first spring and the second spring; and
operating the magnet suspended inside the hollow conductive tube as a tuned mass damper (TMD) to limit a resonant response of the cantilever assembly.

18. The method of claim 17 , further comprising:
generating eddy currents in the hollow conductive tube based on a magnetic field produced by the magnet in proximity to the hollow conductive tube,

Assignees

• Boeing Co

Inventors

• Mosten Randall L
• Montague Brian
• Klein Michael

Classifications

• F16F7/104

  the inertia member being resiliently mounted {(F16F7/1022 takes precedence)} · CPC title

• F16F15/022

  using dampers and springs in combination · CPC title

• F16F15/035 Primary

  by use of eddy or induced-current damping (dynamo-electric brakes of the eddy-current type H02K49/04) · CPC title

• F16F2224/0283

  piezoelectric; electro- or magnetostrictive · CPC title

• F16F2230/08

  Sensor arrangement · CPC title