Translational tuned mass damper with continuously adjustable damping characteristics for application to high speed wind tunnel testing

Patent metadata

Field	Value
Publication number	US-9541149-B2
Application number	US-201414477701-A
Country	US
Kind code	B2
Filing date	Sep 4, 2014
Priority date	Sep 4, 2014
Publication date	Jan 10, 2017
Grant date	Jan 10, 2017

Abstract

A system, including methods and apparatus, of tuning a mass-damping apparatus to reduce dynamics forces on a wind tunnel model during wind tunnel testing. The mass-damping apparatus is coupled to a wind tunnel model and may comprise first and second pressure chambers containing a gas, a mass configured to move back and forth between the pressure chambers in a substantially airtight manner and thereby to alter gas pressure within each pressure chamber, at least one spring configured to exert a position-dependent force upon the mass, and a passageway configured to allow the gas to pass between the chambers.

First claim

What is claimed is:

1. A wind tunnel testing system configured to reduce vibrations of a wind tunnel model due to coupling of the wind tunnel model with a support structure, the system-comprising:
the wind tunnel model;
a mass-damping apparatus coupled to the wind tunnel model, the mass-damping apparatus including:
first and second pressure chambers containing a gas;
a mass configured to move back and forth between the pressure chambers in a substantially airtight manner and thereby to alter gas pressure within each pressure chamber;
at least one spring configured to exert a position-dependent force upon the mass; and
a passageway configured to allow the gas to pass between the chambers; and

the support structure connected to the wind tunnel model and configured to support the wind tunnel model within a wind tunnel during wind tunnel testing;
wherein the spring is characterized by a spring constant chosen based on a natural frequency of the support structure, thereby to reduce vibrations of the wind tunnel model that arise from the coupling of the wind tunnel model with the support structure and to allow measurement of vibrations associated with the actual aerodynamic performance of the wind tunnel model.

2. The system of claim 1 , further comprising a valve configured to control a rate of gas flow through the passageway.

3. The system of claim 2 , wherein the valve includes a plurality of apertures configured to be incrementally opened as the valve is adjusted, thereby regulating gas flow through the passageway.

4. The system of claim 1 , wherein the gas is atmospheric air.

5. The system of claim 1 , wherein the at least one spring includes a first spring configured to exert a force upon a first side of the mass, and a second spring configured to exert a force on a second side of the mass substantially opposite the first side.

6. The system of claim 1 , wherein the mass has a weight in a range of 0.5 to 10 percent of a weight of the wind tunnel model.

7. The system of claim 1 , further comprising a housing that defines the first and second pressure chambers, a cylindrical central portion between the first and second pressure chambers for receiving the mass, and a mounting base configured to couple the housing to the wind tunnel model.

8. A method of reducing dynamic forces on a wind tunnel model during wind tunnel testing, comprising:
selecting a mass with weight equal to a predetermined percentage of weight of the wind tunnel model;
selecting at least one spring with a spring constant chosen (a) based on a natural frequency of a support structure for the wind tunnel model, in order to reduce vibrations of the wind tunnel model that arise from the coupling of the wind tunnel model with the support structure and (b) in order to preserve vibrations associated with the aerodynamic performance of the wind tunnel model;
attaching to the wind tunnel model a mass-damping apparatus that includes:
first and second pressure chambers containing air;
the selected mass configured to move hack and forth between the pressure chambers in a substantially airtight manner and thereby to alter air pressure within each pressure chamber;
the at least one selected spring configured to exert a position-dependent force upon the mass; and
a passageway configured to allow the air to pass between the chambers; and

performing wind tunnel testing upon the wind tunnel model.

9. The method of claim 8 , wherein the mass-damping apparatus further includes a valve configured to regulate air flow through the passageway, and further comprising adjusting air flow through the passageway using the valve.

10. The method of claim 9 , wherein the valve includes a plurality of apertures configured to be incrementally opened as the valve is adjusted, thereby regulating air flow through the passageway.

11. The method of claim 8 , wherein the mass is selected to have a weight in a range of 0.5 to 10 percent of the weight of the wind tunnel model.

12. The method of claim 8 , wherein the mass-damping apparatus includes a housing that defines the first and second pressure chambers, a cylindrical central portion between the first and second pressure chambers for receiving the mass, and a mounting base configured to couple the housing to the wind tunnel model.

13. The method of claim 8 , wherein selecting at least one spring includes selecting at least two springs which collectively have an effective spring constant chosen to reduce motions of the wind tunnel model at the natural frequency of the support structure.

14. A method of tuning a mass-damping apparatus to reduce dynamic forces on a wind tunnel model during wind tunnel testing, comprising:
selecting a mass with weight equal to a predetermined percentage of weight of the wind tunnel model;
selecting at least one spring with a spring constant chosen to reduce vibrations of the wind tunnel model at a natural frequency of a support structure for the wind tunnel model;
installing the mass and the at least one spring in a mass-damping apparatus that allows the mass to move back and forth between first and second gas-filled pressure chambers in a substantially airtight manner while the spring exerts a position-dependent force upon the mass and while gas passes between the chambers through a passageway connecting the chambers; and
adjusting gas flow through the passageway to attain a desired degree of damping of the vibrations of the wind tunnel model that arise from the coupling of the wind tunnel model with the support structure while leaving unclamped the aerodynamic vibrations of the wind tunnel model.

15. The method of claim 14 , further comprising attaching the mass-damping apparatus to the wind tunnel model.

16. The method of claim 14 , wherein the gas is atmospheric air.

17. The method of claim 14 , wherein adjusting gas flow is performed with a valve that includes a plurality of apertures configured to be incrementally opened as the valve is adjusted, thereby regulating gas flow through the passageway.

18. The method of claim 14 , wherein the mass is selected to have a weight in a range of 0.5 to 10 percent of the weight of the wind tunnel model.

19. The method of claim 14 , wherein the mass-damping apparatus includes a housing that defines the first and second pressure chambers, a cylindrical central portion between the first and second pressure chambers for receiving the mass, and a mounting base configured to couple the housing to the wind tunnel model.

20. The method of claim 14 , wherein selecting at least one spring includes selecting at least two springs which collectively have an effective spring constant chosen to reduce motions of the wind tunnel model at the natural frequency of the support structure.

Assignees

• Boeing Co

Inventors

• Mcgranahan Bryan David
• Rueger Mathew Lee

Classifications

• G01M9/04

  Details · CPC title

• F16F7/116 Primary

  on metal springs · CPC title

• F16F7/112

  on fluid springs · CPC title

• F16F15/022

  using dampers and springs in combination · CPC title

• F16F7/104 Primary

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