Translational tuned mass damper with continuously adjustable damping characteristics for application to high speed wind tunnel testing
AssigneeThe Boeing Company
InventorsBryan David McGranahan, Mathew Lee Rueger
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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.
Claims20
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.
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.
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.
Dependencies are inferred from the claim text.