Self tuning vibration absorber

Patent metadata

Field	Value
Publication number	US-9296476-B2
Application number	US-201213450060-A
Country	US
Kind code	B2
Filing date	Apr 18, 2012
Priority date	Apr 18, 2012
Publication date	Mar 29, 2016
Grant date	Mar 29, 2016

Abstract

A system and method to adjustably create a reacting force in response to a vibrating force of a vibrating structure. The system includes an adjustable vibration absorber that creates a range of reacting forces. The method includes continuously monitoring the reacting force and the vibrating force with a sensor system operably associated with a control unit having an algorithm to determine if adjustment of the vibration absorber is required. If required, the control unit commands a driver to selectively adjust the vibration absorber such that the reacting force equals the vibrating force.

First claim

What is claimed is:

1. An aircraft, comprising;
a vibrating structure creating a vibrating force; and
a vibration system, having:
an adjustable vibration absorber that creates a reacting force in response to the vibrating force;
a driver rigidly attached to the vibrating structure and operably associated with the vibration absorber;
a sensor system, having:
a first sensor associated with the vibration absorber;
a second sensor associate with the vibrating structure; and

a control unit in data communication with both the sensor system and the driver, the control unit being configured to analyze a first signal from the first sensor and a second signal from the second sensor and configured to command the driver to adjust the vibration absorber, the control unit, having:
an algorithm, having:
a linear envelope detector;
a differentiator; and
a sign comparator;

wherein the first signal and the second signal pass through the linear detector for determining a first amplitude of the first signal and a second amplitude of the second signal, then a slope of a ratio of the first amplitude and the second amplitude is determined with the differentiator and is compared with the sign comparator;

wherein the vibration system continuously analyzes the vibrating force and the reacting force for determining whether adjustment of the vibration absorber is required; and
wherein if the slope is not equal to zero, then the vibration absorber is adjusted accordingly.

2. The aircraft of claim 1 , further comprising:
a main mass cantilevered at a spaced relationship relative to the vibrating structure.

3. The aircraft of claim 2 , further comprising:
a flexible beam for cantilevering the main mass relative to the vibrating structure.

4. The aircraft of claim 3 , wherein the flexible beam is moveable relative to the vibrating structure.

5. The aircraft of claim 2 , further comprising:
an auxiliary mass cantilevered at a spaced relationship relative to the vibrating structure;
wherein the spaced relationship of the auxiliary mass relative to the vibrating structure is adjusted via the driver.

6. The aircraft of claim 5 , further comprising:
a linkage rigidly attached to the auxiliary mass and operably associated with the driver;
wherein the driver selectively adjusts the spaced relationship of the auxiliary mass relative to the vibrating structure via the linkage.

7. The aircraft of claim 1 , the control unit comprising:
an algorithm, having:
an analog multiplier; and
a dynamic detector;
wherein the first signal and the second signal are multiplied together in the analog multiplier, then passed through the dynamic detector for determining the relative phase angle between the first signal and the second signal.

8. The aircraft of claim 7 , wherein the algorithm determines whether the relative phase angle is equal to 90 degrees, and if so, then the vibration absorber is not adjusted, else, the control unit commands the driver to adjust the vibration absorber until the relative phase angle is equal to 90 degrees.

9. A vibration system for a vibrating structure, comprising:
an adjustable vibration absorber, having:
a first spring element coupled to the vibrating structure and a main absorber mass;
a second spring element spaced from and extending relatively parallel to the first spring element, the second spring element being coupled to the vibrating structure and the main absorber mass; and
a driver disposed between the first spring element and the second spring element for adjusting the spaced relationship therebetween;

a first sensor operably associated with the vibration absorber main mass;
a second sensor operably associate with the vibrating structure; and
a control unit for controlling movement of the driver and a control unit in data communication with both the sensor system and the driver, the control unit being configured to analyze a first signal from the first sensor and a second signal from the second sensor and configured to command the driver to adjust the vibration absorber, the control unit, having:
an algorithm, having:
a linear envelope detector;
a differentiator; and
a sign comparator;
wherein the first signal and the second signal pass through the linear detector for determining a first amplitude of the first signal and a second amplitude of the second signal, then a slope of a ratio of the first amplitude and the second amplitude is determined with the differentiator and is compared with the sign comparator;

wherein if the slope is not equal to zero, then the vibration absorber is adjusted accordingly;
wherein the vibration system continuously analyzes a vibrating force from the vibrating structure and a reacting force from the absorber for determining whether adjustment of the vibration absorber is required; and
wherein if adjustment of vibration absorber is required, the control unit commands the driver to adjust the spaced relationship between the first and second spring elements.

10. A method to adjustably create a reacting force in response to a vibrating force exerted on an absorber spring and mass system by a vibrating structure, the method comprising:
attaching a driver to the vibrating structure, the driver being operably associated with an adjustable absorber configured to create the reacting force;
sensing the reacting force with a first sensor and the vibrating force with a second sensor;
relaying a first signal from the first sensor and a second signal from the second sensor to a control unit;
determining whether adjustment of the absorber is required by analyzing the first signal and the second signal with a control algorithm associated with the control unit;
determining a first amplitude of the first signal and a second amplitude of the second signal;
determining a slope of a ratio of the first amplitude and the second amplitude with a differentiator;
comparing the slope with a sign comparator; and
adjusting the vibration absorber accordingly;
wherein if the slope is not equal to zero, then the vibration absorber is adjusted accordingly.

11. The method of claim 10 , wherein:
adjusting the vibration absorber is achieved by moving a cantilevered mass relative to the vibrating structure; and
suspending the mass relative to the vibrating structure via a linkage operably associated with the driver.

12. The method of claim 11 , further comprising:
telescopically extending the linkage relative to the vibrating structure.

Assignees

• Seifert Michael
• Stamps Frank Bradley
• Smith Michael R
• Heverly David E
• Textron Innovations Inc

Inventors

• Seifert Michael
• Stamps Frank Bradley
• Smith Michael R
• Heverly David E

Classifications

• F16F15/00

  Suppression of vibrations in systems ({damping of non-rotary systems using inertia effect F16F7/10; prevention or isolation of vibrations in machine tools B23Q11/0032; suppression of driveline vibrations in hybrid vehicle transmissions B60W30/20} ; vehicle seat suspension devices B60N2/50; {methods or devices for protecting against, or damping of, acoustic waves, e.g. sound G10K11/16}); Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion ({vibration absorbing or balancing means for aircraft propellers B64C11/008, for rotorcraft rotors B64C27/001} ; testing static and dynamic balance of machines or structures G01M1/00) · CPC title

• B64C27/001 Primary

  Vibration damping devices · CPC title

• F16F7/1005

  characterised by active control of the mass · CPC title

• B64C2027/004

  using actuators, e.g. active systems · CPC title