Method and device for reducing vibrations

• US 6,427,815 B1
• Filed: 07/21/1999
• Issued: 08/06/2002
• Est. Priority Date: 07/21/1998
• Status: Expired due to Term

• Current Assignee: Airbus Helicopters Deutschland Gmbh (Airbus SE)
• Original Assignee: Eurocopter Deutschland Gesellschaft Mit Beschrã¤Nkter Haftung (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Zeller, Siegfried
• Primary Examiner(s): Schwartz, Christopher P.
• Application Number:
  US09/358,343
• Time in Patent Office: 1,112 Days
• Field of Search: 188/378, 188/379, 188/380, 188/382, 267/136, 267/140.1, 318/611, 318/460
• US Class Current: 188/380
• CPC Class Codes: B64C 2027/005 using suspended masses
• CPC Class Codes: B64C 27/001 Vibration damping devices

Abstract

A device and method for reducing vibrations of a structure along an axis of vibration propagation, in particular in a helicopter, wherein two vibrating members of masses m₁ and m₂ are located at the ends of a spring, the spring and/or the masses being so constructed that the resonance characteristics of the assembly may be variably adjusted within a range decisive for the reduction of vibrations of the structure. The phases of the movement of the two masses and of a central point of the spring connected to the structure are measured by accelerometers and the differences of phase angle compared to the base point are maintained at 90° by moving the masses using motors to bring about the necessary change in resonance of the assembly.

Claims

1. A device for reducing vibrations of a. structure along a vibration propagation axis comprising an elongate spring having a central region with a connection for a structure for reducing vibration of said structure, two vibrating bodies each disposed at one of two opposite end portions of the spring, means for measuring movements of each of the vibrating bodies with respect to the central region of the spring, phase detectors for measuring phase difference between the movements of each of the vibrating bodies and the central region of the spring respectively, an amplitude controller for measuring amplitude difference between the movements of the vibrating bodies at the end portions of the spring and means for modifying resonance characteristics of an assembly of the spring and the vibrating bodies to reduce vibrations in the structure as a function (1) of a measured phase difference between the respective movements at the vibrating bodies and the movement at the central region of the spring and (2) of the amplitude difference between the movements of the vibrating bodies at the end portions of the spring.

2. A device according to claim 1, in which the two vibrating bodies at each end portion have masses m₁ and m₂ which include respective mass components Δ

m₁ and Δ

m₂ mounted so as to be displaceable along the axis of vibration propagation relative to the respective masses m₁ and m₂.

3. A device according to claim 2, further including adjusting devices to displace the mass components Δ

m₁, and Δ

m₂ independently along said axis.

4. A device according to claim 3, in which the adjusting devices comprise spindle drives and stepper motors.

5. A device according to claim 1, in which the phase detectors comprise multiplexers.

6. A device according to claim 1, in which the amplitude controller comprises a comparator in which amplitude values of said vibrating bodies are compared.

7. A device according to claim 1, in which the means for measuring movement comprises acceleration sensors.

8. A device according to claim 1, wherein said means for modifying the resonance characteristics comprises a logic component which receives output signals from the amplitude controller and from the phase detectors to provide overall correcting signals for modifying said resonance characteristics.

9. A device according to claim 1, in which said structure comprises a helicopter.

10. A device according to claim 1, wherein said structure comprises a vehicle having a cabin and a seat within the cabin, said device reducing vibration in the seat and being located within the cabin in association with the seat to reduce vibration in the seat in response to different operating conditions of the vehicle.

11. A method for reducing vibrations of a helicopter structure comprising connecting the helicopter structure to a central region of an elongate spring, measuring the movements of two vibrating members of masses m₁ and m₂ attached at ends of the spring relative to a movement of the central region of the spring and modifying resonance characteristics of a system consisting of the spring and the vibrating members by correcting variables derived from phase differences between the movements of the vibrating members and the movement at the central region of the spring respectively until a target phase difference value of 90°

therebetween is attained and also by correcting said variables in dependence on an amplitude difference between the movements of the vibrating members until a set amplitude difference value is attained.

12. A method according to claim 11, in which the correcting variables from the amplitude difference and the correcting variables from the phase differences are combined to form overall correcting variables.

13. A method according to claim 11, in which the adjustment using phase comparison is interrupted in order to perform the adjustment using amplitude difference.

14. A method according to claim 11, in which said phase differences are adjusted by moving weight bodies forming part of the vibrating members along said spring relative to masses m₁ and m₂ respectively.