Vibration isolating device for an elastic coupling of two components

Patent metadata

Field	Value
Publication number	US-10113609-B2
Application number	US-201615175469-A
Country	US
Kind code	B2
Filing date	Jun 7, 2016
Priority date	Jun 29, 2015
Publication date	Oct 30, 2018
Grant date	Oct 30, 2018

Abstract

A vibration isolating device that is adapted for an elastic coupling of a first component to a second component and for vibration isolation in predetermined frequency ranges between the first and second components, the vibration isolating device comprising at least a first and a second elastically deformable plate that are attached to each other in at least two separate connecting points, the first elastically deformable plate comprising a first curvature and the second elastically deformable plate comprising a second curvature, wherein the first and second curvatures are respectively located in a region between the at least two separate connecting points and arranged such that a gap is defined between the first and second elastically deformable plates.

First claim

What is claimed is:

1. A vibration isolating device that is adapted for an elastic coupling of a first component to a second component and for vibration isolation in predetermined frequency ranges between the first and second components, the vibration isolating device comprising at least a first and a second elastically deformable plate that are attached to each other in at least two separate connecting points, the first elastically deformable plate comprising a first curvature located in a region between the at least two separate connecting points and the second elastically deformable plate comprising a second curvature located in a region between the at least two separate connecting points, wherein the first and second curvatures are arranged such that a gap is defined between the first and second elastically deformable plates in the regions between the at least two separate connecting points, and wherein the first and second curvatures are adapted to be reduced in operation if a tension force that moves the at least two separate connecting points away from each other is applied to the vibration isolating device, and wherein the first and second curvatures are adapted to be increased in operation if a compression force that moves the at least two separate connecting points towards each other is applied to the vibration isolating device; wherein at least one of the first and second elastically deformable plates comprises an associated vibration isolation mass and in that the at least one of the first and second elastically deformable plates comprises an associated lever that is mounted to the at least one of the first and second elastically deformable plates, in the region of at least one of the first and second curvatures, of the at least one of the first and second elastically deformable plates, at least one associated lever being provided with a vibration isolation mass.

2. The vibration isolating device according to claim 1 , wherein at least one of the first and second elastically deformable plates comprises at least one of composite material and metal.

3. The vibration isolating device according to claim 2 , wherein the composite material comprises a carbon fiber-reinforced polymer.

4. The vibration isolating device according to claim 1 , wherein the associated vibration isolation mass is arranged in the region of at least one of the first and second curvatures, of the at least one of the first and second elastically deformable plates.

5. The vibration isolating device according to claim 1 , wherein the associated vibration isolation mass is arranged in a region of the at least one of the first and second elastically deformable plates that exhibits a maximum ratio between a bulging distance and a length decrease of the vibration isolating device that occurs in operation in response to an increase of the first and second curvatures during application of a compression force.

6. The vibration isolating device according to claim 1 , wherein the associated vibration isolation mass is arranged on the associated lever in a region that exhibits a maximum ratio between a lever opening distance and a length decrease of the vibration isolating device that occurs in operation in response to an increase of the first and second curvatures during application of a compression force.

7. The vibration isolating device according to claim 6 , wherein the first elastically deformable plate comprises at least one first associated lever and the second elastically deformable plate comprises at least one second associated lever.

8. The vibration isolating device according to claim 7 , wherein the first and second associated levers are interconnected by means of at least one spring element.

9. The vibration isolating device according to claim 8 , wherein the spring element is one of a helical spring, an elastically deformable connecting plate, a diagonally arranged flat spring, a Belleville spring, a disk spring and a coned-disk spring with a connecting rod.

10. The vibration isolating device according to claim 8 , wherein the at least one spring element is arranged in a region of the first and second associated levers that exhibits a maximum ratio between a lever opening distance and a length decrease of the vibration isolating device that occurs in operation in response to an increase of the first and second curvatures during application of a compression force.

11. The vibration isolating device according to claim 1 , wherein the first and second elastically deformable plates are interconnected by means of at least one spring element.

12. The vibration isolating device according to claim 11 , wherein the spring element is one of a helical spring, an elastically deformable connecting plate, a diagonally arranged flat spring, a Belleville spring, a disk spring and a coned-disk spring with a connecting rod.

13. The vibration isolating device according to claim 11 , wherein the at least one spring element is arranged in a region of the at least one of the first and second elastically deformable plates that exhibits a maximum ratio between a bulging distance and a length decrease of the vibration isolating device that occurs in operation in response to an increase of the first and second curvatures during application of a compression force.

14. The vibration isolating device according to claim 1 , wherein the first component is a main gearbox of a helicopter and the second component is a fuselage of the helicopter.

15. The vibration isolating device according to claim 1 , wherein at least one elastically deformable plate comprises a weight adjusting arrangement having an adjustable vibration isolation mass and a drive unit that is mounted on the elastically deformable plate for achieving a weight adjustment by a translational movement a center of gravity of the adjustable vibration isolation mass; the translational movement being imposed on the adjustable vibration isolation mass by means of the corresponding drive unit in the form of a linear drive.

16. The vibration isolating device according to claim 1 , wherein at least one elastically deformable plate comprises a weight adjusting arrangement having an adjustable vibration isolation mass and a drive unit that is mounted on the elastically deformable plate for achieving a weight adjustment by a rotational movement a center of gravity of the adjustable vibration isolation mass; the rotational movement being imposed on the adjustable vibration isolation mass by means of the corresponding drive unit in the form of a rotational drive.

17. A helicopter with a first component that is elastically coupled to a second component by the vibration isolating device according to claim 1 .

Assignees

• Airbus Helicopters Deutschland GmbH

Inventors

• Buesing Moritz

Classifications

• F16F2224/0208

  Alloys · CPC title

• F16F2224/0241

  Fibre-reinforced plastics [FRP] · CPC title

• B64C2027/002

  mounted between the rotor drive and the fuselage · CPC title

• F16F15/04 Primary

  using elastic means (single elements or their attachment F16F1/00 - F16F13/00); {(F16F15/023, F16F15/03 take precedence)} · CPC title

• F16F2228/066

  Variable stiffness · CPC title