Two-dimensional vibration isolator

Patent metadata

Field	Value
Publication number	US-9897162-B2
Application number	US-201414151415-A
Country	US
Kind code	B2
Filing date	Jan 9, 2014
Priority date	Jan 9, 2014
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

An apparatus is provided for vibration damping and isolation. The apparatus includes an annular spring portion including a resilient member that is substantially equally resilient in two dimensions, an annular bellows portion including at least two pairs of diametrically opposed bellows providing damping in the two dimensions, and a rigid connection member coupling the annular spring portion and the annular bellow portion in parallel to one another.

First claim

What is claimed is:

1. A damping system, comprising:
an annular spring portion comprising a resilient member that is substantially equally resilient in two dimensions, and wherein the annular spring portion comprises a central opening;
an annular bellows portion comprising at least two pairs of diametrically opposed bellows providing damping in the two dimensions, and wherein the at least two pairs of diametrically opposed bellows are coupled through a common bellows housing, the bellows housing comprising a central opening;
a rigid connection member coupling the annular spring portion and the annular bellows portion in parallel to one another; and
a rigid vibration-transmitting member passing through the central opening of the annular spring portion and the central opening of the annular bellows portion for transmitting a vibration in the two dimensions from a component to the damping system.

2. The damping system of claim 1 , wherein the rigid vibration-transmitting member connects to a pre-cooler of a gas turbine engine.

3. The damping system of claim 1 , wherein the at least two pairs of diametrically opposed bellows are oriented orthogonally with respect to one another.

4. The damping system of claim 3 , wherein the bellows housing comprises at least two restricted flow passages, each restricted flow passage providing fluid flow between one of the at least two pairs of diametrically opposed bellows.

5. The damping system of claim 4 , wherein the restricted flow passages comprise an axial portion, a longitudinal portion, and a circumferential portion to provide a fluid connection between a respective pair of bellows in a manner so as to avoid passing through the central opening of the bellows housing.

6. The damping system of claim 1 , wherein the annular spring portion comprises a connection portion for coupling with a base portion to which a component requiring damping is coupled.

7. The damping system of claim 6 , wherein the annular bellows portion comprises a retaining member for coupling with the at least two pairs of diametrically opposed bellows.

8. The damping system of claim 7 , wherein the rigid connection member couples between the connection portion of the annular spring and the retaining portion of the annular bellows.

9. The damping system of claim 6 , wherein the annular spring portion comprises a resilient portion comprising a plurality of concentric, annular rings, spaced apart by concentric, annular void spaces, and wherein the central opening of the annular spring portion is disposed at a center of the resilient portion.

10. The damping system of claim 9 , wherein the resilient portion comprises a resilient metal or metal alloy.

11. The damping system of claim 1 , wherein the rigid connection member extends parallel to an axis that is orthogonal to the two dimensions.

12. The damping system of claim 1 , further comprising a temperature compensation device.

13. The damping system of claim 12 , wherein the temperature compensation device is coupled to the annular bellows portion.

14. The damping system of claim 1 , wherein the annular bellows comprises a liquid or a gas damping fluid sealed therewithin.

15. The damping system of claim 6 , wherein the component requiring damping is a gas turbine engine pre-cooler.

16. The damping system of claim 15 , wherein the base portion is a housing portion of a gas turbine engine to which the pre-cooler is coupled.

17. A damping system, comprising:
an annular spring portion comprising a resilient member that is substantially equally resilient in two dimensions, wherein the annular spring portion comprises a central opening, wherein the annular spring portion comprises a connection portion for coupling with a base portion to which a component requiring damping is coupled, wherein the annular spring portion comprises a resilient portion comprising a plurality of concentric, annular rings, spaced apart by concentric, annular void spaces, and wherein the central opening of the annular spring portion is disposed at a center of the resilient portion;
an annular bellows portion comprising at least two pairs of diametrically opposed bellows providing damping in the two dimensions, and wherein the at least two pairs of diametrically opposed bellows are coupled through a common bellows housing, the bellows housing comprising a central opening; and
a rigid connection member coupling the annular spring portion and the annular bellows portion in parallel to one another.

18. The damping system of claim 17 , wherein the resilient portion comprises a resilient metal or metal alloy.

19. The damping system of claim 17 , wherein the component requiring damping is a gas turbine engine pre-cooler.

20. The damping system of claim 19 , wherein the base portion is a housing portion of a gas turbine engine to which the pre-cooler is coupled.

Assignees

• Honeywell Int Inc

Inventors

• Witwer Kevin
• Barber Tim Daniel
• Dearing Stella Silvana
• Young Ken

Classifications

• F16F15/085 Primary

  Use of both rubber and metal springs · CPC title

• F05D2260/96

  Preventing, counteracting or reducing vibration or noise · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title