Alternating-resilience engine mount

• US 5,280,886 A
• Filed: 04/01/1992
• Issued: 01/25/1994
• Est. Priority Date: 05/07/1991
• Status: Expired due to Fees

• Current Assignee: Firma Carl Freudenberg
• Original Assignee: Firma Carl Freudenberg
• Inventors: Gartner, Hanno, Simuttis, Arnold, Hettler, Werner
• Primary Examiner(s): Oberleitner, Robert J.
• Assistant Examiner(s): Poon, Peter M.
• Application Number:
  US07/861,737
• Time in Patent Office: 664 Days
• Field of Search: 267/140.11, 267/140.13, 267/140.14, 267/140.2, 267/219, 267/35, 248/562, 248/636, 180/300, 180/312
• US Class Current: 267/140.13
• CPC Class Codes: B60K 5/1283 Adjustable supports, e.g. the mounting or the characteristics being adjustable
• CPC Class Codes: F16F 13/26 characterised by adjusting or regulating devices responsive to exterior conditions F16F13/101 takes precedence
• CPC Class Codes: F16F 3/087 Units comprising several springs made of plastics or the like material F16F1/40, F16F1/545 take precedence

Abstract

An alternating-resilience engine mount consists of a supporting component and a supported component, both of which move back and forth across an axis. The supported component is supported by the supporting component through the intermediary of two series-connected resilient rubber components. The motion of the second resilient component can be impeded when necessary by a so-called "auxiliary device ". According to the invention, the two resilient components are interconnected and separated by a rigid tray.

Claims

1. In an alternating-resilience engine mount consisting of a supporting component and a supported component, both of which move back and forth in an axial direction, wherein the supported component is supported by the supporting component through the intermediary of two series-connected resilient rubber components, wherein auxiliary means are provided for selectively impeding the motion of the second resilient component and wherein the two resilient components are interconnected and separated by a rigid tray that is covered by a layer of rubber;

the improvement wherein the tray is cup shaped;

wherein the first and the second resilient components are in contact with the rigid tray and at least partially overlap in the axial direction of the engine mount, and wherein the rubber layer covering the tray is formed integrally with at least one of the resilient components.

2. The alternating-resilience engine mount defined in claim 1, wherein the tray has a surface that comes into contact with a counteracting surface on at least one of the supported component and the supporting component.

3. The alternating-resilience engine mount defined in claim 2, wherein the auxiliary means include fluid actuated means for selectively bringing the two surfaces into contact.

4. The alternating-resilience engine mount defined in claim 2, wherein the auxiliary means comprise a bellows that expands when fluid is injected into its interior and can be forced against at least one of the tray and the counteracting contact surface, and that collapses automatically when depressurized.

5. The alternating-resilience engine mount defined in claim 1, wherein the auxiliary means comprises at least one piston and cylinder mechanism.

6. The alternating-resilience engine mount defined in claim 5, wherein said piston and cylinder mechanism is located on at least one of the supported component and the supporting component.

7. The alternating-resilience engine mount defined in claim 5, wherein said piston and cylinder mechanism is located on the tray.

8. The alternating-resilience engine mount defined in claim 5, wherein an axis of motion of the piston and cylinder mechanism parallels an axis of the engine mount.

9. The alternating-resilience engine mount defined in claim 1, wherein the auxiliary means are integrated into the second resilient component in the form of a hollow interior that can be expanded by injecting a fluid into it under pressure.

10. The alternating-resilience engine mount defined in claim 9, wherein the second resilient component can expand parallel to an axis of the engine mount when the fluid is injected into its interior.

11. The alternating-resilience engine mount defined in claim 9, wherein the second resilient component can, while it is unexpanded, be radially separate from a contact surface on the tray and, when it is expanded, be tightly forced radially against that surface.

12. The alternating-resilience engine mount defined in claim 1, wherein the tray is made of sheet metal.

13. The alternating-resilience engine mount defined in claim 1, wherein the two resilient components at least partly overlap in an axial direction of the engine mount as they connect the supporting component to the supported component, one of said resilient components being annular in shape and the other resilient component fitting at least partially within said one resilient component.

14. The alternating-resilience engine mount defined in claim 1, wherein the two resilient components are secured to surfaces on at least one of the tray and the supporting and supported components that extend across its axis.