Methods and apparatus for a suspension system
Various embodiments of the present technology may comprise a method and apparatus for a space-saving suspension system. In various embodiments, the apparatus may comprise a fine suspension device, a coarse suspension device, and a mechanical assembly. In various embodiments, the fine suspension device is arranged at an angle greater than zero degrees from the z-axis. In various embodiments, the mechanical assembly is coupled to the fine suspension device and a payload, such that when a force is exerted on the mechanical assembly by the payload, an applied force is transmitted to the fine suspension device.
1. A suspension apparatus for use with a first element and a second element traveling along a first axis, comprising:
a fine suspension device coupled to at least one of the first element and the second element, wherein the fine suspension device operates on a fine suspension travel axis, and wherein the first axis is not parallel to the fine suspension travel axis;
a mechanical assembly coupled to the fine suspension device and to at least one of the first element and the second element, the mechanical assembly comprising:
a bearing system directly coupled to the first element; and
a lever arm coupled to the bearing system and coupled to the second element wherein the mechanical assembly transfers movement of the first element relative to the second element to the fine suspension device.
2. The suspension apparatus of claim 1 , wherein the lever arm comprises a first segment rotatably coupled to a second segment.
3. The suspension apparatus of claim 1 , wherein the fine suspension device comprises at least one of a gas shock absorber, a liquid-filled damper, and a gas and liquid-filled damper.
4. The suspension apparatus of claim 1 , further comprising a coarse suspension device coupled between the first element and the second element.
5. The suspension apparatus of claim 4 , further comprising an air reservoir coupled to the coarse suspension device.
6. The suspension apparatus of claim 4 , wherein the second element comprises a weight and wherein the coarse suspension device is configured to adapt to the weight of the second element to maintain the position of the first element relative to the second element within an established coarse position range.
7. The suspension apparatus of claim 1 , wherein the bearing system comprises:
a bearing housing comprising a bearing; and
a rotatable shaft, wherein the shaft is rotatable upon the bearing.
8. The suspension apparatus of claim 7 , wherein the lever arm is affixed to the shaft.
9. The suspension apparatus of claim 1 , further comprising a lever coupling the bearing system to the fine suspension device.
10. The suspension apparatus of claim 1 , further comprising a scissor linkage coupled between the first element and the second element.
11. A suspension apparatus adapted to be coupled to a support mount, and to a payload movable along a first axis, comprising:
a fine suspension device comprising a first and second end, wherein:
the first end is coupled to the support mount;
the fine suspension device operates on a fine suspension travel axis; and the first axis is not parallel to the fine suspension travel axis;
a mechanical assembly coupled to the second end of the fine suspension device, the mechanical assembly comprising a bearing system that is further directly coupled to the support mount, and wherein the mechanical assembly transfers an applied force from at least one of the payload and the support mount to the fine suspension device.
12. The suspension apparatus of claim 11 , further comprising a coarse suspension device comprising a first and second end, wherein the first end is coupled to the support mount and the second end is coupled to the payload.
13. The suspension apparatus of claim 12 , wherein the coarse suspension device comprises at least one of the group consisting of a pneumatic spring and a mechanical spring.
14. The suspension apparatus of claim 13 , wherein the coarse suspension device further comprises an air reservoir coupled to the pneumatic spring.
15. The suspension apparatus of claim 11 , wherein the mechanical assembly comprises a rotatable shaft coupled to a bearing system comprising a bearing attached to a bearing housing.
16. The suspension apparatus of claim 15 , wherein the mechanical assembly is coupled to the support mount via a bearing housing.
17. The suspension apparatus of claim 16 , wherein the mechanical assembly further comprises a lever arm, the lever arm comprising a first segment and a second segment, wherein the second segment is coupled to the shaft to effect a torque and the first segment is coupled to the payload.
18. The suspension apparatus of claim 17 , wherein the mechanical assembly further comprises a lever coupling the shaft to the fine suspension device.
19. The suspension apparatus of claim 11 , wherein the fine suspension device comprises at least one of: a gas shock absorber, a liquid-filled damper, and a gas and liquid-filled damper.
20. The suspension apparatus of claim 11 , wherein the fine suspension device comprises a piston.
21. The suspension apparatus of claim 11 , wherein the fine suspension device comprises a magnetorheological damper.
22. The suspension apparatus of claim 11 , wherein the support mount comprises a non-horizontal orientation.
23. A method for reducing vibration transferred from a support mount to a payload, comprising:
absorbing energy transferred along a first axis between the support mount and the payload utilizing a mechanical assembly and a fine suspension device;
wherein the mechanical assembly comprises a bearing system directly coupled to the support mount and is configured to change position according to the amount of energy transferred between the payload and the support mount; and
wherein the fine suspension device operates along a second axis and resists at least one of the forces of compression and expansion according to the change in position of the mechanical assembly; and
wherein the first and second axes are arranged at a non-zero angle relative to each other.
24. The method of claim 23 , further comprising absorbing energy transferred between the payload and the support mount with a coarse suspension device.