Vibration isolator system
View Patent ↗A vibration isolator system for attaching a payload to a supporting base is provided, the payload having a center of mass and the system consisting of at least three vibration isolating pods. Each pod has two associated, non-parallel, elastic struts. A first end of each strut is attached to the supporting base and a second end of each strut is attached to the payload at a respective mounting point, and the a projected elastic center of the system is substantially co-located with said center of mass. The vibration isolator system is operable to substantially prevent translational vibration of the supporting base from inducing angular rotation of the payload.
1. An apparatus for attaching a supported structure to a supporting base, said supported structure having a center of mass, said apparatus comprising:
at least three vibration isolating pods, each said pod comprising two associated, non-parallel, elastic struts, a first end of each said strut attached to the supporting base and a second end of each said strut attached to the supported structure at a respective mounting point, wherein each said respective mounting point is located in a common mounting plane and said common mounting plane is substantially distant from said center of mass; and
the apparatus has a projected elastic center substantially co-located with said center of mass.
2. The apparatus of claim 1 , wherein:
said center of mass is contained in a principal plane and
each elastic strut has a respective longitudinal axis having a respective point of intersection with the principal plane; and
each said respective point of intersection is equidistant from said center of mass.
3. The apparatus of claim 2 , wherein
each said respective mounting point is located in a common mounting plane parallel to the principal plane.
4. The apparatus of claim 1 , wherein
each vibration isolating pod comprises two associated co-planar, elastic struts,
each elastic strut has a respective longitudinal axis,
a respective virtual intersection point is associated with each pod, said respective virtual intersection point being a point of intersection between the respective longitudinal axes of the associated elastic struts within each pod; and
said virtual intersection points are co-planar and equidistant from the center of mass.
5. The apparatus of claim 4 , wherein said virtual intersection points are not co-located.
6. The apparatus of claim 1 , wherein the supported object is a payload.
7. The apparatus of claim 6 , wherein the payload is a gimbal assembly.
8. The apparatus of claim 1 , wherein the elastic struts are passive.
9. The apparatus of claim 1 , wherein said apparatus is operable to substantially prevent translational vibration of the supporting base from inducing angular rotation of the supported structure.
10. A system, comprising
a payload having a center of mass; and
a supporting base, said payload attached to said supporting base by apparatus comprising:
at least three vibration isolating pods, each said pod comprising two associated, non-parallel, elastic struts, a first end of each said strut attached to the support and a second end of each said strut attached to the payload at a respective mounting point, wherein:
each said respective mounting point is located in a common mounting plane and said common mounting plane is substantially distant from said center of mass; and
the apparatus has a projected elastic center substantially co-located with said center of mass.
11. The system of claim 10 , wherein:
said center of mass is contained in a principal plane and
each elastic strut has a respective longitudinal axis having a respective point of intersection with the principal plane; and
each said respective point of intersection is equidistant from said center of mass.
12. The system of claim 11 , wherein:
each said respective mounting point is located in a common mounting plane parallel to the principal plane.
13. The system of claim 10 , wherein:
each vibration isolating pod comprises a pair of associated co-planar, elastic struts,
each elastic strut has a respective longitudinal axis,
a respective virtual intersection point is associated with each pair of associated struts, said respective virtual intersection point being a point of intersection between the longitudinal axes of the associated struts; and
said virtual intersection points are co-planar and equidistant from the center of mass.
14. The system of claim 13 , wherein said virtual intersection points are not co-located.
15. The system of claim 10 , wherein said apparatus is operable to substantially prevent translational vibration of the supporting base from inducing angular rotation of the supported structure.
16. The system of claim 10 , wherein the elastic struts are passive.
17. The system of claim 10 , wherein the payload is a gimbal assembly.