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US 5,291,787 AGranted
Triaxial vibrating platform, particularly for helicopter simulators
AssigneeThomson-CSF
InventorsJacques Laforest, Rene Le Guillou
Life of this patent
Estimating the term…
Abstract
A vibration testing platform includes, on one side, a fastening point connected to three actuators placed in orthogonal directions to one another by link-rods hinged at both ends thereof and, on the other side, three fastening points, each point being connected to the ground by a link-rod hinged at both ends thereof. The two end link-rods are vertically oriented and the third one is horizontally oriented and placed in a transversal direction.
Claims3
A triaxial vibration testing platform, with a general shape that is substantially rectangular, comprising:
- a plurality of suspension devices;
- four points for the fastening of said suspension devices, the first fastening point being located substantially in the middle of a first side of the platform, the second, third and fourth fastening points being distributed along a second, opposite side of the platform, the second fastening point being located substantially in the middle of the second side and the third and fourth fastening points being located near the ends of said second side, the first fastening point being connected to first, second and third suspension devices of said plurality of suspension devices wherein said first, second and third suspension devices are directed along three orthogonal axes, respectively, the second, third and fourth fastening points each being respectively connected to fourth, fifth and sixth suspension devices of said plurality of suspension devices, said fifth and sixth suspension devices for said third and fourth fastening points being positioned in a vertical direction, and the fourth suspension device for the second point being positioned in a horizontal direction, wherein at least the first, second and third suspension devices of the first fastening point comprise actuators having piston rods which are extended by first link-rods hinged at both ends thereof, and wherein the fourth, fifth and sixth suspension devices comprise second link-rods hinged at both ends thereof.
Dependencies are inferred from the claim text.