Multiaxis vibration isolation system
AssigneeHoneywell Inc.
InventorsDavid C. Cunningham, Lawrence P. Davis, Frank M. Schmitt
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AssigneeHoneywell Inc.
InventorsDavid C. Cunningham, Lawrence P. Davis, Frank M. Schmitt
Estimating the term…
A system for isolating a supported structure from transmitting vibrations to a supporting base in a spacecraft provides six degrees of freedom in a kinematic mounting. Six isolator elements in a symmetric arrangement of three skewed isolator pairs provides viscous damping and vibration and shock attenuation during launch and operation in space. The isolators employ two degrees of freedom flexure joints at each mounting point to assure primarily axial deflection and minimize bending moments, and have tuning springs to optimize performance. The system permits deterministic design and allows calculation of all loads from the nominal geometry and the isolator axial stiffness. Limit stops are provided between the supporting structure and the supported structure to limit excursions of the isolator members.
Vibration isolating and damping apparatus for passively isolating vibrations between a supporting structure and a supported structure having a center of mass while permitting movement of the supported structure over six degrees of freedom with respect to the supporting structure, wherein the supported structure contains a torque-producing device for developing predetermined control torques over a given vibration frequency range, comprising:
Vibration isolating and damping apparatus for passively isolating vibrations between a supporting structure and a supported structure having a center of mass while permitting movement of the supported structure over six degrees of freedom with respect to the supporting structure, wherein the supported structure contains a torque-producing device for developing predetermined control torques over a given vibration frequency range, comprising:
Vibration isolating and damping apparatus for passively isolating vibrations between a supporting structure and a supported structure while permitting movement of the supported structure over six degrees of freedom with respect to the supporting structure, comprising:
Dependencies are inferred from the claim text.