摘要: Modular control patches including assemblies of sensors and actuators are provided to impart or vibration foundation members such as struts in aerospace apparatus. Local analog electronic means is associated with each patch assembly. Patches attached mechanically by chemical bonding the outside struts. The corresponding electronics can be selectively removed replaced. being may also embedded a composite structure.
lens.org 参考文章(27)
Michael P. Goldenberg, Mass-loaded cantilever vibrator ,(1992)
Charles J. Swigert, System for wide bandwidth damping ,(1985)
Brian W. Brennan, System for monitoring and controlling physical movement ,(1989)
Lloyd R. Baggs, Piezoelectric saddle for musical instruments and method of making same ,(1979)
Warren P Mason, Vibration damping circuit ,(1943)
Raymond Hoole, Anthony Best, Bethell, Vehicle engine suspension systems ,(1988)
Gregory A. Needham, Louis R. Fontana, David M. Swain, Two-axis beam steering apparatus ,(1988)
Masato Komazawa, Yukihisa Takeuchi, Koji Kimura, Piezoelectric/electrostrictive actuator having at least one piezoelectric/electrostrictive film ,(1991)
Richard J. Silcox, Chris R. Fuller, Gary P. Gibbs, Method and apparatus for minimizing multiple degree of freedom vibration transmission between two regions of a structure ,(1991)
William S. Griffin, Robert L. Forward, Wideband electromagnetic damping of vibrating structures ,(1987)