Piezoelectric power system
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2. AN ELECTRICAL POWER SYSTEM FOR AN AIRCRAFT HAVING A JET ENGINE, SAID SYSTEM COMPRISING, IN COMBINATION, A PLURALITY OF PIEZOELECTRIC TRANSDUCERS MOUNTED FOR INDEPENDENT VIBRATION IN RESPONSE TO ACOUSTICAL ENERGY GENERATED BY SAID ENGINE, EACH OF SAID TRANSDUCERS BEING IN THE FORM OF A PLATE MOUNTED FOR FLEXURE ABOUT AN AXIS, SAID PLATE HAVING AN ELECTRODE ON ONE FACE THEREOF AND A PAIR OF ELECTRODES ON THE OPPOSITE FACE THEREOF ON OPPOSITE SIDES OF SAID AXIS, A SEPARATE RECTIFIER CONNECTED TO EACH OF SAID
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2 Claims
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2. AN ELECTRICAL POWER SYSTEM FOR AN AIRCRAFT HAVING A JET ENGINE, SAID SYSTEM COMPRISING, IN COMBINATION, A PLURALITY OF PIEZOELECTRIC TRANSDUCERS MOUNTED FOR INDEPENDENT VIBRATION IN RESPONSE TO ACOUSTICAL ENERGY GENERATED BY SAID ENGINE, EACH OF SAID TRANSDUCERS BEING IN THE FORM OF A PLATE MOUNTED FOR FLEXURE ABOUT AN AXIS, SAID PLATE HAVING AN ELECTRODE ON ONE FACE THEREOF AND A PAIR OF ELECTRODES ON THE OPPOSITE FACE THEREOF ON OPPOSITE SIDES OF SAID AXIS, A SEPARATE RECTIFIER CONNECTED TO EACH OF SAID
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