Piezoelectric power system
First Claim
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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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Current AssigneeCarol Kolm, Peter H. Fowler
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Original AssigneeCarol Kolm, Peter H. Fowler
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InventorsKolm, Carol, Fowler, Peter H.
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Application NumberUS04/092,701Time in Patent Office1,833 DaysField of SearchUS Class Current307/43CPC Class CodesF23M 2900/13003 Energy recovery by thermoel...F23Q 2/287 piezoelectricF23Q 3/002 using piezoelectric elementsH02N 2/186 Vibration harvestersH10N 30/304 Beam type
