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NASA NTRS ยท 20150003436

Propellant Flow Actuated Piezoelectric Igniter for Combustion Engines

Abstract

A propellant flow actuated piezoelectric igniter device using one or more hammer balls retained by one or more magnets, or other retaining method, until sufficient fluid pressure is achieved to release and accelerate the hammer ball, such that it impacts a piezoelectric crystal to produce an ignition spark. Certain preferred embodiments provide a means for repetitively capturing and releasing the hammer ball after it impacts one or more piezoelectric crystals, thereby oscillating and producing multiple, repetitive ignition sparks. Furthermore, an embodiment is presented for which oscillation of the hammer ball and repetitive impact to the piezoelectric crystal is maintained without the need for a magnet or other retaining mechanism to achieve this oscillating impact process.

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BibTeXRIS

Wollen, Mark A.. 2015-01-13. Propellant Flow Actuated Piezoelectric Igniter for Combustion Engines. https://ntrs.nasa.gov/citations/20150003436

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