Aircraft piston engine magneto and ignition system
OwnerPaul FREDRICKSON, Sean P. KEENAN +2inventors
InventorsPaul FREDRICKSON, Sean P. KEENAN, James P. MULLENS, Thomas L. JUSTICE
Life of this patent
Estimating the term…
Loading patent…
OwnerPaul FREDRICKSON, Sean P. KEENAN +2inventors
InventorsPaul FREDRICKSON, Sean P. KEENAN, James P. MULLENS, Thomas L. JUSTICE
Estimating the term…
An aircraft piston engine magneto having a magnetic rotor and an ignition circuit with a reconfigurable charging coil inductively coupled to magnetic rotor. The charging coil includes multiple coils inductively powered by the magnetic rotor and electronically reconfigurable from a higher turn, lower amperage power coil for use when running at low speeds into a lower turn, higher amperage coil at higher speeds. The charging coil is configured into the higher turn coil by electronically connecting the multiple coils in series, and into the lower turn power coil by electronically connecting the coils in parallel. The ignition circuit is a fully electronic ignition circuit that generates and distributes ignition pulses to the piston engine spark plugs using only non-mechanically actuated electrical components within the magneto.
An aircraft piston engine magneto having a magnetic rotor and an ignition circuit that includes a charging coil inductively coupled to magnetic poles of the rotor, wherein the charging coil comprises a plurality of power coils that are electronically reconfigurable by the ignition circuit between series and parallel connections of the power coils.
An aircraft piston engine magneto having a magnetic rotor and an ignition circuit that includes a reconfigurable charging coil inductively coupled to magnetic poles of the rotor, wherein the reconfigurable charging coil comprises multiple coils that are inductively powered off the magnetic rotor and that are electronically reconfigurable from a higher turn, lower amperage power coil for use when running at low speeds into a lower turn, higher amperage power coil for use when running at higher speeds.
A magneto comprising:
A piston engine ignition system mechanically powered from a single magnetic rotor and having a plurality of high voltage output terminals adapted for connection to ignition leads so as to supply ignition energy to one or more spark plugs via the ignition leads, the ignition system comprising a fully electronic ignition circuit that operates from electrical power supplied only via induction from the magnetic rotor, wherein the ignition circuit generates the ignition energy from the received electrical power and selectively distributes the ignition energy as high voltage ignition pulses to the output terminals, and wherein the ignition circuit comprises a position sensor that detects the rotational angle of the magnetic rotor and further comprises control logic that, based on rotational angle data from the position sensor, controls timing of the ignition pulses relative to the magnetic rotor's rotational angle as a function of rotor speed.
A magneto comprising a permanent magnet rotor, a ferromagnetic core positioned relative to the rotor to concentrate and guide changing magnetic field lines that extend between opposite magnetic poles of the rotor as the rotor spins, and an ignition circuit that inductively extracts power from the changing magnetic field lines, wherein the ignition circuit includes:
A magneto comprising a permanent magnet rotor, a ferromagnetic core positioned relative to the rotor to concentrate and guide changing magnetic field lines that extend between opposite magnetic poles of the rotor as the rotor spins, and an ignition circuit that inductively extracts power from the changing magnetic field lines, wherein the ignition circuit includes:
Dependencies are inferred from the claim text.