Aviation proactive air and surface purification component
AssigneeAviation Clean Air, LLC
InventorsJimmy Devoy Galbreath, Mallie Jamieson Seckinger, Sr.
Life of this patent
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Abstract
The present invention provides methods and systems for an ionization device that includes a base portion, a first pair and a second pair of opposed sidewalls extending upwardly from the base portion to form an upper edge, a top portion is engaged to the upper edge, and a cavity is formed within the base portion, the two pairs of opposed sidewalls, and the top portion. A probe assembly is in electronic communication with the top portion, wherein the probe assembly comprises a probe seat selectively secured to an exterior portion of a conduit of the existing environmental control system of the aircraft and a wire extends through the probe seat for supplying electrical current to an emission portion that emits ions.
Claims20
An ionization device comprising:
- a base portion;
- at least one sidewall extending from the base portion;
- a cavity formed within the base portion and the at least one sidewall;
- an ion generator disposed within the cavity;
- and
- a probe assembly in electronic communication with the ion generator,
- wherein the probe assembly comprises a probe seat selectively secured to a conduit of an existing environmental control system of an aircraft;
- a probe sleeve extending upward from the probe seat;
- a probe retention device for retaining the probe sleeve;
- and a wire extends through the probe seat, probe retention device, and probe sleeve for supplying electrical current to an emission portion that emits ions and
- wherein the device operates on power supplied by a power supply from the aircraft.
An ionization device for use in a conduit of an aircraft, comprising:
- an ion generator, and
- a probe assembly in electrical communication with the ion generator,
- wherein the probe assembly comprises a probe seat selectively secured to the conduit of an existing environmental control system of the aircraft, a probe sleeve extends upwardly from the probe seat,
- a probe retention device for retaining the probe sleeve,
- a wire extending through the probe seat, probe retention device, and the probe sleeve,
- an emission portion of the wire is disposed on an end of the probe sleeve that emits ions into the conduit, and
- wherein the device operates on power supplied by a power supply from the aircraft.
An ionization device for use on aircraft comprising:
- an ion generator, and
- a probe assembly in electrical communication with the ion generator,
- wherein the probe assembly comprises a probe seat selectively secured to an exterior portion of a conduit of an existing environmental control system of the aircraft,
- a probe sleeve extending upward from the probe seat;
- a probe retention device for retaining the probe sleeve,
- a wire extending through the probe seat, probe retention device, and probe sleeve, and an emission portion of the wire that emits ions into the conduit, and
- wherein the device operates on power supplied by a power supply from the aircraft.
Dependencies are inferred from the claim text.