Aircraft 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 disposed on the top portion, wherein the probe assembly comprises a probe seat selectively secured to an exterior portion of the top portion and a wire extends through the probe seat for supplying electrical current to an emission portion that emits ions.
Claims19
An ionization device comprising:
- 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, the top portion has an exterior portion and an interior portion;
- a cavity is formed within the base portion, the two pairs of opposed sidewalls, and the top portion;
- and
- a probe assembly disposed on the top portion, wherein the probe assembly comprises a probe seat with a top portion and a bottom portion that is selectively secured to an exterior portion of the top portion and extending to a height above the exterior portion of the top portion, a bore is disposed within the probe seat and extending from the top portion to the bottom portion of the probe seat that is overtop a corresponding bore on the exterior portion of the top portion for receiving a fastening device, and a wire extends through the probe seat for supplying electrical currently to an emission portion that emits ions.
An ionization device for use in a conduit of an aircraft, comprising:
- 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;
- a cavity is formed within the base portion, the two pairs of opposed sidewalls, and the top portion;
- and
- a probe assembly disposed on the top portion, wherein the probe assembly comprises a probe seat selectively secured to an exterior portion of the top portion and a probe sleeve extends upwardly from the probe seat, a wire extends through the probe seat and the probe sleeve for supplying electrical current to an emission portion that emits ions disposed on an end of the probe sleeve, the probe seat is generally square and having four corners, wherein a bore is positioned adjacent each corner for receiving a correspondingly threaded fastening device.
An ionization device for use on aircraft comprising:
- 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;
- a cavity is formed within the base portion, the two pairs of opposed sidewalls, and the top portion;
- an ion generator disposed within the cavity;
- and
- a probe assembly disposed on the top portion, wherein the probe assembly comprises a probe seat selectively secured to an exterior portion of the top portion and a wire extends through the probe seat for supplying electrical currently to an emission portion that emits ions, the probe seat contains two centrally located bores for receiving a corresponding fastening device.
Dependencies are inferred from the claim text.