Aircraft proactive air and surface purification component
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.
1. 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.
2. The ionization device according to claim 1 , wherein a probe sleeve extends upwardly from the probe seat and the emission portion extends from an end of the probe sleeve.
3. The ionization device according to claim 1 , further comprising an ion generator disposed within the cavity.
4. The ionization device according to claim 1 , wherein the probe seat is selectively secured to the top portion by a fastening device.
5. The ionization device according to claim 1 , wherein the top portion extends over the upper edge of the first pair of sidewalls and forming a lip having at least one bore.
6. The ionization device according to claim 1 , wherein the top portion is selectively secured to the first and second pair of opposed sidewalls allowing access to the cavity.
7. The ionization device according to claim 1 , wherein 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.
8. The ionization device according to claim 1 , wherein the probe seat contains two centrally located bores for receiving a corresponding fastening device.
9. 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.
10. The ionization device according to claim 9 , further comprising a military grade electrical connector disposed within a sidewall for receiving a power supply and providing power to the device.
11. The ionization device according to claim 9 , further comprising a circuit board positioned within the cavity.
12. The ionization device according to claim 9 , further comprising an ion generator positioned within the cavity and a circuit board positioned within the cavity for controlling the ion generator.
13. The ionization device according to claim 9 , further comprising a light emitting diode.
14. The ionization device according to claim 9 , wherein the emission portion comprises an electrode for emitting ions.
15. The ionization device according to claim 9 , wherein the emission portion comprises a brush with a plurality of conductive bristles for emitting ions.
16. 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.
17. The ionization device according to claim 16 , wherein a probe sleeve extends upwardly from the probe seat and the emission portion extends from an end of the probe sleeve.
18. The ionization device according to claim 16 , wherein the device operates at 28 VDC.
19. The ionization device according to claim 16 , wherein the top portion extends over the upper edge of the first pair of sidewalls and forming a lip having at least one bore.