초록

An apparatus for a portable aircraft landing light system. The system has three modalities that can be controlled manually or remotely. The modalities are visible light, infrared light and FLIR emission. A ballast and battery provide constant power supply to each of the three modalities.

대표청구항 ▼

1. A portable self contained landing light apparatus comprising: a first cold cathode lamp to emit visible light; a second cold cathode lamp to emit infrared light; a heating element to emit heat; a ballast coupled to each lamp; a rechargeable battery coupled to the ballast; and a control ci

1. A portable self contained landing light apparatus comprising: a first cold cathode lamp to emit visible light; a second cold cathode lamp to emit infrared light; a heating element to emit heat; a ballast coupled to each lamp; a rechargeable battery coupled to the ballast; and a control circuit coupled to the ballast, heating element and battery to receive manual or radio frequency input to control each lamp and the heating element. 2. The portable landing light apparatus of claim 1 wherein the heating element includes a panel having predetermined dimensions capable of emitting thermal energy having a predetermined wavelength. 3. The portable landing light apparatus of claim 1 wherein the visible light emitted is at least one of white, green, red, yellow and blue. 4. The portable landing light apparatus of claim 1 further comprising a battery-charging jack coupled to the rechargeable battery. 5. The portable landing light apparatus of claim 1 further comprising a switch to provide manual input to the control circuit. 6. The portable landing light apparatus of claim 1 wherein the rechargeable battery is a 12 volt gel cell. 7. The portable landing light apparatus of claim 1 wherein the battery, ballast, each lamp and the heating element operate to provide at least 8 hours of continuous operation. 8. The portable landing light apparatus of claim 1 further comprising: a housing to house at least one of the ballast, rechargeable battery and control circuit, including a stake-mounting hub. 9. The portable landing light apparatus of claim 8 further comprising: a strap to carry the apparatus coupled to the housing. 10. The portable landing light apparatus of claim 1 wherein each cold cathode lamp provides at least 7 candela of luminescence. 11. The portable landing light apparatus of claim 9 further comprising: a BNC coupled to the control circuit. 12. The portable landing light apparatus of claim 11 further comprising an antenna coupled to the BNC connector to provide radio frequency input to the control circuit. 13. The portable landing light apparatus of claim 2 wherein the panel is 1.75 inches by 2.75 inches by 0.05 inches of aluminum. 14. The portable landing light apparatus of claim 1 wherein the control circuit is configured to receive manual input to set a frequency to receive transmission. 15. An apparatus for assisting the landing of aircraft comprising: means for providing visible light to illuminate a landing area; means for providing infrared emissions detectable by an aircraft; means for emitting heat detectable by a forward looking infrared system; means for controlling at least one of the visible light means, infrared emission means, and heat emitting means by remote command. 16. The apparatus of claim 15 further comprising: means for powering at least one of the visible light means, infrared emission means, heat emitting means and control means, wherein the powering means, visible light means, infrared emission means, heat emitting means and control means to provide at least 8 hours of continuous operation. 17. The apparatus of claim 15 further comprising: means for manually setting a receiving frequency. 18. The apparatus of claim 15 further comprising, means for manually controlling the visible light means, infrared emission means, heat emitting means and powering means.