Abstract: An electrical power distribution system for a vehicle may comprise two or more independently grounded buses. An evaluation system may selectively connectable to either of the buses. The evaluation system may comprise a primary side; and a secondary side isolated from the primary side. The primary side may be connected to transmit evaluation data to the secondary side. The primary side may be grounded at a primary grounding level. The primary side may be connectable to either of the buses so that, when connected, the grounding level of the primary side is equalized with a grounding level of the connected bus.

Abstract: A system and method for determining when a LED-based position light is nearing its end of life by providing to maintenance personnel visible indication that end of life is approaching. An example system includes a controller, a main LED light, an indicator LED light, a first elapsed time counter, a second elapsed time counter, and an oscillator. The first elapsed time counter recognizes when a first time threshold is exceeded, causing the indicator LED light to flash and triggering the second elapsed time counter to start counting. The second elapsed time counter recognizes when a second time threshold is exceeded, disabling both the indicator LED light and the main LED lights, thereby notifying maintenance personnel that the main LED lights have reached their end of life.

Abstract: An electrical power distribution system for a vehicle may comprise two or more independently grounded buses. An evaluation system may selectively connectable to either of the buses. The evaluation system may comprise a primary side; and a secondary side isolated from the primary side. The primary side may be connected to transmit evaluation data to the secondary side. The primary side may be grounded at a primary grounding level. The primary side may be connectable to either of the buses so that, when connected, the grounding level of the primary side is equalized with a grounding level of the connected bus.

Abstract: A secure light emitting diodes (LEDs) power system controls power to a plurality of LEDs residing in a secure LED fixture coupled to a secure LED fixture mounting. An exemplary embodiment provides power to the plurality of LEDs and senses the power provided to the LEDs. In response to sensing the power, an authorization signal is communicated from a security sensor residing in the secure LED fixture. Power to the plurality of LEDs is maintained only in response to the communicated authorization signal.

Abstract: A system and method for determining when a LED-based position light is nearing its end of life by providing to maintenance personnel visible indication that end of life is approaching. An example system includes a controller, a main LED light, an indicator LED light, a first elapsed time counter, a second elapsed time counter, and an oscillator. The first elapsed time counter recognizes when a first time threshold is exceeded, causing the indicator LED light to flash and triggering the second elapsed time counter to start counting. The second elapsed time counter recognizes when a second time threshold is exceeded, disabling both the indicator LED light and the main LED lights, thereby notifying maintenance personnel that the main LED lights have reached their end of life.

Abstract: A secure light emitting diodes (LEDs) power system controls power to a plurality of LEDs residing in a secure LED fixture coupled to a secure LED fixture mounting. An exemplary embodiment provides power to the plurality of LEDs and senses the power provided to the LEDs. In response to sensing the power, an authorization signal is communicated from a security sensor residing in the secure LED fixture. Power to the plurality of LEDs is maintained only in response to the communicated authorization signal.

Abstract: A solid state microprocessor or digital signal processor (DSP) for dual mode illumination and dimming into modern aerospace searchlights. The system is a universal dimming platform with “smart functions” that include and are not limited to multiple light intensity linearization curves, analog and/or digital input dimming interface, built-in tests and health monitoring, synchronized dual mode light output with canopy position, light driver redundancy, lamp life reporting, and controlled switching with improved EMI. With real-time monitoring of the system parameters it monitors the lights proper operation and failures which can be a concern for flight-critical lighting.

Abstract: A lighthead for a dual-mode searchlight including a generally concave housing with an attached infrared (IR) light source assembly, an insulating barrier and air gap between the visible and IR portions of the assembly, and a reflector integral to the housing.

Abstract: A solid state microprocessor or digital signal processor (DSP) for dual mode illumination and dimming into modern aerospace searchlights. The system is a universal dimming platform with “smart functions” that include and are not limited to multiple light intensity linearization curves, analog and/or digital input dimming interface, built-in tests and health monitoring, synchronized dual mode light output with canopy position, light driver redundancy, lamp life reporting, and controlled switching with improved EMI. With real-time monitoring of the system parameters it monitors the lights proper operation and failures which can be a concern for flight-critical lighting.

Abstract: A system (10) and method for monitoring the operational life and/or performance of one or more light-emitting diodes (LEDs) (20) based on sensed parameters are disclosed. The remaining life of each LED may be predicted by counting the clock cycles during which the LED-based light is activated. LED current and/or temperature measurements may be used to control the clock signal and, thus, to compensate the predicted life value. Furthermore, operational characteristics of the LED-based light may be monitored based on LED current and/or voltage measurements. Such characteristics may include performance (e.g., intensity) and failure conditions (e.g., open or short circuits).

Abstract: An electronically controlled retractable landing light (100) for use with aircraft. A controller (106) compares the commanded position of a lighthead (108) by means of a contactless absolute position sensor (212). Operation of a brake (111), motor (110), and lamp (112) is controlled by a control unit (210). Electrical power to the brake (111), motor (110), and lamp (112) is slowly applied and removed to reduce electromagnetic emissions and extend the service life of a power stage (208), brake (111), motor (110), and lamp (112). The lighthead (108) may be manually stowed in the event of a fault.

Abstract: A solid state control switching and control system (200) for retractable landing lights. A control unit (208) uses an absolute position sensor (214) to monitor the position of the lighthead (210) of the retractable landing light, and actuates a motor (216), brake (217), and lamp (212) in response to command signals (220,221,223) from the flight crew. Actuation of the motor (216), brake (217), and lamp (212) with solid state switches (100) is gradual and synchronized to minimize electromagnetic interference and extend component life.

Abstract: A solid state control switching and control system (200) for retractable landing lights. A control unit (208) uses an absolute position sensor (214) to monitor the position of the lighthead (210) of the retractable landing light, and actuates a motor (216), brake (217), and lamp (212) in response to command signals (220, 221, 223) from the flight crew. Actuation of the motor (216), brake (217), and lamp (212) with solid state switches (100) is gradual and synchronized to minimize electromagnetic interference and extend component life.

Abstract: An electronically controlled retractable landing light (100) for use with aircraft. A controller (106) compares the commanded position of a lighthead (108) by means of a contactless absolute position sensor (212). Operation of a brake (111), motor (110), and lamp (112) is controlled by a control unit (210). Electrical power to the brake (111), motor (110), and lamp (112) is slowly applied and removed to reduce electromagnetic emissions and extend the service life of a power stage (208), brake (111), motor (110), and lamp (112). The lighthead (108) may be manually stowed in the event of a fault.

Abstract: A multi-mode visible and infrared lighthead (100) for use as a landing light or searchlight. The multi-mode lighthead incorporates a modular design wherein at least one visible light source (200) and at least one infrared diode (302) are mounted into the rear sector (128) of a housing (102). Visible or infrared light is emitted out of the front sector (122) of the housing (102). Lenses (308) are installed onto the front sector (122) of the housing (102) and sealed to protect the interior of the lighthead (100) from the elements. Alternatively, and in combination, an imaging module (1), and infrared laser (400) and/or a fixed-position searchlight with rangefinder and positioning capability is provided in the multi-mode lighthead(100).

Abstract: The method for controlling a motor driving a load holds the speed of the output shaft of the motor substantially constant as the torque imposed upon the shaft by the load varies, then regulates the rate of change of the output torque delivered by the motor's output shaft based on the sensed value of output torque as the motor's speed decreases.

Abstract: The method for controlling a motor driving a load holds the speed of the output shaft of the motor substantially constant as the torque imposed upon the shaft by the load varies, then regulates the rate of change of the output torque delivered by the motor's output shaft as the motor's speed decreases.

Abstract: A system and method for canceling the effects of oscillation in an electromechanical engraving system which has a tendency to ring or vibrate, producing ghost images displaced from a main image, uses a pulse application technique. The variables affecting vibration may be continuously monitored, or set to predetermined pulse values, and the vibration is then predicted based on these variables. Pulses are then applied in a sequence to eliminate different harmonics of each vibration.

Abstract: A liquid fogging apparatus has a motor which operates from the 12 volt power supply of a vehicle and delivers high torque at high speed, operating aproximately at 0.2 horsepower at 28,000 RPM. A rotating ring of porous ceramic material atomizes the liquid. The motor is small, 1.6" in diameter with a 5/8" diameter rotor. The stator has four phases each preferably containing eight three-turn windings of four strand wire, wound in slots in the outer surface of a short laminated stack, which is reinforced in epoxy with its inner surface honed to minimum thickness to reduce flux leakage. Eight bipolar permanent magnets are set in axial slots of a rotor stack with like poles facing tangentially toward each other around the rotor shaft. A controller commutates the motor sensing back-EMF on the windings to control speed and detect motion during start-up.