Systems and methods for detecting ice particle accumulation is disclosed herein. In one exemplary implementation, a method for detecting ice is described in which a parameter within an interior volume of a heated conduit is measured. The method also includes detecting the presence of an accumulation
Systems and methods for detecting ice particle accumulation is disclosed herein. In one exemplary implementation, a method for detecting ice is described in which a parameter within an interior volume of a heated conduit is measured. The method also includes detecting the presence of an accumulation of ice particles based on the parameter measured within the interior volume of the heated conduit.
대표청구항▼
We claim: 1. An ice particle detection system, for use on an airborne vehicle, comprising: a conduit having a longitudinal axis substantially parallel with a flow of air, the conduit including an inlet at a fore portion thereof and an outlet at an aft portion thereof; a sensor configured to detect
We claim: 1. An ice particle detection system, for use on an airborne vehicle, comprising: a conduit having a longitudinal axis substantially parallel with a flow of air, the conduit including an inlet at a fore portion thereof and an outlet at an aft portion thereof; a sensor configured to detect when an accumulation of ice particles at least partially clogs the outlet of the conduit and further configured to provide an indication signal when an accumulation of ice particles is detected; a processing device in communication with the sensor; and a heater configured to heat the conduit to a temperature that can melt the ice particles; wherein the cross-sectional area of the inlet is larger than the cross-sectional area of the outlet, such that ice particles in the flow of air can accumulate at the outlet of the conduit. 2. The system of claim 1, wherein the sensor comprises a sensing element and a transducer. 3. The system of claim 2, wherein the sensing element comprises a pressure tap in a wall of the conduit to sense the pressure within the interior of the conduit. 4. The system of claim 3, wherein the transducer comprises a differential pressure sensor configured to sense the pressure within the interior of the conduit with respect to a reference pressure. 5. The system of claim 4, wherein the conduit is a first conduit, the system further comprising a second conduit, the second conduit comprising a second tap configured to provide the reference pressure. 6. The system of claim 5, wherein the heater is a first heater configured to heat the first conduit to a first temperature, the system further comprising a second heater configured to heat the second conduit to a second temperature, wherein the first and second temperatures are associated with a threshold level, whereby a concentration of ice particles above the threshold level results in the accumulation of a blockage of the first conduit and a concentration of ice particles below the threshold level results in the melting of the ice particles to keep the second conduit substantially ice free. 7. The system of claim 6, wherein the processing device is further configured to adjust the heating outputs of the first and second heaters. 8. The system of claim 1, wherein the sensor comprises a pressure sensor supported within a wall of the conduit, the pressure sensor configured to sense the pressure within the interior of the conduit, the processing device further configured to detect an increase in the pressure within the interior of the conduit, the increase being indicative of an accumulation of ice particles in the conduit. 9. The system of claim 1, wherein the sensor comprises a temperature sensor supported within a wall of the conduit for measuring the temperature of the interior of the conduit, the processing device further configured to detect a change of temperature within the interior of the conduit when an accumulation of ice particles forms in the conduit. 10. The system of claim 1, wherein the sensor comprises a light source and an optical receptive device, the light source configured to radiate a light beam through a portion of the interior of the conduit toward the optical receptive device, and wherein the optical receptive device is configured to detect when the light beam is blocked. 11. The system of claim 1, wherein the processing device transmits a warning signal to an external device to indicate an ice clog condition. 12. The system of claim 1, wherein the conduit has a shape selected from the group of shapes consisting of a truncated cone, a horn, and a bottomless bowl. 13. A conduit used in an ice detecting device, the conduit comprising: a hollow tube having a channel through which air is capable of flowing; an inlet located at a first end of the hollow tube, the inlet configured to allow air to enter the channel, the inlet having a first cross-sectional area; and an outlet located at a second end of the hollow tube, the outlet configured to allow air to exit the channel, the outlet having a second cross-sectional area; wherein the first cross-sectional area is greater than the second cross-sectional area such that an obstruction is formed within the channel when the concentration of ice particles in an airflow exceeds a threshold level. 14. The conduit of claim 13, further comprising a strut, for attachment on the aircraft, wherein air flows through the hollow tube when the aircraft is in flight. 15. The conduit of claim 13, wherein the hollow tube has a frustoconical shape. 16. The conduit of claim 13, wherein the diameter of the tube decreases non-linearly from the inlet to the outlet. 17. The conduit of claim 13, further comprising a heating device configured to heat the tube. 18. A method of detecting ice in the vicinity of an airborne vehicle, the method comprising: heating a conduit at a selected power level; measuring a parameter within an interior volume of the conduit; and detecting the presence of an accumulation of ice particles based on the parameter measured within the interior volume of the conduit. 19. The method of claim 18, further comprising: detecting an absence of said accumulation of ice particles when the ice particles are melted by the heating of the conduit; and measuring a length of time from detecting a start of the accumulation of ice particles to detecting a subsequent absence of the accumulation of ice particles. 20. The method of claim 19, further comprising: measuring conditions of air outside the conduit, the conditions of air outside the conduit including at least one of total pressure, static pressure, total temperature, and static temperature; and adjusting the heating of the conduit based on the measured conditions of air outside the conduit. 21. The method of claim 18, wherein the parameter is selected from the group of parameters consisting of pressure, temperature, and light beam obstruction. 22. The method of claim 18, wherein the conduit is a converging conduit. 23. A program stored on a computer-readable medium, the program comprising: logic configured to receive a measurement of a parameter of an interior portion of a conduit, wherein the conduit includes an inlet having a first cross-sectional area and an outlet having a second cross-sectional area, and the first cross-sectional area is greater than the second cross-sectional area; and logic configured to process the parameter of the interior portion of the conduit to detect when ice particles obstruct the outlet of the conduit. 24. The program of claim 23, further comprising logic configured to control a heating output of a heater adapted to heat the conduit. 25. The program of claim 23, further comprising logic configured to generate a signal indicating the presence of an ice particle obstruction at the outlet of the conduit.
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이 특허에 인용된 특허 (13)
Blaha David A. (3323 W. Ridgewood Dr. Parma OH 44134), Aircraft icing detection system.
Botura, Galdemir Cezar; Sweet, Dave Bert; Hindel, James Thomas; Jackson, Darren Glenn, Aircraft ice protection optimization based on ice-detection input.
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