System and method for detecting ice formation on an aircraft
View Patent ↗A system and method for detecting ice formation on the surface of an aircraft includes a small rotatable disc disposed on and flush with a surface of a aircraft wing and/or stabilizer and a DC motor for rotating the disc. The disc is rotated periodically and the peak current which is directly proportional to the torque required to break any ice is monitored. When the torque exceeds a pre-selected amount a warning is sounded in the cockpit. If the torque required to rotate the disc increases a second warning is given and the amount of ice accumulation is calculated. In one embodiment of the invention, a stall warning system is automatically modified to increase the margin to accommodate for the increase due to ice accumulation.
1. A system for detecting ice formation on an outer surface, said system comprising:
means defining a small moveable surface area flush with the outer surface of an aircraft and exposed to the atmosphere;
means for rotating said small moveable surface to break any ice formed between said small moveable surface and the surface of an aircraft;
means for determining the torque required to rotate the small moveable surface area; and
means for warning a pilot of ice formation when the torque required to rotate the small moveable surface area exceeds a pre-selected amount.
2. A system for detecting ice formation on an outer surface of an aircraft according to claim 1 which includes means for periodically rotating the small moveable surface area.
3. A system for detecting ice formation on an outer surface of an aircraft according to claim 2 in which said small moveable surface area is a portion of a cylinder.
4. A system for detecting ice formation on an outer surface of an aircraft according to claim 2 in which said small moveable surface area is a circular disc.
5. A system for detecting ice formation on an outer surface of an aircraft according to claim 2 in which said means for rotating said small moveable surface area is a DC electric motor.
6. A system for detecting ice formation on an outer surface of an aircraft according to claim 5 in which torque is determined by measuring the peak current to rotate the small moveable surface area.
7. A system for detecting ice formation on an outer surface of an aircraft according to claim 6 which includes means for comparing the peak currents at two periods of time and means for issuing a second warning signal of ice accumulation when a subsequent peak current exceeds a previous peak current that was above the pre-selected amount.
8. A system for detecting ice formation on an outer surface of an aircraft according to claim 4 in which the circular disc is flush with the surface of a wing.
9. A system for detecting ice formation on an outer surface of an aircraft according to claim 4 in which the circular disc is flush with the surface of a horizontal stabilizer.
10. A system for detecting ice formation on an outer surface of an aircraft according to claim 4 in which the disc has a small air gap between its edge and the surface of the aircraft.
11. A system for detecting ice formation on an outer surface of an aircraft according to claim 2 in which said means for rotating said moveable surface is a torque programmable motor which includes means for increasing the torque in small steps until the small moveable surface breaks free of ice.
12. A system for detecting ice formation on an outer surface of an aircraft according to claim 7 which includes means for determining the ice accumulation on the surface of the aircraft.
13. A system for detecting ice formation on an outer surface of an aircraft according to claim 12 which includes a stall warning system and means for increasing the margin on the stall warning system to accommodate for ice accumulated on the surface of the aircraft.
14. A method for detecting ice formation on an outer surface of an aircraft comprising the steps of:
providing a small rotatable surface area flush with an outer surface of an aircraft and exposed to the atmosphere;
rotating the small moveable surface;
determining the torque required to rotate the small moveable surface; and
warning a pilot of ice formation when the torque required to rotate the small moveable surface area exceeds a predetermined amount.
15. A method for detecting ice formation on an outer surface of an aircraft according to claim 14 in which the small moveable surface is rotated periodically and in which a second warning is given to the pilot when the torque required for a subsequent rotation exceeds the torque required for a previous rotation.
16. A method for detecting ice formation on an outer surface of an aircraft according to claim 14 which includes the step of providing a stall warning system and increasing the margin on the stall warning system to accommodate for ice accumulation.