Optical system and element for detecting ice and water
View Patent ↗An optical system for detecting ice and water on the surface of an aircraft includes an elongated transparent optical element having first and second end portions. A light source and light detector are disposed in one end of the optical element and a reflective surface is disposed in the opposite end portion. The reflective surface defines a critical angle and reflects light from the light source to the light detector when the critical angle is in contact with air and refracts the light toward the external environment when the reflective surface is in contact with ice or water. The system may also incorporate an optical element wherein the reflective surface includes a continuous array of convex elements extending outwardly from and across one end of the optical element and wherein each of the convex elements defines a critical angle.
1. An optical element for use in detecting ice and water on a surface of an aircraft, said element comprising:
an elongated transparent body defining an optical channel and a light source for generating a beam of light disposed at one end of said elongated transparent body, a light detector and means for generating variable signals dependent on an amount of light received by said detector disposed in said one end of said elongated transparent body, and a reflective surface at an opposite end of said elongated transparent body and said reflective surface comprising a plurality of convex elements extending outwardly from said elongated transparent body and wherein each of said convex elements define a critical angle whereby light from said light source is reflected toward said light detector when said convex elements are in contact with air and refracted toward an external environment when said convex elements are in contact with ice or water.
2. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 1 , in which said reflective surface comprises a continuous array of convex elements extending outwardly from and across said opposite end of said elongated transparent body.
3. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 2 , which includes a temperature sensor in said opposite end of said elongated transparent body.
4. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 3 , in which each of said convex elements defines a prism.
5. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 3 , in which each of said convex elements defines a cone.
6. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 4 , in which each of said prisms defines an angle of about 90°.
7. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 6 , in which each of said convex elements have a height of less than 0.25 inches.
8. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 6 , in which said elongated transparent body is glass.
9. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 6 , in which said elongated transparent body is plastic.
10. An optical element for use in detecting ice and water on the surface of an aircraft according to claim 6 , in which said elongated transparent body is quartz.