Impedance type ice detector

• US 5,955,887 A
• Filed: 12/20/1996
• Issued: 09/21/1999
• Est. Priority Date: 12/22/1995
• Status: Expired due to Term

• Current Assignee: Goodrich Corporation (Rtx Corporation)
• Original Assignee: Goodrich Corporation (Rtx Corporation)
• Inventors: Pruzan, Daniel A., Codner, Gerald Willey, Reich, Allen Donald, Rauckhorst, Richard Lawrence III, Sweet, David Bert
• Primary Examiner(s): Ballato, Josie
• Assistant Examiner(s): Solis, Jose M.
• Application Number:
  US08/770,923
• Time in Patent Office: 1,005 Days
• Field of Search: 324/664, 324/671, 324/687, 324/688, 324/689, 324/690, 324/665, 324/679
• US Class Current: 324/689
• CPC Class Codes: B64D 15/20 Means for detecting icing or initiating de-icing
• CPC Class Codes: G01N 27/041 of a solid body

Abstract

An ice detector includes a pair of electrodes connected by a pair of leads to a control unit which measures the total impedance between leads to thereby sense and detect the presence of ice and other contaminants formed on top thereof utilizing a comparator circuit. The electrodes are integrated into patch which can be placed at different locations on an aircraft.

Claims

1. An apparatus for detecting ice on a surface of an aircraft exposed to the environment comprising:

first, second and third electrodes disposed at the exposed surface of the aircraft, the electrodes being spaced apart and arranged substantially parallel to the plane of the surface, wherein the second electrode is spaced closer to the first electrode than the third electrode;

a signal driver for applying a drive signal to the first electrode;

a first device for providing a first signal indicative of the current flowing through the second electrode;

a second device for providing a second signal indicative of the current flowing through the second electrode; and

,

a third device for determining the difference between the second and third signal.

2. An apparatus in accordance with claim 1, wherein the apparatus operates while the aircraft is in operation.

3. A method of detecting ice on the surface of an aircraft comprising the steps of:

providing first, second and third electrodes disposed at the exposed surface of the aircraft, the electrodes being spaced apart and arranged substantially parallel to the plane of the surface, wherein the second electrode is spaced closer to the first electrode than the third electrode;

applying a signal to the first electrode;

providing a first signal indicative of the current flowing through the second electrode;

providing a second signal indicative of the current flowing through the second electrode; and

,

determining the difference between the second and third signal.

4. A method of detecting ice on the surface of an aircraft in accordance with claim 3, wherein the steps are performed while the aircraft is in operation.

5. A method of detecting ice on the surface of an aircraft comprising the steps of:

providing first, second and third electrodes disposed at the exposed surface of the aircraft, the electrodes being spaced apart and arranged substantially parallel to the plane of the surface, wherein the second electrode is spaced closer to the first electrode than the third electrode;

applying a signal to the first electrode;

providing a first signal indicative of the current flowing through the second electrode;

providing a second signal indicative of the current flowing through the second electrode; and

,

correlating the thickness of the ice on the surface with a determination of when the second and third signals are equal.

6. A method of detecting ice on the surface of an aircraft in accordance with claim 5, wherein the steps are performed while the aircraft is in operation.