Piezoelectric sensor

• US 5,191,791 A
• Filed: 05/04/1990
• Issued: 03/09/1993
• Est. Priority Date: 01/10/1989
• Status: Expired due to Fees

• Current Assignee: Innovative Dynamics, Inc.
• Original Assignee: Gail A. Hickman, Joseph J. Gerardi, Philip R. Dahl
• Inventors: Dahl, Philip R., Gerardi, Joseph J., Hickman, Gail A.
• Primary Examiner(s): WOODIEL, DONALD
• Application Number:
  US07/518,043
• Time in Patent Office: 1,040 Days
• Field of Search: 73/178 R, 73/178 H, 73/178 T, 73/170 R, 73/147, 364/424.06
• US Class Current: 73/178.00R
• CPC Class Codes: B64D 15/16 by mechanical means
• CPC Class Codes: B64D 15/20 Means for detecting icing or initiating de-icing
• CPC Class Codes: G01M 5/0016 of aircraft wings or blades
• CPC Class Codes: G01M 5/0066 by exciting or detecting vibration or acceleration vibration testing of structures G01M7/00
• CPC Class Codes: G01M 5/0083 by measuring variation of impedance, e.g. resistance, capacitance, induction
• CPC Class Codes: G08B 19/02 Alarm responsive to formation or anticipated formation of ice

Abstract

The change in capacitance of a sensor is linearly proportional to ice thickness provided that the ice thickness is significantly less than the distance between the conductive electrodes. By employing sensors with different electrodes, the sensitivity to ice may be traded off against the ability to measure greater ice thickness. A sensor with small spacing between electrodes will exhibit a large change in capacitance when covered by a thin layer of ice, however, the capacitance change will be linear only for very thin layers of ice. A sensor with greater spacing between electrodes is less sensitive to ice accretion but has a correspondingly greater ice thickness measurement range. Accordingly, sensor (55) is relatively sensitive and is employed to determine whether or not ice or water is present. This is accomplished by circuit (60) determini

STATEMENT REGARDING GOVERNMENT FUNDED RESEARCH

This invention was made with Government support under NAS1-18421, NAS2-12890 and NAS3-25618 awarded by the National Aeronautics and Space Administration. The Government has certain rights in this invention.

Claims

1. An apparatus for measuring localized ice thickness comprising:

an ice presence sensor having a first metallization layer facing towards an environment, a second metallization layer, and a dielectric layer between said first and second metallization layers, said second metallization layer being greater in surface area than said first metallization layer, wherein existence of ice in an area surrounding said first metallization layer causes a capacitance value associated with said ice presence sensor to change; and

an ice thickness sensor having a dielectric layer, and having first and second metallization layers located on one side of said dielectric layer and facing towards the environment, wherein existence of ice in an area between said first and second layers of said ice thickness sensor causes a capacitance value associated with said ice thickness sensor to change.

2. The sensor of claim 1 further comprising a temperature sensor having a first metallization layer facing towards the environment, a second metallization layer, and a dielectric layer between said first and second metallization layers of said temperature sensor, wherein said dielectric layer has a dielectric constant which varies in a known manner with temperature.

3. The sensor of claim 1 further comprising capacitance measuring means for measuring a capacitance value of said ice presence sensor in which said first and second metallization layers of said ice presence sensor function as electrodes, and for measuring a capacitance value of said ice thickness sensor in which said first and second metallization layers of said ice thickness sensor function as electrodes.

4. The sensor of claim 1 wherein said dielectric layer of said ice presence sensor and said dielectric layer of said ice thickness sensor comprise corresponding portions of a single dielectric layer.

5. The sensor of claim 4 wherein said single dielectric layer is constructed from polyvinylidene fluoride.

6. The sensor of claim 1 wherein said ice presence sensor has a capacitance value without ice or water present which is greater than a capacitance value of said ice thickness sensor without ice or water present.

7. The sensor of claim 1 wherein said dielectric layer of said ice presence sensor and said dielectric layer of said ice thickness sensor are constructed from piezoelectric material.

8. An apparatus for detecting non-localized icing on a surface, comprising:

transducer means for transducing aerodynamic forces applied over the surface and to said transducer means into electrical signals, said transducer means being attached to said surface, and said aerodynamic forces varying in accordance with formation of ice on said surface and upstream from said transducer means; and

signal processing means for processing said electrical signals to detect a change in said electrical signals upon the formation of ice on said surface and upstream from said transducer means.

9. An apparatus for detecting non-localized icing on an aircraft wing comprising;

a plurality of transducer means for transducing forces applied to said transducer means into electrical signals, said transducer means being attachable to and placed on said aircraft wing at various chord lengths downstream from a leading edge of said wing; and

signal processing means for processing said electrical signals so as to detect a change in said electrical signals upon the formation of ice upstream from said transducer means, and said signal processing means for processing said electrical signals to determine the boundary layer flow characteristics and then correlating the boundary layer flow characteristics to ice thickness.

10. The apparatus of claim 9 wherein said signal processing means detects ice formation upstream from at least one of said transducer means by detecting boundary layer separation.

11. The apparatus of claim 9 further comprising a boot in which said plurality of transducer means are located and which is retrofittable onto said wing.

12. The apparatus of claim 9 wherein said plurality of transducer means are embedded within said wing.

13. The apparatus of claim 9 wherein said plurality of transducer means comprises a piezoelectric sensor having a first metallization layer, a second metallization, and a piezoelectric layer therebetween.

14. A sensor for determining ice thickness on a surface comprising:

first and second electrodes arranged on the surface such that the capacitance between said first and second electrodes is indicative of the presence of ice on said surface;

third and fourth electrodes arranged on the surface such that the capacitance between said third and fourth electrodes varies in accordance with the amount of ice on said surface; and

fifth and sixth electrodes arranged on the surface such that the capacitance between said fifth and sixth electrodes varies in accordance with the temperature of said surface.