Resonator-based, surface-condition sensor

• US 5,695,155 A
• Filed: 09/21/1995
• Issued: 12/09/1997
• Est. Priority Date: 09/21/1995
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Macdonald, Perry A., Butler, Jennifer M.
• Primary Examiner(s): Kashnikow, Andres
• Assistant Examiner(s): DINH, TIEN QUANG
• Application Number:
  US08/531,876
• Time in Patent Office: 810 Days
• Field of Search: 244/134 F, 340/580, 340/581, 340/582, 340/583, 340/962, 73/170.26
• US Class Current: 244/134.00F
• CPC Class Codes: B64D 15/20 Means for detecting icing or initiating de-icing

Abstract

A sensor is provided for detecting the presence of dielectric media, e.g., ice. The sensor includes a plurality of microstrip resonators which are positioned for electromagnetic coupling with a microstrip transmission line. The resonators produce amplitude minima in a radio-frequency signal that is carried over the transmission line. The resonance of the resonators changes in response to the addition of a dielectric coating. Each resonator can be configured with a different resonant frequency which serves as a signature that identifies the respective resonator'"'"'s position. The sensor has a thin aerodynamic profile, can conform to nonplanar surfaces and its installation requires no intrusion into an aircraft skin.

Claims

1. A sensor for use with a swept-frequency signal in identifying the presence and thickness of a dielectric media on a surface, said sensor comprising:

an elongate transmission line positioned across said surface; and

at least one resonator configured to have a resonant frequency, positioned on said surface and separated from said transmission line by a space to electromagnetically couple said resonator with said transmission line;

said resonator producing a detectable difference at said resonant frequency in an amplitude response of said swept-frequency signal when said swept-frequency signal is transported along said transmission line; and

said resonant frequency having a frequency shift in response to the presence of said dielectric media on said resonator with the extent of said frequency shift corresponding to said dielectric media thickness.

2. The sensor of claim 1, wherein said at least one resonator includes a plurality of resonators arranged along said transmission line with each resonator configured to have a different one of a plurality of resonant frequencies.

3. The sensor of claim 1, wherein said transmission line is a microstrip transmission line and said resonator includes a microstrip signal line arranged to form a closed path.

4. The sensor of claim 3, wherein said closed path is arranged in the form of a circle.

5. The sensor of claim 3, wherein said closed path is arranged in the form of a polygon.

6. The sensor of claim 3, wherein said closed path has a length substantially equal to nλ

_g wherein n is a positive integer and λ

_g is a wavelength of said resonant frequency in said microstrip signal line.

7. The sensor of claim 1, wherein said transmission line is a microstrip transmission line and said resonator is a microstrip patch resonator.

8. A sensor system for identifying the presence and thickness of a dielectric media on a surface, comprising:

an elongate transmission line positioned across said surface;

at least one resonator configured to have a resonant frequency, positioned on said surface and separated from said transmission line by a space to electromagnetically couple said resonator with said transmission line;

a generator configured to generate a swept-frequency signal, said generator coupled to said transmission line; and

a detector coupled to said transmission line for detecting an amplitude response of said signal;

wherein said generator, said resonator and said detector are positioned so that said signal couples to said resonator prior to its detection by said detector;

said resonator producing a detectable difference at said resonant frequency in said amplitude response; and

said resonant frequency having a frequency shift in response to the presence of said dielectric media on said resonator with the extent of said frequency shift corresponding to said dielectric media thickness.

9. The system of claim 8, wherein:

said transmission line has a characteristic impedance and first and second ends;

said generator and said detector are coupled to said first end; and

said second end is configured to have an impedance which differs from said characteristic impedance.

10. The system of claim 8, wherein:

said transmission line has first and second ends;

said generator is coupled to said first end; and

said detector is coupled to said second end.

11. The system of claim 8, wherein said at least one resonator includes a plurality of resonators arranged along said transmission line with each resonator configured to have a different one of a plurality of resonant frequencies.

12. The system of claim 8, wherein said transmission line is a microstrip transmission line and said resonator includes a microstrip signal line arranged to form a closed path.

13. The system of claim 12, wherein said closed path is arranged in the form of a circle.

14. The system of claim 12, wherein said closed path is arranged in the form of a polygon.

15. The system of claim 12, wherein said closed path has a length substantially equal to nλ

_g wherein n is a positive integer and λ

_g is a wavelength of said resonant frequency in said microstrip signal line.

16. The system of claim 8, wherein said transmission line is a microstrip transmission line and said resonator is a microstrip patch resonator.

17. An aircraft equipped with a sensor system for identifying the presence and thickness of ice, comprising:

an aircraft having an aerodynamic surface;

an elongate transmission line positioned across said surface;

at least one resonator configured to have a resonant frequency, positioned on said surface and separated from said transmission line by a space to electromagnetically couple said resonator with said transmission line;

a generator configured to generate a swept-frequency signal, said generator coupled to said transmission line; and

a detector coupled to said transmission line for detecting an amplitude response of said signal;

wherein said generator, said resonator and said detector are positioned so that said signal couples to said resonator prior to its detection by said detector;

said resonator producing a detectable difference at said resonant frequency in said amplitude response; and

said resonant frequency having a frequency shift in response to the presence of said dielectric media on said resonator with the extent of said frequency shift corresponding to said dielectric media thickness.

18. The aircraft and sensor system of claim 17, wherein:

said transmission line has a characteristic impedance and first and second ends;

said generator and said detector are coupled to said first end; and

said second end is configured to have an impedance which differs from said characteristic impedance.

19. The aircraft and sensor system of claim 17, wherein said at least one resonator includes a plurality of resonators arranged along said transmission line with each resonator configured to have a different one of a plurality of resonant frequencies.

20. The aircraft and sensor system of claim 17, wherein said transmission line is a microstrip transmission line and said resonator includes a microstrip signal line arranged to form a closed path.

21. A sensor for use with a swept-frequency signal in identifying the presence and thickness of a dielectric media on a surface, said sensor comprising:

a plurality of electromagnetic resonators arranged over said surface and each configured to have a respective resonant frequency; and

an elongate transmission line arranged across said surface so as to be separated from each of said resonators by a space which electromagnetically couples that resonator to said transmission line;

the magnitude of said swept-frequency signal across said transmission line being reduced at the resonant frequency of each of said electromagnetic resonators by electromagnetic coupling between that resonator and said transmission line and the resonant frequency shifting in response to the presence and thickness of said dielectric media on said surface.

22. The sensor of claim 21, wherein each of said resonators is configured to have a different resonant frequency.

23. The sensor of claim 21, wherein said transmission line is a microstrip transmission line and each of said resonators includes a microstrip signal line arranged to form a closed path.

24. The system of claim 21, wherein said transmission line has a characteristic impedance and one end of said transmission line is configured to have an impedance which differs from said characteristic impedance.