Microwave ice detector

• US 4,054,255 A
• Filed: 04/01/1976
• Issued: 10/18/1977
• Est. Priority Date: 04/01/1976
• Status: Expired due to Term

• Current Assignee: System Development Incorporated
• Original Assignee: System Development Incorporated
• Inventors: Magenheim, Bertram
• Primary Examiner(s): Blix, Trygve M.
• Assistant Examiner(s): Kelmachter, Barry L.
• Application Number:
  US05/672,616
• Time in Patent Office: 565 Days
• Field of Search: 244/134 R, 244/134 D, 244/134 F, 73/170 R, 73/178 H, 324/58.5 B, 416/95, 340/234, 343/704
• US Class Current: 244/134.00F
• CPC Class Codes: B64D 15/20 Means for detecting icing or initiating de-icing
• CPC Class Codes: G08B 19/02 Alarm responsive to formation or anticipated formation of ice

Abstract

A system for detecting ice on exterior surfaces of aircraft by transmitting a relatively low power microwave electromagnetic signal into a dielectric layer functioning as a surface waveguide, and monitoring the signals transmitted into and reflected from the waveguide. The waveguide includes a termination element which is mismatched with the waveguide impedance, resulting in partial or total reflection of the microwave energy from the remote end of the waveguide. As ice builds up on the surface waveguide, the impedance or reflection characteristics of the composite waveguide comprising the ice layer and the permanent surface waveguide give a reliable indication of the presence and location of the ice. The reflection characteristics are conventionally monitored utilizing a dual directional coupler and a reflectometer.

Claims

1. Aircraft ice detection apparatus, comprising:

a source of microwave electromagnetic energy;

surface waveguide coupling means for coupling the microwave energy to a surface layer of ice in such a manner that the ice functions as a surface waveguide and the energy is transmitted along the layer in a direction substantially parallel with the layer and with the surface on which it is formed, and is at least partially reflected back to said coupling means on reaching the end of the ice layer;

signal monitoring means for comparing microwave signals transmitted into and reflected from the ice layer;

whereby variations in the amount of ice result in corresponding variations in the reflected energy signal.

2. Aircraft ice detection apparatus, comprising:

a surface waveguide of dielectric material overlying a surface to be deiced;

a source of microwave electromagnetic energy;

a surface waveguide coupler for coupling the microwave energy to said surface waveguide;

a dual directional coupler connected between said microwave energy source and said surface waveguide coupler to monitor the transmission of energy in both directions; and

reflectometer means coupled with said dual directional coupler, to monitor the relationship between the microwave energy transmitted into said waveguide and the energy reflected from said waveguide;

whereby the reflection characteristics of said surface waveguide will be modified by the presence of ice thereon and said reflectometer means is indicative of the presence of ice.

3. Apparatus as set forth in claim 2, and further including waveguide terminating means operative to reflect at least partially the energy transmitted along said surface waveguide.

4. A method of detecting ice on exterior surfaces of aircraft, comprising the steps of:

generating a microwave electromagnetic signal;

coupling the microwave signal to a permanent surface waveguide of dielectric material having a dielectric constant approximately the same as that of ice;

transmitting the microwave signal along the surface waveguide in a direction substantially parallel with a surface on which ice is to be detected;

reflecting at least a portion of the microwave energy back along the waveguide from its remote end; and

detecting in a reflectometer a ratio between transmitted and reflective energy with respect to the waveguide;

whereby accretion of ice on the surface waveguide results in a different reflection characteristic of the composite waveguide comprising the ice layer and the permanent surface waveguide, and the presence and location of ice may be detected by means of the reflectometer.

5. Aircraft ice detection apparatus, comprising:

a source of microwave electromagnetic energy;

surface waveguide coupling means for coupling the microwave energy to a surface layer of ice in such a manner that the ice functions as a surface waveguide, said surface waveguide coupling means including a permanent surface waveguide of dielectric material overlying a surface on which the presence of ice is to be detected, and further including means for coupling the microwave energy to said permanent surface waveguide in such a manner that the energy is transmitted along said permanent surface waveguide and along any ice layer formed there on, as a composite surface waveguide; and

signal monitoring means for comparing the microwave signals transmitted into and reflected from the ice layer;

whereby variations in the amount of ice result in corresponding variations in the amount of reflected energy.