Optical device for the detection of icing conditions on aircraft

• US 6,091,335 A
• Filed: 09/03/1998
• Issued: 07/18/2000
• Est. Priority Date: 09/09/1997
• Status: Expired due to Fees

• Current Assignee: Sextant Avionique
• Original Assignee: Sextant Avionique
• Inventors: Naim, Monique, Choisnet, Joel, Breda, Jean-Marc
• Primary Examiner(s): Lee, Benjamin C.
• Application Number:
  US09/146,539
• Time in Patent Office: 684 Days
• Field of Search: 340/580, 340/581, 340/583, 340/584, 340/588, 340/589, 340/600, 340/604, 340/602, 340/905, 250/573, 250/574, 250/578.1, 250/575, 244/134 F, 73/170.26, 73/170.17, 342/26, 342/22, 342/460, 356/381, 356/382, 356/338
• US Class Current: 340/580
• CPC Class Codes: B64D 15/20 Means for detecting icing or initiating de-icing

Abstract

An optical device on board an aircraft for detecting icing conditions including an optical beam emitter to create at least one illuminated external volume of measurement through which there circulates a flow of air charged with water particles; a collector optical system for the collection of at least a part of the light beam back-scattered by the water particles (the external volume of measurement being located on the optical axis of said collector optical system); a photodetector for detecting back-scattered optical beams; a signal processor for processing the signal delivered by the photodetector to compute the severity of the icing conditions; an information provider for providing information on the calculated severity of the icing conditions. Advantageously, the optical means for the differentiation of device includes a differentiation for differentiating between liquid water particles and solid water particles, based on analysis of the polarization.

Claims

1. An optical device on board an aircraft and coupled to temperature and velocity sensors of the aircraft for detecting icing conditions, the device comprising:

an optical beam emitter for emitting an optical beam to create at least one illuminated volume of measurement external to the aircraft through which flows air charged with water particles;

a collector optical system for collecting a portion of light back-scattered by the water particles, wherein the volume of measurement is located on an optical axis of said collector optical system;

photodetection means for detecting a varying polarization of the back-scattered light collected by the collector optical system over time to distinguish between liquid water particles and ice particles;

a signal processor for processing a signal output by the photodetection means, a velocity received from the velocity sensors, and a temperature received from the temperature sensor to compute a severity of the icing conditions, wherein the severity of icing conditions is indicative of a water concentration multiplied by a speed of the aircraft; and

means for providing information on the computed severity of the icing conditions, wherein the optical beam emitter is external to a back-scattering path of the back-scattered light.

2. The optical device according to claim 1, wherein the optical beam comprises a laser diode.

3. The optical device according to claim 2, wherein the laser diode is polarized and the collector optical system comprises a polarization separator, delivering two optical beams with different types of polarization.

4. The optical device according to claim 3, wherein the photodetection means comprise two photodetectors for collecting the two optical beams with different types of polarization.

5. An optical device for the detection of icing conditions according to claim 3, wherein collector optical system further comprises means to introduce a difference in optical path for the two optical beams with different types of polarization, the photodetection means comprising a photodetector to receive the two optical beams with different types of polarization that are temporally staggered due to the difference in optical path.

6. An optical device according to claim 2, further comprising a birefringent element, interposed between the laser diode and an exterior of the aircraft, for creating, from the optical beam delivered by the laser diode, two external volumes of measurement and two optical beams back-scattered by the water particles, wherein the photodetection means comprises a photodetector to receive two temporally staggered optical beams.

7. An optical device according to claim 1, further comprising:

a first optical fiber for carrying the emitted optical beam within the first optical fiber up to an external end of the temperature probe externally mounted on the aircraft; and

a second optical fiber mounted on the external end of the temperature probe for receiving the back-scatter light and applying the back-scattered light through the second optical fiber to the collector optical system.

8. An optical device according to claim 1, wherein optical axes of the optical beam emitter and the photodetection means mutually form a rainbow angle of about 40°

to optimize an energy received by the photodetection means.