System and method for deriving airspeed from a particle sensor

Patent metadata

Field	Value
Publication number	US-11525841-B2
Application number	US-201815957629-A
Country	US
Kind code	B2
Filing date	Apr 19, 2018
Priority date	Apr 19, 2018
Publication date	Dec 13, 2022
Grant date	Dec 13, 2022

Abstract

A system comprises a particle sensor assembly, which includes a light source that transmits a light beam into an external interrogation air region; a set of receive optics that provides a receive channel, the receive optics configured to collect a scattered portion of the light beam from a particle in the interrogation air region; and an optical detector that receives the collected scattered portion. The optical detector measures a signal intensity as a function of time from the scattered portion, with the signal intensity indicating a particle size and a signal duration indicating motion of the particle through the interrogation air region. A processor is in communication with the optical detector and is operative to determine a transit time of the particle through the interrogation air region based on the signal duration, and compute an airspeed based on parameters comprising the transit time and a size of the light beam.

First claim

What is claimed is:

1. A system comprising:
a particle sensor onboard a vehicle, the particle sensor provided to one side of an external interrogation air region, the particle sensor comprising:
at least one light source configured to transmit a light beam into the external interrogation air region;
a set of receive optics configured to provide at least one receive channel, the receive optics configured to collect a scattered portion of the transmitted light beam from at least one particle in the external interrogation air region; and
an optical detector in communication with the at least one receive channel and configured to receive the collected scattered portion of the transmitted light beam, the optical detector operative to measure a signal intensity as a function of time from the scattered portion, the signal intensity indicating a particle size and a signal duration indicating motion of the at least one particle through the external interrogation air region; and

a processor in communication with the optical detector, the processor operative to:
determine a transit time of the at least one particle through the external interrogation air region based on the signal duration;
determine a size of the at least one particle based on the signal intensity; and
compute an estimated airspeed based on parameters comprising the transit time, the size of the at least one particle, and a size of the light beam.

2. The system of claim 1 , wherein the at least one light source comprises a laser transmitter.

3. The system of claim 2 , wherein the laser transmitter and the receive optics are implemented in an optical transceiver configured to collect a scattered portion of the transmitted light beam.

4. The system of claim 1 , wherein the processor is further operative to:
compute the estimated airspeed based on the parameters comprising the transit time, the size of the at least one particle, and the size of the light beam using the following equation:
estimated airspeed =(w+d)/(tt) where w is a width of the light beam, d is a diameter of the at least one particle, and tt is the transit time of the at least one particle.

5. The system of claim 1 , wherein the optical detector comprises a particle by particle detector that is configured to record the transit time of each particle in the external interrogation air region, allowing for derivation of true airspeed (TAS), and/or indicated airspeed (IAS), and/or calibrated airspeed (CAS), from the transit time and size of each particle.

6. The system of claim 1 , wherein the particle sensor assembly and is configured to operate in a potential icing environment.

7. The system of claim 1 , wherein the vehicle is an aircraft.

8. The system of claim 7 , wherein the processor is further operative to send the estimated airspeed to an avionics unit onboard the aircraft.

9. A method for an aircraft, the method comprising:
providing a particle sensor onboard the aircraft a vehicle, and a processor;
providing the particle sensor to one side of an external interrogation air region, the particle sensor comprising at least one light source, a set of receive optics configured to provide at least one receive channel, the receive optics collocated with the at least one light source, and an optical detector in communication with the at least one receive channel;
transmitting a light beam from the at least one light source into the external interrogation air region;
collecting in the receive optics, a scattered portion of the transmitted light beam from at least one particle in the external interrogation air region;
receiving in the optical detector, the collected scattered portion of the transmitted light beam from the at least one receive channel; and
measuring with the optical detector, a signal intensity as a function of time from the scattered portion, the signal intensity indicating a particle size and a signal duration indicating motion of the at least one particle through the external interrogation air region;
wherein the processor is in communication with the optical detector, and the processor performs a method comprising:
determining a transit time of the at least one particle through the external interrogation air region based on the signal duration;
determining a size of the at least one particle based on the signal intensity; and
computing an estimated airspeed based on parameters comprising the transit time, the size of the at least one particle, and a size of the light beam.

10. The method of claim 9 , wherein the at least one light source comprises a laser transmitter.

11. The method of claim 10 , wherein the laser transmitter and the receive optics are implemented in an optical transceiver that collects a scattered portion of the transmitted light beam.

12. The method of claim 9 , wherein:
the estimated airspeed is computed based on the parameters comprising the transit time, the size of the at least one particle, and the size of the light beam using the following equation:
estimated airspeed =(w+d)/(tt) where w is a width of the light beam, d is a diameter of the at least one particle, and tt is the transit time of the at least one particle.

13. The method of claim 9 , wherein the optical detector comprises a particle by particle detector that is configured to record the transit time of each particle in the external interrogation air region, allowing for derivation of true airspeed (TAS), and/or indicated airspeed (IAS), and/or calibrated airspeed (CAS), from the transit time and size of each particle.

14. The method of claim 9 , further comprising:
sending the estimated airspeed to an avionics unit onboard the aircraft.

15. The method of claim 9 , wherein a particle by particle estimated airspeed is averaged over a time frame to generate an average estimated airspeed.

Assignees

• Honeywell Int Inc

Inventors

• Wienkes Lee R
• Wiebold Matthew
• Fan Xiao Zhu

Classifications

• G01S17/58

  Velocity or trajectory determination systems; Sense-of-movement determination systems · CPC title

• G01F1/7086

  using optical detecting arrangements · CPC title

• G01P5/26 Primary

  by measuring the direct influence of the streaming fluid on the properties of a detecting optical wave · CPC title

• G01N15/1459 Primary

  the analysis being performed on a sample stream · CPC title

• G01N2015/0003

  Determining electric mobility, velocity profile, average speed or velocity of a plurality of particles · CPC title