Sonic Anemometer Low-Pressure Wind Speed Measurement

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Solution Overview

Problem

Sonic anemometers face challenges in accurately measuring wind speeds in low-pressure environments, such as those found on Mars, due to issues like radiative heating, low convective heat losses, and sensitivity to temperature and pressure fluctuations, which affect the accuracy and precision of traditional measurement methods.

Innovation Solution

A sonic anemometer system utilizing multiple transducer pairs that measure bi-directional acoustic data to calculate flow speed, with a controller configured to correct for temperature, pressure, and wake effects using a system model, enabling precise measurements in low-pressure conditions by determining phase lags and flight times, and generating reports on flow speed.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional hot wire/film systems are used for wind speed measurement, then the measurement mechanism is simple, but the accuracy and precision deteriorate in low-pressure environments

Engineering Contradiction:
Improvewind speed measurement accuracyVSAvoidmeasurement system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces traditional mechanical hot wire/film anemometers with a sonic anemometer system that uses ultrasonic transducers and acoustic wave propagation measurements. This substitution eliminates the mechanical heating elements that fail in low-pressure environments, using instead the propagation of sound waves through the atmosphere to measure wind speed, thereby achieving accurate measurements in low-pressure conditions without relying on thermal convection mechanisms

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The patent changes the measurement parameter from thermal convection (hot wire/film) to acoustic wave propagation (sonic transducers). By measuring the time of flight and phase differences of ultrasonic waves traveling through the atmosphere, the system adapts to low-pressure environments where thermal convection is insufficient, fundamentally changing the physical parameter used for wind speed measurement

Inventive Principle:
Principle #35Parameter changes

2Measurement precision

If sonic anemometer system is used, then measurement accuracy in low-pressure environments improves, but device complexity increases

Engineering Contradiction:
Improvewind speed measurement accuracyVSAvoidtransducer and control system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent implements a controller that performs multiple functions: it measures time of flight, calculates phase differences, compensates for temperature and pressure effects, and generates flow speed measurements. This multi-functional controller consolidates what would otherwise require separate systems, reducing overall device complexity while maintaining high measurement accuracy in low-pressure environments

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent incorporates feedback mechanisms where the controller continuously monitors environmental conditions (temperature, pressure) and adjusts measurements accordingly. The system uses feedback loops to compensate for environmental variations affecting acoustic wave propagation, ensuring accurate wind speed measurements by dynamically adjusting for temperature and pressure effects on sound speed

Inventive Principle:
Principle #23Feedback

3Reliability

If multiple transducer pairs are used for bi-directional measurements, then measurement reliability improves, but device complexity increases

Engineering Contradiction:
Improvemeasurement reliabilityVSAvoidnumber of transducer pairs
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines multiple transducer pairs into an integrated sonic anemometer system where all transducers are coordinated by a single controller. The bi-directional measurements from multiple transducer pairs are merged and processed together to calculate three-dimensional flow vectors, achieving high reliability through redundant measurements while consolidating control functions to manage system complexity

Inventive Principle:
Principle #5Merging (Combining)

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

The system provides accurate and precise wind speed measurements in low-pressure environments, offering 20 times improvement over traditional hot wire/film systems, with sensitivity to winds as small as 5 cm/s and independent measurements at 20 Hz, suitable for planetary science applications and high-altitude measurements.

Implementation Method 1

A sonic anemometer uses ultrasonic sound waves to determine wind speed. Broadly, wind speed can be determined in real-time by measuring the effect of the wind on the speed of sound waves traveling between a pair of transducers.

Methodology Applied
Scientific EffectSound wave propagation: Sound

Implementation Method 2

The controller is further configured to measure phase lags corresponding to the bi-directional acoustic data, and determine bi-directional flight times using the phase lags.

Methodology Applied
Scientific EffectPhase lag measurement:

Data Source

PatentUS12085430B2Systems and methods for operation of a sonic anemometer
Publication Date: 2024.09.10 VANDERVALK NEESON INSTRUMENTS LTD
  • US12085430B2 patent drawing
  • US12085430B2 patent drawing
  • US12085430B2 patent drawing

AI summary

A method of determining flow speed in a low pressure environment. The method includes obtaining bi-directional acoustic data from a plurality of transducer pairs as a fluid moves relative to the plurality of transducer pairs. The method further includes measuring phase lags corresponding to the bi-directional acoustic data, and determining bi-directional flight times using the phase lags. Additionally, the method includes calculating a flow speed of the fluid corresponding to each transducer pair from the bi-directional flight times. The method includes correcting for at least one of temperature effects, pressure effects, and wake effects, using a system model. The method further includes generating a report including the flow speed of the fluid.