Self-Sustaining Aerological Sonde for Direct Storm Turbulence Sensing

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Solution Overview

Problem

Existing aerological sondes have limited capability to provide detailed data on the intensity and strength of cyclonic storms, relying primarily on GPS location information for intensity and strength data, which is insufficient for accurate weather prediction.

Innovation Solution

An aerological sonde with a self-sustaining design that utilizes a turbulence sensor and gyroscopic or accelerometer components to measure turbulence and orientation in atmospheric flows, eliminating the need for external stabilizing elements like balloons or parachutes, allowing the sonde to freely migrate in atmospheric conditions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If traditional aerological sondes use GPS location information to determine storm intensity, then the device structure remains simple, but the measurement precision of storm intensity and wind speed is insufficient

Engineering Contradiction:
Improvemeasurement precision of storm intensityVSAvoiddevice complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent replaces the GPS-based location tracking system with a turbulence sensor system that directly measures atmospheric turbulence and sonde movement. The turbulence sensor detects turbulent kinetic energy and movement characteristics, providing direct mechanical measurement of storm intensity rather than inferring it from location data changes.

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

Solution Approach 2:

The patent changes the measurement parameter from GPS location coordinates to turbulence intensity and movement characteristics. By measuring the turbulent kinetic energy and movement of the sonde directly, the system obtains more accurate storm intensity data without relying on indirect location-based calculations.

Inventive Principle:
Principle #35Parameter changes

2Stability of the object's composition

If aerological sondes use external stabilizing elements like balloons or parachutes, then the stability of the sonde is improved, but the device complexity and additional weight increase

Engineering Contradiction:
Improvestability of the sondeVSAvoiddevice complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The patent removes external stabilizing elements such as balloons and parachutes from the sonde system. The sonde is designed to operate without these additional components, relying instead on its own turbulence sensing capabilities to measure atmospheric conditions during free migration.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The sonde performs self-stabilization and self-measurement by using its turbulence sensor to detect atmospheric conditions and its own movement characteristics. The system serves itself by measuring its migration pattern and turbulence exposure directly, eliminating the need for external stabilization apparatus.

Inventive Principle:
Principle #25Self-service

3Measurement precision

If aerological sondes rely on GPS location data for storm intensity measurement, then the loss of information is minimized, but the measurement precision of wind speed and turbulence remains insufficient

Engineering Contradiction:
Improvemeasurement precision of wind speedVSAvoidloss of turbulence information
Core Design Contradiction:
Measurement precisionVSLoss of information

Solution Approach 1:

The patent replaces GPS location-based wind speed calculation with direct turbulence sensing. The turbulence sensor measures turbulent kinetic energy and movement characteristics directly, providing accurate wind speed and turbulence data without relying on position changes over time.

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

Solution Approach 2:

The turbulence sensor acts as an intermediary between the sonde and the atmospheric turbulence. It directly detects turbulent kinetic energy and movement characteristics, serving as a mediator that captures turbulence information that would otherwise be lost in GPS-only systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Enables accurate measurement of turbulence and storm intensity by measuring the sonde's movement and orientation, providing detailed data for improved weather prediction and storm tracking.

Implementation Method 1

The turbulence sensor is arranged to measure turbulence in the cyclonic storm

Methodology Applied
Scientific EffectTurbulence: Turbulence

Implementation Method 2

The outer casing surface of the sonde casing is arranged to form drag surface of the aerological sonde such that a self-sustaining aerological sonde is formed

Methodology Applied
Scientific EffectDrag: Drag

Implementation Method 3

the turbulence sensor comprises a gyroscopic sensor arranged to measure orientation of the aerological sonde

Methodology Applied
Scientific EffectGyroscope: Gyroscope

Implementation Method 4

the turbulence sensor comprises an accelerometer arranged to measure change of rate of velocity of the aerological sonde

Methodology Applied
Scientific EffectAccelerometer: Accelerometer

Implementation Method 5

migrating the aerological sonde in the atmosphere by utilizing the drag surface of the aerological sonde

Methodology Applied
Scientific EffectDrag force: Drag

Data Source

PatentUS12411262B2Aerological sonde and method for measuring meteorological conditions
Publication Date: 2025.09.09 SKYFORA OY
  • US12411262B2 patent drawing
  • US12411262B2 patent drawing
  • US12411262B2 patent drawing

AI summary

An aerological sonde for measuring meteorological conditions in a cyclonic storm, the aerological sonde including a sonde casing having an outer casing surface and measurement unit arranged inside the sonde casing. The outer casing surface is arranged to form a sole drag surface of the aerological sonde such that a self-sustaining aerological sonde is formed. The measurement unit of the self-sustaining aerological sonde includes a turbulence sensor arranged to measure change of movement of the self-sustaining aerological sonde.