High-Altitude Balloon Altitude Control System

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

High-altitude balloons used for weather prediction and communications tend to drift due to cross winds, limiting their mission duration within a designated geographic region.

Innovation Solution

A system and method that includes a high-altitude balloon with a control system to determine and adjust its altitude based on environmental parameters, maximizing the time it remains within a specific geographic area by compensating for wind velocity and direction changes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If the balloon is launched to a fixed initial mission optimum altitude, then the balloon can reach a high altitude quickly, but the balloon drifts out of the designated geographic region due to cross winds

Engineering Contradiction:
Improveascend speedVSAvoidmission duration
Core Design Contradiction:
SpeedVSDuration of action of moving object

Solution Approach 1:

The patent implements dynamic altitude adjustment by continuously monitoring wind conditions and modifying the balloon's altitude in real-time. The control system adjusts the balloon's vertical position to exploit vertical wind shear, changing the balloon's characteristics from static to dynamic to counteract cross-wind drift and extend mission duration within the designated geographic region.

Inventive Principle:
Principle #15Dynamics

2Device complexity

If the balloon remains at a constant altitude, then the control system is simple, but the balloon cannot compensate for wind velocity and direction changes

Engineering Contradiction:
Improvecontrol system complexityVSAvoidposition maintaining capability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The patent employs a feedback control system that continuously monitors wind velocity and direction, balloon position, and altitude. This feedback information is processed to generate control commands that adjust the balloon's altitude, creating a closed-loop system that maintains reliable position within the designated region while adapting to changing wind conditions.

Inventive Principle:
Principle #23Feedback

3Duration of action of moving object

If the balloon descends to counteract cross winds, then the balloon can remain in the geographic region longer, but the mission life is limited by the balloon's maximum altitude capability

Engineering Contradiction:
Improvetime within geographic regionVSAvoidgas temperature
Core Design Contradiction:
Duration of action of moving objectVSTemperature

Solution Approach 1:

The patent utilizes parameter changes by modifying the balloon's altitude parameter in response to wind conditions. By changing altitude rather than relying solely on temperature adjustments or payload weight changes, the system exploits the vertical dimension to counteract cross-wind drift, thereby extending the time the balloon remains within the designated geographic region.

Inventive Principle:
Principle #35Parameter changes

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 effectively extends the mission duration of high-altitude balloons by optimizing their altitude to counteract wind effects, ensuring they remain within the designated region for longer periods.

Implementation Method 1

Balloons are filled with a highly buoyant gas (e.g., helium) that allows the balloon to ascend to a maximum altitude

Methodology Applied
Scientific EffectBuoyancy: Archimedes' Principle (Buoyancy)

Data Source

PatentUS10359784B2Balloon maneuvering/positioning system
Publication Date: 2019.07.23 NORTHROP GRUMMAN SYSTEMS CORP
  • US10359784B2 patent drawing
  • US10359784B2 patent drawing
  • US10359784B2 patent drawing

AI summary

An aviation system is disclosed that has the capabilities to position a high-altitude aviation vehicle within a designated geographic region for extended periods of time or maneuver the high-altitude aviation vehicle along predetermined designated paths.