Prow Radar Obstacle Simulator for Indoor Aircraft Testing

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Solution Overview

Problem

Current aircraft radar ground testing outdoors is challenging due to the need to simulate various weather and obstacle conditions, which are not consistently replicable and can lead to undetected issues until flight, requiring costly repairs and repeated tests.

Innovation Solution

A prow radar obstacle simulator system that uses a hood with RF absorbent material and signal processing means to simulate radar RF signals, allowing for indoor testing of aircraft radars by generating echo signals based on predefined patterns to mimic weather, obstacles, and targets, ensuring precise detection and reducing testing time and costs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If aircraft radar is tested outdoors to avoid RF safety hazards, then safety conditions are improved, but testing consistency and reliability deteriorate due to variable weather conditions

Engineering Contradiction:
ImproveRF safety hazardsVSAvoidtesting consistency
Core Design Contradiction:
Object-affected harmful factorsVSReliability

Solution Approach 1:

The patent introduces an RF absorbent hood as an intermediary structure that contains the radar system and provides a controlled testing environment. The hood absorbs RF emissions internally, allowing safe indoor testing while maintaining consistent testing conditions independent of external weather variables.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent uses signal processing means to generate synthetic echo signals that copy and simulate real radar returns from weather conditions, obstacles, and targets. This allows consistent reproduction of testing scenarios indoors without relying on actual external weather conditions.

Inventive Principle:
Principle #26Copying

2Ease of manufacture

If aircraft radar is tested outdoors with variable weather conditions, then testing setup simplicity is improved, but detection accuracy deteriorates due to inability to replicate specific weather patterns

Engineering Contradiction:
Improvetesting setup simplicityVSAvoiddetection accuracy
Core Design Contradiction:
Ease of manufactureVSMeasurement precision

Solution Approach 1:

The patent employs signal processing means that can dynamically change parameters of echo signals to simulate different weather conditions (rain, snow, fog, turbulence). This allows precise control of testing parameters to match specific detection scenarios while maintaining indoor testing simplicity.

Inventive Principle:
Principle #35Parameter changes

3Device complexity

If aircraft radar testing is performed outdoors, then equipment complexity is reduced, but testing time increases due to need for repeated flight tests

Engineering Contradiction:
Improveequipment complexityVSAvoidtesting time
Core Design Contradiction:
Device complexityVSLoss of time

Solution Approach 1:

The patent implements comprehensive ground-based testing using the hood system that simulates all necessary operating conditions before flight. This preliminary action identifies and resolves issues during ground testing, eliminating the need for repeated flight tests and significantly reducing total testing time.

Inventive Principle:
Principle #10Preliminary action

4Reliability

If aircraft radar is tested indoors with RF absorbent hood, then testing consistency is improved, but device complexity increases due to additional hood and signal processing equipment

Engineering Contradiction:
Improvetesting consistencyVSAvoidequipment complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent combines the RF absorbent hood, multiple antennas, signal processing means, and control unit into an integrated testing system. This merging of components into a unified indoor testing platform achieves consistent and reliable radar testing while managing complexity through systematic integration.

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

Enables safe and efficient indoor testing of aircraft radars, reducing testing time by 95% and allowing for immediate identification and repair of issues without the need for outdoor testing, ensuring radar functionality before flight.

Implementation Method 1

a hood comprising a plurality of antennas configured to receive radar radio frequency (RF) signals from an aircraft radar, the hood being made of a RF absorbent material

Methodology Applied
Scientific EffectRF absorption: Absorption (EM radiation)

Implementation Method 2

a signal processing means for processing the radar RF signals received by the plurality of antennas, the signal processing means being in data communication with the plurality of antennas and comprising first converting means for converting radar RF signals to an intermediate frequency (IF) signal and vice versa

Methodology Applied
Scientific EffectFrequency conversion:

Implementation Method 3

at least one antenna of the plurality of antennas is also configured to emit the generated echo signal to the aircraft radar

Methodology Applied
Scientific EffectElectromagnetic radiation:

Data Source

PatentEP3798666A1Prow radar obstacle simulator for testing on an aircraft and a method thereof
Publication Date: 2021.03.31 AIRBUS DEFENCE & SPACE SAU
  • EP3798666A1 patent drawingFigure 1
  • EP3798666A1 patent drawingFigure 2
  • EP3798666A1 patent drawingFigure 3~6

AI summary

The present invention provides a prow radar obstacle simulator system for testing on an aircraft, the system comprising: a hood comprising a plurality of antennas configured to receive radio frequency (RF) signals from an aircraft radar, the hood being made of a RF absorbent material; a signal processing means for processing the radar RF signals received by the plurality of antennas, the signal processing means being in data communication with the plurality of antennas and comprising first converting means for converting radar RF signals to an intermediate frequency (IF) signal and vice versa; and a control unit in data communication with the signal processing means and configured to process the IF signals for generating an echo signal based on at least one predefined echo pattern; wherein at least one antenna of the plurality of antennas is also configured to emit the generated echo signal to the aircraft radar.