Runway Identification via Weather Radar Corner Reflectors

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Solution Overview

Problem

Current runway identification systems for aircraft are not automated, require additional equipment, and are inefficient, especially in low visibility conditions, necessitating a rapid and cost-effective solution that utilizes existing aircraft sensors.

Innovation Solution

A runway identification system that employs a weather radar system to process radar returns from corner reflectors placed near the runway ends, determining the runway identification by analyzing the reflected electromagnetic code, thereby providing automated and rapid identification without additional aircraft equipment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Extent of automation

If pilots visually determine runway alignment during approach, then runway identification can be achieved, but the system is not automated and is inefficient in low visibility conditions

Engineering Contradiction:
Improverunway identification automationVSAvoidrunway identification reliability in low visibility
Core Design Contradiction:
Extent of automationVSReliability

Solution Approach 1:

The patent replaces the mechanical/visual determination method with an automated electronic system. The weather radar system transmits electromagnetic signals and processes radar returns to automatically identify the runway, eliminating the need for visual determination and providing automated identification even in low visibility conditions.

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

Solution Approach 2:

The patent introduces corner reflectors as intermediary objects placed on the runway. These reflectors serve as mediators between the weather radar system and the runway, providing distinct radar return signatures that enable automated identification. The reflectors are positioned at specific locations (threshold and far end) to create identifiable radar patterns.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Extent of automation

If additional equipment is installed for runway identification, then automated identification capability is achieved, but system cost increases

Engineering Contradiction:
Improverunway identification automationVSAvoidaircraft equipment complexity
Core Design Contradiction:
Extent of automationVSDevice complexity

Solution Approach 1:

The patent makes the weather radar system multi-functional by enabling it to perform both its traditional weather detection function and runway identification function. The same radar transmitter, receiver, and processing equipment are used for both purposes, eliminating the need for separate dedicated runway identification equipment and reducing overall system complexity.

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

3Speed

If rapid runway identification is implemented, then pilot safety is improved, but system complexity increases

Engineering Contradiction:
Improverunway identification speedVSAvoididentification system complexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The patent implements preliminary action by pre-positioning corner reflectors at specific locations on the runway (threshold and far end) before the aircraft arrives. These reflectors are permanently installed and configured to provide identifiable radar signatures. When the aircraft approaches, the radar system can immediately detect and process these pre-positioned reflectors for rapid identification without requiring complex real-time analysis or moving components.

Inventive Principle:
Principle #10Preliminary action

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 rapid and automated runway identification during approach, even in low visibility conditions, using existing weather radar systems, ensuring pilot safety and reducing costs by leveraging existing aircraft sensors.

Implementation Method 1

a weather radar system configured to transmit a radar beam and receive a radar return

Methodology Applied
Scientific EffectRadar: Radar

Implementation Method 2

a set of runway corner reflectors configured to reflect the radar beam from an aircraft

Methodology Applied
Scientific EffectReflection: Reflection

Implementation Method 3

receiving electromagnetic returns from a beam directed toward the set corner reflectors

Methodology Applied
Scientific EffectElectromagnetic radiation:

Data Source

PatentUS8576113B1Runway identification system and method
Publication Date: 2013.11.05 ROCKWELL COLLINS INC
  • US8576113B1 patent drawing
  • US8576113B1 patent drawing
  • US8576113B1 patent drawing

AI summary

A runway identification system and method utilizes a set of (reflectors or sources). The reflectors or sources can be located in proximity to the end of runway. The method receives electromagnetic energy from the reflectors or sources. A runway identification is determined from the electromagnetic energy. The runway identification can be displayed on a display in the aircraft. The reflectors can be corner reflectors, laser reflectors or other reflective optics.