Combined Aircraft Take-off and Tower Signal Light Unit

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Solution Overview

Problem

Modern aircraft exterior lighting systems are complex due to the variety of light units required for different functionalities, necessitating a solution that enhances functionality without increasing complexity.

Innovation Solution

A combined aircraft take-off and tower signal light unit with a single light source and mounting configuration that generates a take-off light output and two tower signal light outputs, allowing independent optimization of each, with the tower signal light output oriented to minimize glare and ensure visibility to air traffic control personnel.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single combined light unit is used for both take-off and tower signal functions, then device complexity is reduced, but it becomes difficult to independently optimize each light output's characteristics

Engineering Contradiction:
Improvelighting system complexityVSAvoidindependent optimization capability
Core Design Contradiction:
Device complexityVSAdaptability or versatility

Solution Approach 1:

The patent divides the lighting system into distinct functional segments: a take-off light unit with its own optical system for forward illumination, and a tower signal light unit with its own optical system for angled signaling. Each segment can be independently optimized for its specific function while being integrated into a single combined mounting structure, thus reducing overall device complexity while maintaining independent optimization capability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The combined light unit employs a universal mounting structure and control system that serves multiple functions: it can independently generate take-off light output for pilot illumination and tower signal light output for air traffic control communication. The single combined unit replaces what would traditionally require separate light units, achieving multi-functionality without proportionally increasing complexity.

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

2Illumination intensity

If take-off light intensity is increased to improve visibility, then illumination effectiveness is improved, but pilot glare risk increases

Engineering Contradiction:
Improvetake-off light visibilityVSAvoidpilot glare
Core Design Contradiction:
Illumination intensityVSObject-affected harmful factors

Solution Approach 1:

The take-off light unit incorporates an optical system with asymmetric beam distribution that concentrates high intensity light in the forward horizontal direction where illumination is needed for take-off roll visibility, while deliberately reducing intensity in upward and lateral directions where it would cause pilot glare. This local quality variation optimizes illumination effectiveness while minimizing harmful effects.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent converts the potential harmful effect of high-intensity light into a beneficial directional illumination pattern. By using an optical system that shapes the beam, the high intensity is redirected forward to illuminate the runway and taxiway during take-off, while the areas that would normally receive excessive light (above and to the sides of the pilot's view) are intentionally darkened, thus converting what could be glare into useful forward illumination.

Inventive Principle:
Principle #22Blessing in disguise (Convert harm into benefit)

3Measurement precision

If tower signal light is oriented to maximize visibility to tower personnel, then signal recognition is improved, but stray light and potential pilot interference increase

Engineering Contradiction:
Improvesignal recognition accuracyVSAvoidstray light
Core Design Contradiction:
Measurement precisionVSObject-generated harmful factors

Solution Approach 1:

The tower signal light unit employs an asymmetric optical design with two light sources positioned at different angles relative to the aircraft's longitudinal axis. This asymmetric arrangement creates two distinct beam patterns that are oriented specifically toward typical tower locations, maximizing signal recognition accuracy for air traffic control personnel while the asymmetric geometry naturally confines the light paths to avoid the pilot's forward view and reduce stray light interference.

Inventive Principle:
Principle #4Asymmetry

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

This configuration increases the efficiency of take-off lighting while reducing the risk of pilot glare and ensures reliable signaling to tower personnel, optimizing both light outputs for improved recognition and reduced complexity.

Implementation Method 1

an LED group with a plurality of LEDs

Methodology Applied
Scientific EffectLight emission from LED: Light Emitting Diode

Data Source

PatentEP3403936B1Combined aircraft take-off and tower signal light unit and aircraft comprising the same
Publication Date: 2021.07.14 GOODRICH LIGHTING SYST GMBH
  • EP3403936B1 patent drawingFigure 1
  • EP3403936B1 patent drawingFigure 2
  • EP3403936B1 patent drawingFigure 3a~3b

AI summary

A combined aircraft take-off and tower signal light unit (2) comprises a mounting portion (7) for mounting the combined aircraft take-off and tower signal light unit (2) to an aircraft (30), in particular to a front running gear (36) of the aircraft (30), wherein the mounting portion (7) is configured for orienting a horizontal cross-sectional plane (H) of the combined aircraft take-off and tower signal light unit (2) substantially horizontally with respect to the aircraft (30); and at least one light source (10a, 10b, 10c). The combined aircraft take-off and tower signal light unit (2) has a take-off light output (40), which is centered on a take-off light emission axis (A) and which has a take-off light peak intensity, and a tower signal light output (42), which is centered on a tower light emission axis (B) and which has a tower light peak intensity. The tower light emission axis (B) is oriented at an angle of between 10° to 30°, in particular at an angle of between 15° and 25°, with respect to the take-off light emission axis (A), when projected onto the horizontal cross-sectional plane (H), and the tower light peak intensity is smaller than the take-off light peak intensity.