Aircraft Headlight Parabolic Reflector Stray Light Management

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Solution Overview

Problem

Aircraft headlight systems face issues with stray light generation due to the close packing of parabolic reflectors, leading to deviations from the parabolic shape at reflector contact sections, which results in undesired light distribution and potential blinding of pilots by reflected stray light.

Innovation Solution

The design incorporates a combination of parabolic and non-parabolic reflector contact sections in adjacent lighting arrangements, allowing for dense packing while minimizing stray light emission by adjusting the geometry of non-parabolic sections to direct stray light away from undesirable directions, such as the upper hemisphere.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Area of stationary object

If lighting arrangements are arranged very closely to use available space efficiently, then space utilization is improved, but stray light is generated due to reflector shape deviations at contact sections

Engineering Contradiction:
Improvespace utilizationVSAvoidstray light
Core Design Contradiction:
Area of stationary objectVSObject-generated harmful factors

Solution Approach 1:

The reflector is designed with different surface properties in different regions: the contact section has a modified geometry (planar or convex) to prevent stray light generation, while the non-contact sections maintain the parabolic shape for optimal light collimation. This local differentiation allows the reflector to simultaneously achieve dense packing without stray light and maintain lighting performance.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The reflector surface is segmented into functionally distinct zones: contact sections where reflectors meet adjacent units and non-contact sections. Each segment serves its specific purpose - contact sections are optimized for preventing stray light while non-contact sections maintain collimation performance, allowing the overall system to achieve both dense packing and reduced stray light.

Inventive Principle:
Principle #1Segmentation

2Area of stationary object

If reflector contact sections are made non-parabolic to accommodate adjacent reflectors, then dense packing is achieved, but light collimation performance deteriorates

Engineering Contradiction:
Improvepacking densityVSAvoidlight collimation
Core Design Contradiction:
Area of stationary objectVSIllumination intensity

Solution Approach 1:

The reflector design applies different geometric qualities to different regions: contact sections use planar or convex surfaces to enable dense packing, while non-contact sections maintain the parabolic shape for optimal light collimation. This local differentiation ensures that the compromise in shape is confined only to necessary contact areas.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The potential harm of having to modify reflector shapes for packing is converted into a benefit by strategically placing the modifications only in contact sections. The non-contact sections retain full parabolic performance, and the contact section modifications actually help define precise boundaries between adjacent reflectors, improving overall system organization.

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

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 effectively reduces stray light in undesirable directions, enhancing pilot visibility and aircraft safety by minimizing reflections from clouds or fog while maintaining a dense and efficient lighting arrangement.

Implementation Method 1

Aircraft head lights, as they are employed in airplanes and helicopters, may comprise a plurality of lighting arrangements, each of said lighting arrangements comprising a reflector, in particular a reflector having a parabolic shape. With the parabolic reflectors, a strong collimation of light is achieved for providing a bright illumination in a desired direction.

Methodology Applied
Scientific EffectLight collimation by parabolic reflector: Reflection

Implementation Method 2

the reflector contact section of the generally parabolic reflector of the second lighting arrangement is non-parabolic... The non-parabolic reflector contact section is a portion of the generally parabolic reflector that is modified as compared to a fully parabolic reflector... to direct stray light away from undesirable directions

Methodology Applied
Scientific EffectLight reflection and redirection: Reflection

Data Source

PatentUS10518899B2Aircraft head light
Publication Date: 2019.12.31 GOODRICH LIGHTING SYST GMBH
  • US10518899B2 patent drawing
  • US10518899B2 patent drawing
  • US10518899B2 patent drawing

AI summary

An aircraft head light comprises: a plurality of lighting arrangements, each lighting arrangement comprising a light source and a generally parabolic reflector surrounding the respective light source. The plurality of lighting arrangements are arranged in a side-by-side relationship, with the generally parabolic reflectors of adjacent lighting arrangements having respective reflector contact sections. For at least one adjacent pair of the plurality of lighting arrangements, said adjacent pair comprising a first lighting arrangement and a second lighting arrangement the reflector contact section of the generally parabolic reflector of the first lighting arrangement is parabolic and the reflector contact section of the generally parabolic reflector of the second lighting arrangement is non-parabolic.