Aircraft Anti-Collision Light With Reflective Modules
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Solution Overview
Problem
Existing anti-collision light systems for aircraft do not fully comply with the optical coverage and intensity requirements specified in FAR25-CS25/FAR23-CS23, particularly in terms of angular coverage and intensity distribution, and lack efficient infrared illumination for covert flight modes.
Innovation Solution
The anti-collision light system consists of three axially symmetric modules with LEDs and reflectors, providing visible illumination that meets the angular coverage requirements and includes an optional infrared module for covert operations, utilizing high-power aviation-colored LEDs and near-infrared LEDs with specific reflector designs to ensure compliance with regulatory standards.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Illumination intensity
If conventional anti-collision light systems are used, then basic illumination is provided, but they do not fully comply with optical coverage and intensity requirements specified in FAR25-CS25/FAR23-CS23
Solution Approach 1:
The patent applies parameter changes by carefully selecting LED characteristics (color temperature, wavelength, luminous intensity) and reflector geometries to achieve the specific optical intensity distribution required by FAR25-CS25/FAR23-CS23 regulations. The system adjusts parameters such as LED power output and reflector surface angles to meet the minimum candela values at different angles while maintaining compliance reliability.
2Adaptability or versatility
If conventional anti-collision light systems are used, then basic illumination is provided, but they lack efficient infrared illumination for covert flight modes
Solution Approach 1:
The patent implements multi-functionality by integrating both visible light LEDs and infrared LEDs into a single anti-collision light system. The visible LEDs provide standard anti-collision illumination, while the infrared LEDs enable covert flight modes where the aircraft remains invisible to the human eye. This universal design allows the same physical structure to serve multiple operational purposes without requiring separate systems.
Solution Approach 2:
The patent utilizes color changes by employing LEDs that emit different wavelengths - visible spectrum light for normal operation and infrared radiation for covert modes. The system can switch between these electromagnetic spectrum regions, effectively changing the 'color' or wavelength of emitted radiation to adapt to different flight requirements while managing power consumption through selective activation.
3Illumination intensity
If multiple LEDs are used to achieve required illumination, then optical coverage is improved, but device complexity increases
Solution Approach 1:
The patent applies segmentation by dividing the anti-collision light system into three axially symmetric modules, each containing a specific number of LEDs (e.g., 7 LEDs per module in one embodiment). This modular segmentation allows the system to achieve the required angular coverage and intensity distribution while maintaining manageable complexity through standardized, repeatable units that can be independently designed and assembled.
Solution Approach 2:
The patent combines multiple LEDs within each axially symmetric module and integrates all modules with a common reflector structure to achieve the required optical coverage. By merging the functionality of multiple LEDs and modules into a unified system with shared optical components, the patent reduces overall device complexity while maintaining the necessary illumination performance across all angular requirements.
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 achieves enhanced visibility and compliance with regulatory standards by providing high-intensity illumination within specified angles and efficient infrared emission for covert flight modes, while ensuring safety and visibility requirements are met, and includes monitoring and feedback mechanisms for LED efficiency and failure detection.
Implementation Method 1
a first reflector (15) with parabolic section and cylindrical symmetry around axis (9) having a first smaller end portion (15a) with radius r1 (r1< r) and a second larger end portion (15b) (having radius close to radius R) spaced from board (10)—the reflector (15) faces LEDs (12)
Data Source
AI summary
An anti-collision light for aircraft comprising two illuminating modules each comprising a number of LEDs disposed along a ring and coplanar to a plane, a first reflector facing the LEDS and a second reflector surrounding the LEDS; the first and the second reflector are so configured as to reflect the light emitted by LEDs toward angles between 0 and 75° above or below said plane. An additional module providing infra-red radiation is may be provided; the additional module comprising number of infra red LEDs disposed along a ring and coplanar to a plane and a reflector facing the infra red LEDs.


