Aircraft Lamp Control Substrate Shielding and Maintenance

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Solution Overview

Problem

Aircraft lamps face challenges in maintaining a good driving state of light sources due to noise interference and require improved maintainability of control substrates, particularly in scenarios where control substrate issues arise.

Innovation Solution

The aircraft lamp design incorporates a shielding plate to enclose and shield the control substrate within a unit accommodation portion, allowing for easy exchange and noise reduction, while using a heat-dissipating attaching plate to manage heat generated by electronic components, and employing multiple light source units with distinct control substrates and lenses to optimize light irradiation directions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If the control substrate is integrated into the lamp housing, then the structure is more compact, but the maintainability and ease of replacement deteriorate

Engineering Contradiction:
Improvestructural integrationVSAvoidcontrol substrate replacement
Core Design Contradiction:
Device complexityVSEase of repair

Solution Approach 1:

The control substrate is separated from the lamp housing and placed in a dedicated control substrate accommodation portion, allowing independent access and replacement without disassembling the entire lamp structure. This segmentation enables easy maintenance while keeping the overall structure integrated.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The control substrate accommodation portion is pre-configured with insertion/removal ports and positioning structures during manufacturing. This preliminary preparation allows the control substrate to be quickly installed or replaced without requiring complex assembly procedures or specialized tools.

Inventive Principle:
Principle #10Preliminary action

2Temperature

If the control substrate is exposed, then the heat dissipation is improved, but the noise interference to instruments deteriorates

Engineering Contradiction:
Improveheat dissipationVSAvoidnoise interference
Core Design Contradiction:
TemperatureVSObject-affected harmful factors

Solution Approach 1:

A shielding plate is introduced as an intermediary element between the control substrate and the instrument space. The shielding plate has a heat-dissipating structure that allows thermal energy to pass through while blocking electromagnetic noise, thus mediating between heat dissipation requirements and noise interference prevention.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The shielding plate is designed with different local properties: it has heat-dissipating structures (such as heat sinks or thermal conduits) in areas facing the control substrate, while maintaining electromagnetic shielding properties in areas facing the instrument space. This local differentiation allows simultaneous achievement of heat dissipation and noise protection.

Inventive Principle:
Principle #3Local quality

3Ease of manufacture

If the insertion/removal port is left open, then the assembly is simpler, but the noise shielding effectiveness deteriorates

Engineering Contradiction:
Improveassembly simplicityVSAvoidnoise shielding
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The shielding plate is merged with the control substrate accommodation portion, forming an integrated noise barrier that is built into the housing structure. This merging provides effective noise shielding without requiring separate, complex assembly steps or additional components.

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

This configuration ensures a stable operation of aircraft instruments, enhances maintainability by simplifying control substrate replacement, and provides efficient and flexible lighting options for various aircraft configurations.

Implementation Method 1

a shielding plate that shields noise generated in the control substrate

Methodology Applied
Scientific EffectElectromagnetic shielding: Faraday Cage

Implementation Method 2

employing multiple light source units with distinct control substrates and lenses to optimize light irradiation directions

Methodology Applied
Scientific EffectThermal conduction: Conduction (thermal)

Data Source

PatentUS11739912B2Aircraft lamp
Publication Date: 2023.08.29 KOITO MFG CO LTD
  • US11739912B2 patent drawing
  • US11739912B2 patent drawing
  • US11739912B2 patent drawing

AI summary

An aircraft lamp includes: a lamp outer housing configured by a lamp housing having an opening and a cover attached to the lamp housing in a state where the opening is closed, wherein an internal space is formed as an arrangement space; a light source unit arranged in the arrangement space and having a light source; and a control unit including a control substrate that controls an ON/OFF of the light source, and a shielding plate that shields noise generated in the control substrate. The lamp housing is provided with a unit accommodation portion having a concave shape and an insertion/removal port. The control substrate is configured to be accommodated in and removed from the unit accommodation portion via the insertion/removal port. At least a part of the insertion/removal port is closed by the shielding plate in a state where the control substrate is accommodated in the unit accommodation portion.