Translating Aperture Lightning Stroke Simulator for Aircraft Testing

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Evaluating and testing lightning swept strokes on aircraft surfaces is challenging due to the displacement and elongation of the plasma channel during a lightning strike, which is difficult to simulate effectively.

Innovation Solution

A simulator device comprising dielectric structures with elongate slits that overlap to form a translating aperture, coupled with an electrode and a voltage source, to simulate a lightning swept stroke by forming a plasma channel that elongates along a test structure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If a stationary electrode is used to simulate lightning strike, then the plasma channel forms between electrode and test structure, but the plasma channel cannot be elongated in the direction of aircraft motion to simulate swept stroke phenomenon

Engineering Contradiction:
Improveplasma channel shapeVSAvoiddevice complexity
Core Design Contradiction:
ShapeVSDevice complexity

Solution Approach 1:

The electrode is made movable along the test structure to dynamically create the elongated plasma channel shape. The electrode translates in the direction of aircraft motion, allowing the plasma channel to be stretched and swept along the test structure surface, accurately simulating the lightning swept stroke phenomenon while maintaining a relatively simple single-electrode design

Inventive Principle:
Principle #15Dynamics

2Speed

If high voltage is applied to form plasma channel at supersonic velocities, then the lightning swept stroke phenomenon is accurately simulated, but the voltage requirements become excessively high

Engineering Contradiction:
Improveaperture translation speedVSAvoidvoltage requirement
Core Design Contradiction:
SpeedVSUse of energy by moving object

Solution Approach 1:

The aperture is made dynamic by translating it along the test structure at controlled speeds. This dynamic translation allows the plasma channel to be elongated and swept in the direction of aircraft motion, accurately simulating supersonic lightning swept strokes. The controlled translation mechanism enables achievement of supersonic velocities without requiring excessively high voltages, as the motion itself contributes to the swept stroke effect

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The translating aperture acts as an intermediary between the electrode and test structure. By moving the aperture through which the plasma channel forms, the system can simulate the swept stroke phenomenon at reduced voltage levels compared to attempting to achieve the same effect through voltage alone. The aperture translation speed serves as a controllable parameter to achieve supersonic simulation velocities

Inventive Principle:
Principle #24Intermediary (Mediator)

Data Source

PatentUS20250369831A1Lightning swept stroke simulator devices and methods
Publication Date: 2025.12.04 THE BOEING CO
  • US20250369831A1 patent drawing
  • US20250369831A1 patent drawing
  • US20250369831A1 patent drawing

AI summary

Lightning swept stroke simulator devices comprise a first dielectric structure defining a first elongate slit, a second dielectric structure defining a second elongate slit, and an electrode positioned relative to the first dielectric structure and the second dielectric structure and configured to be operatively coupled to a voltage source. The first dielectric structure and the second dielectric structure are configured to be selectively moved relative to each other so that the first elongate slit and the second elongate slit overlap and collectively define an aperture that extends through the first dielectric structure and the second dielectric structure and that translates linearly along the first dielectric structure and the second dielectric structure.