Light Pipe Support Members for Rotorcraft Visibility and Stability
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Solution Overview
Problem
Radio controlled model rotorcrafts face challenges in user control, flight performance, structural stability, visibility, resistance to impact, and vibration, which existing technologies have not adequately addressed.
Innovation Solution
The implementation of light pipe support members and LED harnesses within the rotorcraft's design, which enhance visibility, structural stability, and resistance to impact by providing illumination and distributing light throughout the model, while also serving as structural components to support the rotor assemblies and improve flight performance.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If traditional support members are used in rotorcraft, then the structure is simple and easy to manufacture, but the rotorcraft has poor visibility and insufficient resistance to impact and vibration
Solution Approach 1:
The support members are designed to perform multiple functions simultaneously: they provide structural support for the rotor assemblies, serve as light pipes for illumination and visibility, and act as impact-resistant structural elements. This multi-functionality resolves the contradiction by integrating what would otherwise be separate components into a unified structure that improves reliability without proportionally increasing complexity.
Solution Approach 2:
The support members incorporate light-pipe material properties into traditional structural components, creating a composite functional structure. This allows the same component to provide both mechanical support and optical functions, thereby improving visibility and impact resistance while maintaining manufacturing feasibility through integrated design.
2Illumination intensity
If light pipe support members are implemented, then visibility and structural stability are improved, but the device complexity increases
Solution Approach 1:
The patent merges the support member structure with the light pipe function into a single integrated component. Instead of adding separate lighting systems to existing support members, the design combines these functions so that the support members themselves serve as light pipes, thereby improving visibility without the complexity of separate mounting systems.
Solution Approach 2:
The support members are designed as multi-functional components that simultaneously provide mechanical support and optical illumination functions. This universality allows a single component to fulfill multiple roles, improving visibility while avoiding the complexity of adding dedicated lighting systems.
3Stability of the object's composition
If integrated light pipe support members are used, then visibility and structural stability are enhanced, but manufacturing complexity increases
Solution Approach 1:
The support members are designed as discrete, replaceable components that can be manufactured separately and then assembled into the rotorcraft. This segmentation allows for specialized manufacturing of the light pipe material sections while maintaining the ability to produce them using standard techniques, thereby improving structural stability without excessively complicating the manufacturing process.
Solution Approach 2:
The invention changes the material parameters of the support members by incorporating light-pipe material properties. This parameter change enables the support members to transmit light effectively while maintaining their structural function, thereby improving visibility and structural stability through material selection rather than complex manufacturing processes.
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 solution improves user control and flight performance by increasing visibility and structural stability, making the rotorcraft easier to navigate, especially in low-light conditions, and enhances resistance to impact and vibration, leading to more stable and reliable flight operations.
Implementation Method 1
providing illumination and distributing light throughout the model
Data Source
AI summary
A radio controlled model rotorcraft implemented with features improving flight performance using increasing structural stability and increasing rotorcraft visibility and orientation awareness through the use of multifunctioning, configurable, and aesthetically pleasing components.