Rotational Launch Mechanism for Flying Structures

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Solution Overview

Problem

Existing flying structures face challenges in efficiently initiating flight, particularly in achieving sufficient lift and altitude due to limitations in rotational movement and launch mechanisms.

Innovation Solution

A rotational arrangement is coupled with the flying structure, allowing users to impart rotational movement and automatically varying the radius of rotation, which includes a user-employable trigger and a pliable or elastic effective member that extends between the user and the flying structure, enabling controlled launch and flight.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a rotational arrangement with automatically varying radius is used to initiate flight, then the ability to achieve lift and altitude is improved, but the device complexity increases

Engineering Contradiction:
Improveability to achieve lift and altitudeVSAvoidcomplexity of rotational arrangement
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The rotational arrangement employs a pliable or elastic effective member that automatically varies the radius of rotation during the launching motion. This dynamic adjustment allows the system to optimize lift generation at different stages of rotation without requiring complex mechanical control mechanisms, thereby improving flight initiation reliability while keeping the device relatively simple.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes the physical parameter of the effective member (from rigid to pliable/elastic) to enable automatic radius variation. This material-based parameter change allows the radius to dynamically adjust during rotation, improving the flying structure's ability to achieve lift and altitude without adding complex control systems.

Inventive Principle:
Principle #35Parameter changes

2Productivity

If the radius of rotation is automatically varied during launch, then flight initiation efficiency is improved, but the ease of operation decreases

Engineering Contradiction:
Improveflight initiation efficiencyVSAvoidease of imparting rotational movement
Core Design Contradiction:
ProductivityVSEase of operation

Solution Approach 1:

The pliable or elastic effective member serves itself by automatically varying the radius of rotation in response to the launching motion. The material's inherent elasticity enables the system to self-adjust without requiring user intervention or complex control mechanisms, thereby improving flight initiation efficiency while maintaining relatively simple operation.

Inventive Principle:
Principle #25Self-service

3Ease of operation

If a pliable or elastic effective member is used to extend between user and flying structure, then controlled launch is achieved, but the device complexity increases

Engineering Contradiction:
Improvecontrolled launch capabilityVSAvoidcomplexity of effective member system
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The system changes the physical parameter of the effective member from rigid to pliable/elastic, which provides inherent control capabilities through the material's elastic properties. This allows the effective member to extend and retract smoothly during launch, providing controlled launch capability without requiring additional control mechanisms or increasing overall device complexity.

Inventive Principle:
Principle #35Parameter changes

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 solution enhances the flying structure's ability to achieve lift and altitude by optimizing the radius of rotation, allowing for more efficient and controlled flight initiation and navigation.

Implementation Method 1

a pliable or elastic effective member that extends between the user and the flying structure

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentUS8146857B2Initiating flight of a flying structure
Publication Date: 2012.04.03 FREESTYLE ENG
  • US8146857B2 patent drawing
  • US8146857B2 patent drawing
  • US8146857B2 patent drawing

AI summary

In example embodiments described herein, techniques are described for launching flying structures such as a plank wings or a gliders, canards, or any other flying structures. In some example embodiments, a rotational arrangement facilitates such launches. In operation, a rotational arrangement couples with the flying structure and is configured to allow a user to impart rotational movement to the flying structure. In imparting the rotational movement, the rotational mechanism allows an automatic variation of a radius of the associated radius of curvature.