Shuttlecock Launching Mechanism for Trajectory Accuracy

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Solution Overview

Problem

Existing shuttlecock launching machines experience a significant change in trajectory and loss of velocity due to air pressure, resulting in reduced accuracy and efficiency in launching shuttlecocks.

Innovation Solution

A shuttlecock launching machine that uses rotating finger-like projections and coordinating levers to orient shuttlecocks parallel to the ejecting wheels, ensuring consistent trajectory and minimizing orientation changes at ejection, thus maintaining velocity and accuracy.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If the shuttlecock is launched using conventional spinning wheels or chutes, then the shuttlecock can be propelled forward, but the trajectory changes significantly and velocity is lost due to air pressure

Engineering Contradiction:
Improveshuttlecock velocityVSAvoidvelocity loss due to air pressure
Core Design Contradiction:
SpeedVSLoss of energy

Solution Approach 1:

The shuttlecock is pre-oriented in a vertical position within the loading mechanism before ejection. The rotating finger-like projections and coordinating levers prepare the shuttlecock by aligning it parallel to the wheel plane in advance, ensuring optimal orientation at the moment of ejection to minimize air resistance and velocity loss

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The invention changes the orientation parameter of the shuttlecock from vertical (in storage) to parallel with the wheel plane (at ejection). The pitch of the wheel plane about the wheel horizontal axis is selectively indexed, allowing adjustment of the ejection angle while maintaining the shuttlecock's optimal orientation relative to the trajectory, thereby reducing air pressure effects

Inventive Principle:
Principle #35Parameter changes

2Adaptability or versatility

If the shuttlecock orientation changes significantly prior to ejection, then the launching mechanism can accommodate different trajectories, but the velocity is lost and trajectory accuracy is reduced

Engineering Contradiction:
Improvetrajectory rangeVSAvoidtrajectory accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The invention employs dynamic coordination between the rotating finger-like projections and the levers to maintain the shuttlecock's orientation parallel to the wheel plane throughout the ejection process. The system adapts to different trajectories by indexing the pitch of the wheel plane while keeping the shuttlecock's relative orientation constant, ensuring both versatility and precision

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The invention replaces the conventional mechanical launching system (spinning wheels or simple chutes) with a coordinated mechanism of rotating fingers and levers. This new mechanical system provides precise control over the shuttlecock's orientation and ejection angle, enabling accurate trajectory control without significant orientation changes that would cause velocity loss

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 machine achieves accurate and efficient shuttlecock launch with reduced velocity loss and improved trajectory consistency by ensuring the shuttlecock is ejected in an orientation parallel to the wheel plane, maintaining intended trajectory and accuracy.

Implementation Method 1

A shuttlecock launching machine that uses rotating finger-like projections and coordinating levers to orient shuttlecocks parallel to the ejecting wheels

Methodology Applied
Scientific EffectMechanical orientation:

Implementation Method 2

the shuttlecock is ejected in an orientation parallel to the surface plane of the wheels, said orientation causing the shuttlecock to be accelerated by the wheels

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentUS10124231B1Shuttlecock launching apparatus
Publication Date: 2018.11.13 SKLAR ALLAN
  • US10124231B1 patent drawing
  • US10124231B1 patent drawing
  • US10124231B1 patent drawing

AI summary

A shuttlecock loading mechanism with a grabbing mechanism and a pair of ejecting wheels defining a wheel plane. The grabbing mechanism receives a shuttlecock entering the loading mechanism in a vertical position and ejects the shuttlecock from the loading mechanism in an orientation parallel to the wheel plane wherein the pitch of the wheel plane about a wheel horizontal axis is selectively indexed about the wheel's horizontal axis.