Flywheel Projectile Launcher for UAV Cattle Marking

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Solution Overview

Problem

Current methods for diagnosing and treating sick cattle in crowded feed lots are inefficient due to cattle's instinct to hide symptoms, making it difficult to quickly identify and separate infected animals.

Innovation Solution

An actuated projectile launcher system integrated with a UAV, featuring flywheel propulsion wheels that launch projectiles for marking or delivering payloads, allowing for efficient identification and separation of sick cattle by temporarily marking them for visual recognition.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Difficulty of detecting and measuring

If a UAV with a camera is used to observe cattle, then sick cattle can be identified from a distance, but the cattle will eventually become accustomed to the UAV and separate from the herd to display symptoms, reducing identification effectiveness

Engineering Contradiction:
Improvedifficulty of identifying sick cattleVSAvoidreliability of symptom display
Core Design Contradiction:
Difficulty of detecting and measuringVSReliability

Solution Approach 1:

The patent introduces an intermediary marking system (visual markers applied to cattle) that allows identification without requiring the cattle to display natural symptoms. The marker acts as a mediator between the observer and the cattle, enabling reliable identification even when cattle behavior changes in response to UAV presence

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The patent replaces the reliance on cattle's natural mechanical/behavioral response (symptom display) with an artificial marking system. Instead of observing natural behaviors that cattle can control, the system applies external markers that provide consistent visual identification regardless of cattle behavior

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

2Adaptability or versatility

If a projectile launcher is designed to launch various types of projectiles with different payloads, then the system becomes highly versatile, but the device complexity increases

Engineering Contradiction:
Improveversatility of projectile typesVSAvoidcomplexity of launcher system
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The patent designs a universal projectile launcher that can accommodate multiple projectile types and payloads through standardized interfaces. The system uses a common propulsion mechanism (flywheels) and launching structure that works with different projectile configurations, achieving multi-functionality without proportionally increasing complexity

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The patent employs dynamically adjustable support arms that can pivot and position themselves to accommodate different projectile types. The support arms can be adjusted during operation to match various projectile geometries and sizes, allowing the system to adapt to different payloads without requiring multiple specialized launchers

Inventive Principle:
Principle #15Dynamics

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

Enables rapid and effective identification and separation of sick cattle through temporary marking, facilitating early diagnosis and treatment, while the system's versatility in launching various projectiles and payloads enhances its utility.

Implementation Method 1

each of the two or more propulsion wheels is a flywheel configured to store rotational energy imparted by a motor and transfer that stored rotational energy to the projectile through direct engagement therewith

Methodology Applied
Scientific EffectRotational energy storage and transfer: Flywheel

Data Source

PatentUS12259210B1Actuated flywheel projectile launcher
Publication Date: 2025.03.25 NATIONAL TECHNOLOGY & ENGINEERING SOLUTIONS OF SANDIA LLC
  • US12259210B1 patent drawing
  • US12259210B1 patent drawing
  • US12259210B1 patent drawing

AI summary

Various embodiments include an actuated projectile launcher, including: a base structure; a projectile support, and a holding area from which a projectile launches; propulsion wheels selectively driven to rotate; and support arms, each supporting at a first end thereof a separate one of the propulsion wheels and being supported at an opposed second end thereof by the base structure. The support arms are configured to move the propulsion wheels between an expanded position and a contracted position, in which the propulsion wheels are closer to one another in the contracted position as compared to the expanded position. The movement of the propulsion wheels toward the contracted position brings the propulsion wheels into engagement with the projectile and drives the projectile from the holding area.