Auto-Lock Broadhead Cam Mechanism Prevents Premature Blade Deployment

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Solution Overview

Problem

Current mechanical broadheads suffer from reliability issues, including premature opening during flight, blade collapse on impact, and lack of a positive locking system, relying on unreliable mechanisms like rubber bands to maintain blade deployment.

Innovation Solution

The Auto-Lock broadhead features a self-locking mechanism with a locking notch, ferrule pin, and coil spring to ensure blades remain closed during launch and open upon impact, utilizing a cam action and spring tension to maintain locked positions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a rubber band is used to keep blades closed during launching, then the broadhead can maintain blade closure, but the reliability is poor and blades may open prematurely

Engineering Contradiction:
Improveblade closure reliabilityVSAvoidlocking mechanism complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The broadhead uses its own kinetic energy and structural geometry to lock and unlock blades automatically. The cam action converts forward motion into blade deployment, and the locking surfaces engage passively without requiring external power sources or complex actuating mechanisms.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The locking mechanism transitions from static (locked closed) to dynamic (blades opening) based on motion state. The cam profile is designed so that during forward acceleration, the blades remain locked, but upon impact deceleration, the cam releases and allows blade deployment.

Inventive Principle:
Principle #15Dynamics

2Reliability

If the blades are designed to open upon impact, then the wound channel is larger, but the blades may collapse on impact instead of staying deployed

Engineering Contradiction:
Improveblade deployment reliabilityVSAvoidblade structural stability
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The locking surfaces and cam profile are pre-configured to engage automatically when the broadhead experiences impact deceleration. The geometry is designed so that the locking surfaces are positioned to catch and hold the blades in the deployed position without requiring additional activation.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The blade assembly is segmented into movable blade components and a fixed ferrule body. This segmentation allows the blades to move independently for deployment while the ferrule provides structural support and houses the locking mechanism.

Inventive Principle:
Principle #1Segmentation

3Reliability

If a positive locking system is implemented, then the reliability increases, but the device complexity increases

Engineering Contradiction:
Improvelocking system reliabilityVSAvoidmechanical structure complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The cam profile acts as an intermediary element between the forward motion of the broadhead and the blade deployment action. It mediates the conversion of linear kinetic energy into rotational blade movement and subsequent locking engagement.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The design replaces complex multi-component mechanical locking systems with a simplified cam-based release mechanism. The cam profile geometry itself provides the locking and release functions, eliminating the need for separate springs, latches, or actuators.

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

4Speed

If the broadhead remains closed during launching, then the aerodynamic flight is maximized, but the blades may open prematurely causing erratic flight

Engineering Contradiction:
Improveaerodynamic flight performanceVSAvoidblade closure maintenance
Core Design Contradiction:
SpeedVSReliability

Solution Approach 1:

The locking mechanism is designed to preemptively counteract any forces that might cause premature blade opening during flight. The cam profile and locking surfaces are positioned to maintain positive engagement throughout the acceleration phase, preventing unintended deployment.

Inventive Principle:
Principle #9Preliminary anti-action

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 design significantly increases reliability by preventing premature opening during flight and ensuring blades remain fully deployed and locked in both closed and open positions, enhancing the performance and effectiveness of mechanical broadheads.

Implementation Method 1

incorporating a coil spring that keeps the intrinsically designed notches in the front of the blade forced forward, inside the ferrule, during launching

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

utilizing a cam action and spring tension to maintain locked positions

Methodology Applied
Scientific EffectCam mechanism: Cam

Implementation Method 3

including a blade with a locking notch that positively enables the blades to lock open; providing a ferrule pin for the blade notches to lock onto

Methodology Applied
Scientific EffectMechanical Fastening: Mechanical Fastener

Implementation Method 4

utilizing a cam action and spring tension to maintain locked positions

Methodology Applied
Scientific EffectSpring force: Spring

Data Source

PatentUS9857152B2Auto-lock broadhead
Publication Date: 2018.01.02 FRANCO SR ROGER DENNIS
  • US9857152B2 patent drawing
  • US9857152B2 patent drawing
  • US9857152B2 patent drawing

AI summary

An Auto-Lock Broadhead is disclosed having incorporated a unique, new, fail-safe, self-locking system to eliminate the possibility of blade failure, either upon launching, or upon impact. It is the only current design of its kind in existence.