Spring-Loaded Broadhead Blade Deployment Mechanism

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Solution Overview

Problem

Existing expandable broadheads in archery hunting equipment face mechanical failures, leading to inconsistent deployment upon impact and reduced reusability.

Innovation Solution

A broadhead design featuring a spring-loaded retaining member, a pin, and a blade member that transitions from a retracted to a fully deployed position upon impact, with retaining features to prevent accidental deployment during flight and facilitate easy reset and reuse.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If a spring-loaded retaining member is used to hold the blade member in a retracted position, then flight stability is improved, but device complexity increases

Engineering Contradiction:
Improveflight stabilityVSAvoiddevice complexity
Core Design Contradiction:
Stability of the object's compositionVSDevice complexity

Solution Approach 1:

The blade member transitions from a static fixed position to a dynamic retracted/deployed position system. The spring-loaded retaining member creates a dynamic locking mechanism that automatically engages during flight to stabilize the blade in a retracted position, and automatically deploys upon target impact. This dynamic behavior resolves the contradiction by providing flight stability through controlled movement rather than fixed structure.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The spring-loaded retaining member with pin and notch mechanism provides self-regulating functionality. The spring automatically maintains the blade in the retracted position during flight without external control, and automatically triggers deployment upon impact. The system serves itself by using the impact force to compress the spring and release the blade, eliminating the need for external actuators or complex control systems.

Inventive Principle:
Principle #25Self-service

2Reliability

If the blade member is designed to automatically deploy upon impact, then reliability is improved, but device complexity increases

Engineering Contradiction:
Improvereliable expansionVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The spring is pre-loaded in a compressed state within the retaining member, storing elastic potential energy that is ready to be released. This preliminary action ensures that when impact occurs, the blade member immediately receives the stored energy to drive deployment, guaranteeing reliable expansion without requiring complex sensing or actuation systems.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The pin acts as an intermediary element between the spring-loaded retaining member and the blade member. During normal flight, the pin engages with the notch to hold the blade in the retracted position. Upon impact, the pin serves as a transfer mechanism that allows the spring force to be transmitted to the blade, facilitating automatic deployment. This simple intermediary mechanism achieves reliable automatic deployment without complex systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Productivity

If the broadhead is designed for easy reset and reuse, then productivity is improved, but device complexity increases

Engineering Contradiction:
ImprovereusabilityVSAvoiddevice complexity
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The spring-loaded retaining member mechanism is designed to be easily reset by simply pushing the blade member back into the retracted position, where the spring automatically re-engages the pin with the notch. This recovering mechanism allows the broadhead to be rapidly reused without disassembly or complex adjustment, significantly improving productivity while maintaining relatively simple construction.

Inventive Principle:
Principle #34Discarding and recovering

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 broadhead achieves improved flight stability by maintaining blades in a retracted position during flight, ensures reliable expansion upon target impact, and allows for multiple uses with straightforward resetting.

Implementation Method 1

The spring-loaded retaining member is bias to translate in a longitudinal direction along the body towards the target penetrating end of the body

Methodology Applied
Scientific EffectSpring: Spring

Data Source

PatentUS20250155229A1Broadhead
Publication Date: 2025.05.15 TRIKAUSA INC
  • US20250155229A1 patent drawing
  • US20250155229A1 patent drawing
  • US20250155229A1 patent drawing

AI summary

A broadhead includes a body, a blade member, and a plunger. The body defines a target penetrating end. The blade member is positioned partially within an inner volume of the body. The blade member is configured to rotate and translate relative to the body by a pin that is fixedly coupled with the body being received through a slot of the blade member. The blade member is transitionable between a retracted position and a deployed position. The plunger is bias by a spring in a longitudinal direction towards the target penetrating end. The plunger is configured to be received within a recess of the blade member when the blade member is in the retracted position.