Expandable Broadhead Retainer Geometry for Clean Blade Deployment
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Solution Overview
Problem
Conventional mechanical broadheads face issues with blades inadvertently transitioning to the deployed mode during launch, affecting aerodynamic performance and trajectory, and struggle with inconsistent deployment and reusability due to friction mechanisms.
Innovation Solution
An expandable broadhead design featuring a ferrule with a slot and retainer system, using dimples and arms to securely maintain blades in the retracted mode and facilitate consistent deployment upon impact, with varying slot depths to reduce friction and allow easy transition.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a spring is used to push blades outward against walls to hold them in retracted mode, then the blades can be secured during flight, but the spring creates excessive friction that prevents proper deployment upon target engagement
Solution Approach 1:
The patent removes the spring component from the blade retention system and replaces it with a frictionless mechanical constraint using a pin and slot geometry. This extraction eliminates the source of excessive friction while maintaining reliable blade retention during flight through geometric constraints rather than elastic forces.
Solution Approach 2:
The patent introduces a pin-slot mechanism as an intermediary between the blade and ferrule walls. The slot acts as a guided constraint that allows controlled blade movement while preventing premature deployment, replacing the direct spring-blade contact that caused friction issues.
2Reliability
If a spring is mounted between blades to secure them in retracted mode, then blade retention is achieved, but the spring damages during reuse and reduces broadhead reusability
Solution Approach 1:
The patent replaces the disposable spring component with a durable, non-consumable mechanical constraint system. The pin and slot geometry are designed to withstand multiple use cycles without degradation, eliminating the need for spring replacement and enhancing broadhead reusability.
Solution Approach 2:
The patent substitutes the elastic mechanical system (spring) with a rigid geometric constraint system (pin and slot). This replacement eliminates the wear and damage issues associated with spring fatigue while maintaining the essential blade retention function throughout the broadhead's service life.
3Reliability
If blades are secured with friction mechanisms, then they can be held in retracted mode, but the friction prevents clean and consistent deployment upon impact
Solution Approach 1:
The patent removes friction-based retention mechanisms and replaces them with a frictionless geometric constraint system. The pin and slot design provides deterministic blade retention during launch through geometry rather than friction, enabling consistent and clean deployment upon target impact.
Solution Approach 2:
The patent changes the retention mechanism from friction-dependent to geometry-dependent parameters. By controlling blade position through slot geometry rather than friction forces, the system achieves predictable and consistent deployment characteristics that are insensitive to variations in contact pressure or surface conditions.
4Ease of manufacture
If the slot depth is uniform throughout, then manufacturing is simpler, but friction increases during blade transition from closed to open mode
Solution Approach 1:
The patent applies varying slot depths at different locations along the blade path. The slot is deeper in regions where blade movement is required and shallower where retention is needed, optimizing both blade transition smoothness and retention reliability without excessive manufacturing complexity.
Data Source
AI summary
An expandable broadhead is provided with a ferrule defining a slot within which one or more blades are moveably mounted to a pin. A retainer in the slot can secure the blades in a closed mode when an arrow associated with the broadhead is shot from an archery bow. The retainer can include a dimple and a blade can include a retainer hole within which the dimple nests to secure the blade. The retainer hole can be common with and/or extend from a mass reducing opening defined by the blade. The dimple can ride over contours of the blade on a path to enter the hole with significantly less force than that to release the dimple and retainer from, and deploy, the blade. The slot can increase in depth beyond the dimple to reduce frictional engagement of the blades with slot sidewalls during deployment. A related method is provided.


