Drive Bit Taper Angles for Consistent Fastener Retention

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Solution Overview

Problem

Current drive systems lack consistent and reliable frictional engagement between drive bits and fasteners due to tolerance band overlaps, leading to inconsistent force requirements for achieving desired frictional engagement levels.

Innovation Solution

The drive system features a drive bit with a tapered pilot end and a fastener with a tapered internal recess, where the leading wall angle and recess wall angle tolerance bands do not overlap, ensuring consistent frictional engagement by defining a targeted focal area for contact, allowing for friction fit to jam fit levels of engagement based on deformation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the pilot recess and drive bit are configured with matching angles and overlapping tolerance bands to achieve frictional engagement, then the fastener can be retained on the drive bit, but the frictional engagement becomes inconsistent and unreliable

Engineering Contradiction:
Improvefrictional engagement consistencyVSAvoidangle tolerance band overlap
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

The patent modifies the geometric parameters of the pilot recess and drive bit by specifying non-overlapping tolerance bands for their respective angles. The pilot recess angle is maintained within a first tolerance band, while the drive bit angle is maintained within a second tolerance band that does not overlap with the first, ensuring consistent frictional engagement without relying on overlapping tolerances

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces the traditional mechanical interference fit approach (relying on overlapping tolerance bands to create friction) with a controlled deformation mechanism. The drive bit is designed to elastically deform the pilot recess material to a specific strain level, creating predictable frictional engagement through controlled material deformation rather than geometric interference

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

2Reliability

If a light force is applied to the drive bit to avoid deformation of the pilot recess, then the recess remains undamaged, but no frictional engagement is achieved

Engineering Contradiction:
Improvefrictional engagementVSAvoidend load on drive bit
Core Design Contradiction:
ReliabilityVSForce

Solution Approach 1:

The patent establishes specific parameter ranges for the drive bit geometry (angle, length, diameter) and pilot recess properties that enable controlled elastic deformation. By configuring these parameters within defined ranges, the system achieves frictional engagement through predictable material deformation at controlled force levels, rather than requiring excessive force or relying on light contact

Inventive Principle:
Principle #35Parameter changes

3Reliability

If excessive force is applied to achieve high frictional engagement (jam fit), then the fastener is securely retained, but the pilot recess undergoes non-elastic deformation that may compromise future engagements

Engineering Contradiction:
Improvefrictional engagement levelVSAvoidpilot recess structural integrity
Core Design Contradiction:
ReliabilityVSStrength

Solution Approach 1:

The patent incorporates feedback mechanisms through specified geometric parameters and material properties that limit deformation to elastic ranges. The drive bit configuration (angle, length, diameter) and pilot recess dimensions are designed to work together to ensure that during installation, the force applied results in elastic deformation only, preventing permanent damage while achieving sufficient frictional engagement

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent defines specific parameter ranges for drive bit and pilot recess geometry that control the deformation behavior. By maintaining angles within non-overlapping tolerance bands and specifying dimensional relationships, the system ensures that installation forces produce elastic deformation within safe limits, achieving jam fit or stick fit engagement without compromising the pilot recess structure

Inventive Principle:
Principle #35Parameter changes

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 configuration provides reliable and consistent frictional engagement between the drive bit and fastener, ensuring the fastener remains securely attached without disengagement, with adjustable friction levels achieved through controlled deformation.

Implementation Method 1

A stick fit is achieved by applying enough force to the bit to have the internal pilot recess both elastically and non-elastically deformed with more elastic than non-elastic deformation of the recess

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Implementation Method 2

Friction holds the bit into the pilot recess and requires a predefined force, i.e., end load to push the bit into the pilot recess to achieve a desired level of frictional engagement between the bit pilot end and the pilot recess

Methodology Applied
Scientific EffectFriction: Friction

Data Source

PatentUS11926021B2Drive system configured to provide frictional fit engagement
Publication Date: 2024.03.12 TTAPDRIVE
  • US11926021B2 patent drawing
  • US11926021B2 patent drawing
  • US11926021B2 patent drawing

AI summary

A drive system including a bit with a bit end configured to provide targeted frictional engagement with a fastener. The bit end has an outer leading wall tapered with respect to the bit end longitudinal axis at a leading wall angle selected from leading wall angle values ranging within a leading wall angle tolerance band and the fastener has an inner recess wall tapered with respect to the fastener longitudinal axis at a recess wall angle selected from recess wall angle values ranging within a recess wall angle tolerance band, wherein the leading wall angle values within the leading wall angle tolerance band and the recess wall angles values within the recess wall angle tolerance band do not overlap when the outer leading wall contacts the inner pilot recess wall at a targeted focal area to achieve a desired level of frictional engagement between the pilot end and the fastener.