Folded Spring Tape Actuator for Higher Skew Servo Bandwidth

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Solution Overview

Problem

The performance of track following servo systems in tape drives is constrained by the performance of the skew actuator, which is limited by the moving mass and flexibility of the actuator, hindering track density scaling and capacity gains.

Innovation Solution

A folded spring actuator design with U-shaped sections and stiffener wings, reducing the moving mass and increasing stiffness, thereby enhancing track and skew following performance.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If a conventional spring actuator design is used, then the structure is simple, but the moving mass is high and stiffness is low

Engineering Contradiction:
Improvemoving massVSAvoidactuator structure complexity
Core Design Contradiction:
Weight of moving objectVSDevice complexity

Solution Approach 1:

The actuator is divided into multiple segments including top section, middle section with parallelized spring legs, and bottom section. This segmentation allows each part to be optimized independently for mass reduction while maintaining structural integrity through the folded C-shape configuration.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent introduces stiffener wings that extend perpendicular to the main spring legs, adding a third dimension to the structure. This dimensional addition increases stiffness without significantly increasing mass, as the stiffeners are positioned to provide leverage against bending moments.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Speed

If the actuator mass is reduced, then skew servo bandwidth improves, but structural stiffness decreases

Engineering Contradiction:
Improveskew servo bandwidthVSAvoidactuator stiffness
Core Design Contradiction:
SpeedVSStrength

Solution Approach 1:

The actuator employs a composite structure combining spring steel for the flexible spring legs with additional stiffening elements. This composite approach allows the primary spring elements to remain lightweight and flexible for high bandwidth while the stiffeners provide the necessary rigidity to suppress flexible modes.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

Stiffener wings are added perpendicular to the spring legs, creating a three-dimensional structure that resists bending moments more effectively. This dimensional addition provides stiffness enhancement without the mass penalty of traditional rigid constructions.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Productivity

If track density scaling is increased, then capacity gains are achieved, but servo system performance is constrained by actuator limitations

Engineering Contradiction:
Improvetrack density scalingVSAvoidservo system performance
Core Design Contradiction:
ProductivityVSReliability

Solution Approach 1:

The actuator design changes key parameters including mass reduction by approximately 48% and stiffness enhancement, which directly improves the servo system's ability to track high-density tracks. These parameter changes enable the actuator to respond faster and more accurately to track following requirements.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The segmented design with parallelized spring legs allows for optimized mass distribution and stiffness characteristics that are specifically tailored for high-speed track following, enabling the servo system to handle increased track density without sacrificing reliability.

Inventive Principle:
Principle #1Segmentation

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 design achieves a 48% reduction in total moving mass, improving skew servo bandwidth and enabling increased track density and capacity through enhanced track following and skew following performance.

Implementation Method 1

a folded spring actuator design with U-shaped sections and stiffener wings

Methodology Applied
Scientific EffectElasticity: Elasticity

Implementation Method 2

stiffener wings, reducing the moving mass and increasing stiffness

Methodology Applied
Scientific EffectStructural reinforcement:

Data Source

PatentUS12555599B2Folded spring tape track following actuator
Publication Date: 2026.02.17 INTERNATIONAL BUSINESS MACHINE CORPORATION
  • US12555599B2 patent drawing
  • US12555599B2 patent drawing
  • US12555599B2 patent drawing

AI summary

An apparatus for a spring actuator positioned in a folded spring actuator assembly includes a top section, a middle section, and a bottom section of the spring actuator that form a C-shape for the spring actuator. The middle section includes two parallelized spring legs, where a cable head module is slidable into a gap formed by the top section and two parallelized spring legs of the middle section of the spring actuator.