Out-of-plane accelerometer pillar stiffening

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Solution Overview

Problem

Out-of-plane accelerometers face challenges with high raw bias and bias stability due to assembly stress, temperature changes, and aging effects, which are not adequately addressed by existing decoupling frames and manufacturing methods.

Innovation Solution

The design incorporates a seismic mass acting as a capacitor plate, with a pillar extending between two capacitor plates, supported by elastic beams anchored to the pillar, and a decoupling frame with a limited surface area for mounting, which reduces bias sensitivity and improves stability through stiffening and stress decoupling.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If a decoupling frame with stacked wafer layers is used to reduce assembly stress, then the initial raw bias is reduced, but the structure becomes more complex and difficult to mount on a package

Engineering Contradiction:
Improveraw biasVSAvoidstructure complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The accelerometer is divided into separate functional modules: a sensor box containing the capacitive sensing elements and a seismic mass, and a separate decoupling frame. This segmentation allows each module to be optimized independently - the sensor box for sensing precision and the decoupling frame for stress management and mounting ease.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The decoupling frame acts as an intermediary element between the sensor box and the package substrate. It provides a compliant mounting interface that decouples assembly stresses from the sensitive sensor box while maintaining mechanical support, thereby reducing raw bias without complicating the mounting process.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If the decoupling frame is made thin to bend under stress without transmitting it to the sensor box, then assembly stress is reduced, but the surface area for mounting becomes very small making mounting cumbersome

Engineering Contradiction:
Improveraw biasVSAvoidmounting ease
Core Design Contradiction:
Measurement precisionVSEase of operation

Solution Approach 1:

The decoupling frame exhibits local quality variations: it has thin, compliant regions that bend to absorb assembly stress and protect the sensor box, while simultaneously providing sufficient mounting surface area in strategic locations for easy attachment to the package substrate. This localized differentiation of mechanical properties resolves the contradiction between stress decoupling and mounting ease.

Inventive Principle:
Principle #3Local quality

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 significantly reduces raw bias and improves bias stability by minimizing die attach stress and enhancing the sensor box's stiffness, allowing for more accurate acceleration detection over time.

Implementation Method 1

The mass displacement is sensed through capacitive detection. Two capacitor plates are arranged in parallel configuration above and below the seismic mass.

Methodology Applied
Scientific EffectCapacitive detection: Capacitance

Implementation Method 2

The seismic mass is supported by elastic beams anchored to a frame. This structure absorbs stress and reduces bias instability.

Methodology Applied
Scientific EffectElastic deformation: Elasticity

Data Source

PatentUS10598689B2Out-of plane-accelerometer
Publication Date: 2020.03.24 SAFRAN SENSING TECHNOLOGIES SWITZERLAND SA
  • US10598689B2 patent drawing
  • US10598689B2 patent drawing
  • US10598689B2 patent drawing

AI summary

Accelerometer including a seismic mass in a plane and a first capacitor plate and a second capacitor plate arranged parallel to the plane. The seismic mass is arranged in between the first capacitor plate and the second capacitor plate. The first capacitor plate and the second capacitor plate are configured to detect movements of the seismic mass out of the plane. A pillar extending from the first capacitor plate to the second capacitor plate through a cut-out in the seismic mass for stiffening the accelerometer.