MEMS Taper Layer Clamping for Thin Membrane Robustness

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Solution Overview

Problem

MEMS structures with membrane structures face challenges in achieving a balance between stability and performance, particularly in applications requiring robustness under high pressure conditions, such as True Wireless Stereo (TWS), where mechanical strain can lead to failure.

Innovation Solution

A MEMS structure design featuring a second clamping structure with a structured taper layer and a second structured oxide layer that extends laterally over the cavity, providing improved support to the membrane structure, while a first clamping structure is laterally offset to form a gap, reducing stress hotspots and enhancing mechanical stability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the membrane structure size or thickness is increased to improve stability, then the mechanical robustness is improved, but the device performance is negatively affected

Engineering Contradiction:
Improvemechanical robustnessVSAvoiddevice performance
Core Design Contradiction:
ReliabilityVSProductivity

Solution Approach 1:

The patent applies local quality by implementing a structured taper layer with varying thickness (from thicker region to thinner region) at specific locations where mechanical support is needed, rather than uniformly increasing the entire membrane structure. This allows localized strengthening at the clamping structure interface while preserving the performance characteristics of the main membrane area.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent uses composite materials by combining the membrane structure with a structured oxide layer and a structured taper layer (e.g., SiON or SiO2) to create a composite clamping structure. This composite approach provides enhanced mechanical support and stress distribution without requiring the entire membrane to be thicker, thus maintaining performance while improving robustness.

Inventive Principle:
Principle #40Composite materials

2Ease of manufacture

If a single back-plate design is used to simplify structure, then manufacturing is easier, but the Distance Airblow Test robustness is insufficient

Engineering Contradiction:
Improvestructural simplicityVSAvoidDAT robustness
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent segments the clamping structure into multiple functional layers: a first clamping structure with a first structured oxide layer, a second clamping structure with a second structured oxide layer and structured taper layer. This segmentation allows each layer to perform specific functions (support, stress distribution, gradual transition) that collectively achieve high DAT robustness while maintaining manufacturing feasibility through standardized deposition processes.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent adds dimensional complexity by introducing a structured taper layer with gradual thickness variation in the vertical dimension, transitioning from the second structured oxide layer to the membrane structure. This dimensional approach (varying thickness rather than uniform structure) provides superior mechanical support and stress distribution for DAT robustness without significantly complicating the manufacturing process.

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

3Reliability

If the first clamping structure is positioned close to the cavity to maximize support, then mechanical support is improved, but stress hotspots are created leading to potential failure

Engineering Contradiction:
Improvemechanical supportVSAvoidstress hotspots
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent implements beforehand cushioning by introducing a structured taper layer with gradual thickness transition between the second structured oxide layer and the membrane structure. This gradual transition acts as a cushion that distributes mechanical stress evenly, preventing the formation of stress hotspots that would occur with abrupt transitions, thereby eliminating potential failure points before they can develop under pressure.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

Data Source

PatentEP4626034A1MEMS structure with a structured taper layer
Publication Date: 2025.10.01 INFINEON TECHNOLOGIES AG
  • EP4626034A1 patent drawingFigure 1
  • EP4626034A1 patent drawingFigure 2a~2d
  • EP4626034A1 patent drawingFigure 3

AI summary

A MEMS structure, comprising a back-plate structure, a support structure having a cavity, a membrane structure between the back-plate structure and the support structure, a first clamping structure having a first structured oxide layer between the support structure and the membrane structure, wherein an inner edge of the first clamping structure is laterally offset from an edge of the cavity, wherein the offset of the first clamping structure forms a gap between the support structure and the membrane structure, and a second clamping structure having a second structured oxide layer and a structured taper layer between the back-plate structure and the membrane structure, wherein the second structured oxide layer is arranged between the back-plate structure and the structured taper layer, and wherein an inner edge of the second structured oxide layer laterally extends over the cavity, and wherein the structured taper layer is arranged between the second structured oxide layer and the membrane structure and has a tapered edge region, which laterally extends beyond the edge of the second structured oxide layer on the membrane structure.