NMR-MAS Turbine Cap Geometry for 111 kHz Stability

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Solution Overview

Problem

Conventional NMR-MAS rotors face challenges in achieving higher rotation frequencies due to issues with running stability, production difficulties, and bending oscillations, especially at frequencies above 70 kHz, where tangential speeds approach the speed of sound, making it hard to maintain stability and produce suitable turbine caps with effective blade geometries.

Innovation Solution

A turbine cap with a specific blade geometry and design, featuring a stopper region with a sealing section and a turbine region with five blades, where the blade tips have a sharp radius of curvature and merge into a concave first blade piece, is used to drive an NMR-MAS rotor to a rotation frequency of up to 111 kHz, ensuring good running stability and efficiency through fine milling and mechanical stabilization.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If the rotor radius is reduced to achieve higher rotation frequencies, then the tangential speed decreases and higher frequencies become achievable, but production difficulties increase and bending oscillations become more relevant

Engineering Contradiction:
Improverotation frequencyVSAvoidproduction difficulty
Core Design Contradiction:
SpeedVSEase of manufacture

Solution Approach 1:

The patent applies parameter changes by precisely controlling the blade geometry parameters, specifically the radius of curvature at the blade tip (0.0020-0.0045 mm) and the concave first blade piece radius (0.050-0.150 mm). These parameter optimizations enable the rotor to achieve frequencies up to 111 kHz while maintaining manufacturability through fine milling processes.

Inventive Principle:
Principle #35Parameter changes

2Speed

If the rotor radius is reduced to achieve higher rotation frequencies, then the tangential speed decreases and higher frequencies become achievable, but bending oscillations increase

Engineering Contradiction:
Improverotation frequencyVSAvoidrunning stability
Core Design Contradiction:
SpeedVSStability of the object's composition

Solution Approach 1:

The patent employs curvature principles by designing blade tips with a specific radius of curvature (0.0020-0.0045 mm) and incorporating a concave first blade piece with radius (0.050-0.150 mm). This curved geometry optimizes gas flow patterns and reduces turbulence, thereby minimizing bending oscillations and improving running stability at high rotation frequencies up to 111 kHz.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Ease of manufacture

If conventional blade geometries are used at high rotation frequencies, then production is simpler, but running stability deteriorates due to bending oscillations and turbulence

Engineering Contradiction:
Improveproduction simplicityVSAvoidrunning stability
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent applies local quality by optimizing specific regions of the turbine blade rather than the entire blade structure. The blade tip region features a precise radius of curvature (0.0020-0.0045 mm) and the leading edge incorporates a concave first blade piece (0.050-0.150 mm radius). These localized geometric optimizations improve gas flow characteristics and reduce turbulence in critical areas, enhancing running stability while maintaining overall production feasibility through fine milling.

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

The described turbine cap allows for efficient operation at frequencies up to 111 kHz with improved line sharpness in NMR spectra and reduced production complexity, maintaining mechanical robustness and stability, while minimizing bending oscillations and turbulence.

Implementation Method 1

A drive nozzle system drives the turbine blades with compressed gas flows

Methodology Applied
Scientific EffectCompressed gas flow:

Implementation Method 2

the rotor is usually mounted in a noncontact manner by means of two radial bearings and a bottom bearing with compressed gas flows

Methodology Applied
Scientific EffectGas bearing: Air Lubrication

Data Source

PatentUS10241162B2NMR-MAS turbine assembly
Publication Date: 2019.03.26 BRUKER BIOSPIN MRI GMBH
  • US10241162B2 patent drawing
  • US10241162B2 patent drawing
  • US10241162B2 patent drawing

AI summary

A nuclear magnetic resonance-magic angle spinning (NMR-MAS) turbine assembly has a MAS rotor with turbine cap having a stopper region and a turbine region. The stopper region allows feeding into a rotor tube and has at least one sealing section for resting against an inner wall of the rotor tube. The turbine region has a collar section for resting against a face side of the rotor tube and a turbine section that forms the turbine blades, which protrude axially from the collar section without extending radially further than the collar section. The arrangement of the rotor allows for very high rotation frequencies that, correspondingly, reduce line broadening in NMR measurements.