NMR MAS Probe Rotor Housing Temperature Gradient Control

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Solution Overview

Problem

In nuclear magnetic resonance (NMR) spectroscopy, temperature gradients across samples in magic angle spinning (MAS) experiments, especially at high temperatures, adversely affect spectral resolution and analysis, due to inhomogeneous heating and inefficient heat transfer, making it challenging to maintain uniform temperatures for accurate data interpretation.

Innovation Solution

The implementation of a rotor housing assembly that controllably heats the bearing gas flow and/or drive gas flow, in addition to the traditional variable temperature gas flow, to minimize temperature gradients across the sample, using heated gas flows to maintain a temperature gradient of 3° C. or less, compatible with standard rotors and high-pressure WHiMS rotors, allowing for in-situ NMR studies of mixed-phase reactions.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If conventional VT heating with heated VT gas stream is used, then sample temperature can be raised to high temperatures, but temperature gradient across the sample increases

Engineering Contradiction:
Improvesample temperatureVSAvoidtemperature gradient
Core Design Contradiction:
TemperatureVSStability of the object's composition

Solution Approach 1:

The heating system is segmented into multiple independent heating zones: a central VT heating zone and two end heating zones. Each zone has its own heated gas flow inlet, allowing independent temperature control to compensate for heat loss at rotor ends and eliminate temperature gradients across the sample.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Different regions of the rotor receive differently heated gas flows tailored to their specific thermal requirements. The central sample region receives hot VT gas, while the end regions receive additional heated gas to compensate for heat loss, creating locally optimized temperature distribution throughout the rotor.

Inventive Principle:
Principle #3Local quality

2Reliability

If high flow rates of driving and bearing gas are used for cooling, then rotor stability is improved, but cooling effects create temperature gradients

Engineering Contradiction:
Improverotor stabilityVSAvoidtemperature uniformity
Core Design Contradiction:
ReliabilityVSStability of the object's composition

Solution Approach 1:

The temperature parameter of the bearing gas is changed from ambient to elevated temperatures. By heating the bearing gas to match the sample temperature, the gas no longer creates cooling effects and temperature gradients, while still providing necessary lubrication and rotor stability.

Inventive Principle:
Principle #35Parameter changes

3Speed

If laser heating is used to achieve temperature jumps, then heating speed is improved, but spatial temperature distribution becomes inhomogeneous

Engineering Contradiction:
Improveheating speedVSAvoidtemperature distribution
Core Design Contradiction:
SpeedVSStability of the object's composition

Solution Approach 1:

Heated gas flows are directed to specific local regions (central VT inlet and end inlets) to create targeted heating zones. This distributed local heating approach achieves rapid temperature increase throughout the sample while maintaining spatial temperature uniformity, avoiding the inhomogeneous heating problem of laser methods.

Inventive Principle:
Principle #3Local quality

4Temperature

If inductive heating with platinum layers is used, then temperature jumps can be achieved, but specialized rotors and inserts are required

Engineering Contradiction:
Improvetemperature jump capabilityVSAvoidspecialized rotor requirements
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The heated gas flow system serves multiple functions: it heats the sample, compensates for end heat loss, and can be adjusted for different temperature requirements. This universal heating approach works with standard rotors and can be adapted to any rotor size and spin rate, eliminating the need for specialized platinum-coated rotors or inserts.

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 approach enables precise temperature control across the sample, enhancing spectral resolution and allowing for the first in-situ NMR monitoring of chemical reactions at temperatures above 250° C. in a pressurized environment, significantly improving the accuracy of high-temperature MAS experiments.

Implementation Method 1

A first heated gas flow from a first gas source is controllably flowable through the first heated gas flow inlet and into the interior space of the housing to heat the interior space and the rotor

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

A second heated gas flow from a second gas source through the second heated gas flow outlets is controllable to heat distal and proximal areas of the sample space within the rotor to minimize a temperature gradient

Methodology Applied
Scientific EffectConduction (thermal): Conduction (thermal)

Data Source

PatentUS11137458B2High-temperature NMR MAS probe with optimized temperature gradient across sample rotor
Publication Date: 2021.10.05 BATTELLE MEMORIAL INST
  • US11137458B2 patent drawing
  • US11137458B2 patent drawing
  • US11137458B2 patent drawing

AI summary

A rotor housing assembly for NMR spectroscopy. An elongate rotor has a distal drive end, a proximal end and an internal sample space positioned along its length between the drive and proximal ends. The rotor is driveable about a rotation axis by a drive gas flow. A rotor housing has an interior space in which the rotor is at least partially received. At least one first heated gas flow inlet is positioned opposite the internal sample space, through which a first heated gas flow is controllably flowable into the interior space to heat it and the rotor. At least a pair of spaced apart second heated gas flow outlets are axially spaced from the first heated gas flow inlet to controllably convey a second heated gas flow to heat distal and proximal areas of the sample space to minimize a temperature gradient extending axially within the sample space.