Removable Turbine Gaspath Sensor Sleeve Mounting

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Solution Overview

Problem

Turbine gaspath sensors in gas turbine engines face reduced service life due to high temperatures and combustion gases, leading to seized threaded connections that complicate removal and replacement, increasing labor and downtime.

Innovation Solution

A mounting arrangement using a sleeve with a releasable cap system that secures the sensor to the turbine case, allowing easy access and cooling air circulation, reducing thermal stress and facilitating inspection and replacement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If the sensor is mounted in a threaded bore within the turbine case, then the sensor is securely held in position, but the threaded connection seizes, corrodes, or accumulates contaminants making removal difficult

Engineering Contradiction:
Improvesensor mounting securityVSAvoidsensor removal ease
Core Design Contradiction:
ReliabilityVSEase of repair

Solution Approach 1:

The mounting system is divided into separate components: an outer case with outer ports, an inner case with inner ports, and removable sleeves that connect them. This segmentation allows the sensor to be accessed and removed through the outer ports without disturbing the inner case threading, eliminating the seizure problem while maintaining secure mounting.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The sleeve acts as an intermediary component between the inner case and outer case. It provides a removable connection path that bypasses the problematic threaded bore, allowing sensor removal without disassembling the main turbine case structure.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Device complexity

If the sensor is mounted directly in the turbine case, then the mounting structure is simple, but labor and downtime for sensor replacement increase

Engineering Contradiction:
Improvemounting structure simplicityVSAvoidsensor replacement downtime
Core Design Contradiction:
Device complexityVSLoss of time

Solution Approach 1:

By segmenting the mounting structure into outer case, inner case, and removable sleeves, the system enables quick sensor replacement through the outer ports without complex disassembly, reducing downtime despite the added structural components.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The sleeves are pre-positioned and secured to the inner case before sensor installation. This preliminary action allows the sensor to be quickly accessed and replaced through the outer ports without requiring assembly/disassembly of the main case structure during maintenance.

Inventive Principle:
Principle #10Preliminary action

3Measurement precision

If the sensor probe extends into the gaspath, then the sensor can measure combustion parameters, but high temperatures and combustion gases reduce service life

Engineering Contradiction:
Improvecombustion parameter measurementVSAvoidsensor service life
Core Design Contradiction:
Measurement precisionVSDuration of action of stationary object

Solution Approach 1:

The removable sleeve acts as a protective intermediary between the sensor and the harsh combustion environment. It can be removed and replaced without removing the sensor from the protected inner case position, extending sensor service life while maintaining measurement capability.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The mounting system transitions from a fixed threaded connection to a dynamic, removable sleeve-based connection. This allows the sensor to be quickly replaced when degraded by thermal exposure, restoring measurement precision without prolonged exposure to high temperatures.

Inventive Principle:
Principle #15Dynamics

Data Source

PatentUS10876426B2Removable turbine gaspath sensor
Publication Date: 2020.12.29 PRATT & WHITNEY CANADA CORP
  • US10876426B2 patent drawing
  • US10876426B2 patent drawing
  • US10876426B2 patent drawing

AI summary

A gas turbine engine comprises a turbine within a turbine case defining a hot combustion gas path. The turbine case has an inner port. An outer case is disposed radially outward from the turbine case. The outer case has an outer port. A sleeve releasably engages the outer port and the inner port. A sensor is mounted to a distal end of the sleeve. The sensor has a probe extending through the inner port into the hot combustion gas path.