Hinged Gas Turbine Access Panel for Blade Maintenance

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing access systems for gas turbine engines face challenges in efficiently accessing and adjusting components, particularly due to obstructive flow surface orientations that impede the removal and installation of blades.

Innovation Solution

An integrated access panel that is hinged to the nacelle and equipped with a biasing member, such as a spring, allowing for movement relative to the flow surface while remaining attached, enabling blade removal and adjustment without rotating the blade row, and featuring a seal to manage working fluid flow.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a fixed access panel is used, then the flow surface orientation is maintained, but blade removal and installation are impeded

Engineering Contradiction:
Improveblade removal and installationVSAvoidaccess panel mechanism
Core Design Contradiction:
Ease of operationVSDevice complexity

Solution Approach 1:

The access panel is transformed from a fixed structure to a movable one, capable of rotating between a first position for blade access and a second position for flow surface alignment. This dynamic configuration allows the panel to adapt to different operational requirements, facilitating blade removal while maintaining aerodynamic performance.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The access panel is divided into movable and stationary components, with the movable portion allowing independent rotation. This segmentation enables the panel to provide both access functionality and flow surface functionality at different times, resolving the contradiction between ease of operation and device complexity.

Inventive Principle:
Principle #1Segmentation

2Ease of operation

If the access panel is moved for blade access, then blade removal is enabled, but working fluid leakage occurs

Engineering Contradiction:
Improveblade accessVSAvoidworking fluid leakage
Core Design Contradiction:
Ease of operationVSObject-generated harmful factors

Solution Approach 1:

A seal is introduced as an intermediary element between the access panel and the housing. This seal prevents working fluid leakage when the panel is in the open position while allowing the panel to move for blade access. The seal acts as a mediator that maintains system integrity during panel movement.

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The seal is configured to be effective in the closed position, dynamically adapting to the panel's position. When the panel rotates to the open position, the seal retracts or adjusts to allow access, and when closed, it engages to prevent leakage, thus resolving the contradiction between access and sealing.

Inventive Principle:
Principle #15Dynamics

3Ease of operation

If the blade row is rotated for blade access, then blade removal is possible, but engine operation is interrupted

Engineering Contradiction:
Improveblade removalVSAvoidengine operation continuity
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

Instead of rotating the entire blade row, only the access panel is segmented and rotated independently. This allows blade access without interrupting the rotation and operation of the remaining blade row, maintaining engine productivity while enabling maintenance operations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The access function is extracted from the blade row rotation mechanism and implemented through a separate, independently movable access panel. This extraction allows blade removal operations to be performed on stationary blades without requiring the interruption of engine operation or rotation of the entire blade row.

Inventive Principle:
Principle #2Taking out (Extraction)

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

Facilitates efficient removal, installation, and adjustment of blades by overcoming obstructive flow surface orientations and maintaining engine operation, while ensuring secure closure and minimizing fluid leakage.

Implementation Method 1

equipped with a biasing member, such as a spring, allowing for movement relative to the flow surface

Methodology Applied
Scientific EffectSpring: Spring

Implementation Method 2

featuring a seal to manage working fluid flow

Methodology Applied
Scientific EffectSealing:

Data Source

PatentUS9759095B2Gas turbine engine access panel
Publication Date: 2017.09.12 ROLLS ROYCE CORP
  • US9759095B2 patent drawing
  • US9759095B2 patent drawing
  • US9759095B2 patent drawing

AI summary

An integrated access panel is disclosed that can be used to assist in adjusting a component like a fan blade of a turbofan engine. in one form the integrated access panel is hinged at one end such that the panel remains attached during adjustment of the fan blade. The access panel can be positioned in an angled flow surface of a nacelle such that the fan blade cannot be removed from a wheel without removal of the nacelle or opening of the access panel. The integrated access panel can be spring-loaded and positioned to allow the fan blade to be removed from a wheel by moving the access panel out of the way. Subsequent blade removal can occur by rotation of the wheel to locate another blade in proximity to the access panel.