Gas Turbine Cover Plate Angled Tabs Installation

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The limited space available for mounting cover plates in gas turbine engine rotor assemblies complicates their installation and removal, and existing solutions do not effectively address the need for efficient retention and sealing without reducing the effectiveness of cover plate bores.

Innovation Solution

The design includes radially and circumferentially retained cover plates with angled tabs and slots that provide clearance for installation and removal, along with seal lands and radial retention features to prevent deflection and ensure secure attachment to the rotor disk, using a tool for installation and removal to facilitate the process.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If cover plates are mounted in limited space of rotor assembly, then sealing between adjacent blade sets is achieved, but installation and removal become complicated

Engineering Contradiction:
Improvesealing effectivenessVSAvoidinstallation and removal ease
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The cover plate is segmented into a body portion and multiple tabs extending from it. The tabs can be inserted into slots in the rotor disk separately, allowing the cover plate to be assembled in sections rather than as a single rigid piece, facilitating installation in limited spaces

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A tool is introduced as an intermediary device to facilitate the installation and removal of the cover plate. The tool engages with the tabs or body of the cover plate, providing mechanical leverage and control during installation and removal operations in the confined rotor assembly space

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If tabs are added for retention, then secure attachment to rotor disk is achieved, but space requirements increase

Engineering Contradiction:
Improveretention securityVSAvoidcover plate volume
Core Design Contradiction:
ReliabilityVSVolume of moving object

Solution Approach 1:

The tabs are designed to nest within slots in the rotor disk when the cover plate is installed. The tabs fit into the slots like nested structures, providing secure retention while minimizing the overall volume occupied by the cover plate assembly

Inventive Principle:
Principle #7Nested doll (Nesting)

Solution Approach 2:

The tabs extend in a radial direction from the body, utilizing the radial dimension of the rotor disk for retention. This dimensional approach allows secure attachment without increasing the axial or tangential dimensions of the cover plate, maintaining compact overall volume

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

Data Source

PatentEP2984303B1Cover plate for a rotor assembly of a gas turbine engine
Publication Date: 2024.12.04 RTX CORP
  • EP2984303B1 patent drawingFigure 1
  • EP2984303B1 patent drawingFigure 2
  • EP2984303B1 patent drawingFigure 3~4

AI summary

A cover plate according to an exemplary aspect of the present disclosure includes, among other things, a body, a first tab near a bore of the body, and a second tab circumferentially spaced from the first tab. A slot is defined between the first tab and the second tab, the first tab, the second tab and the slot extending at an angle relative to a slot axis that extends through the bore. In another embodiment, the cover plate includes a bumper that limits deflection of the body.