Castellated Turbomachine Flanges for Faster Assembly and Clocking

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Solution Overview

Problem

Current turbomachine component coupling methods require significant time for installing fastener hardware and limit thrust reverser clocking due to the large number of interface flanges, which is inefficient and restrictive for certain turbofan engine configurations.

Innovation Solution

The use of castellation flanges with internal and external attachment flanges, where each flange section extends radially and is disposed perpendicular to the axis of symmetry, forming mating pairs with receptacle sections that allow for anti-rotation features and asymmetric spacing, facilitating efficient coupling and assembly without the need for extensive fastener installation and enabling flexible clocking.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If traditional interface flanges with multiple bolts and nuts are used to couple turbomachine components, then the connection is secure and reliable, but the assembly time becomes excessively long and the clocking flexibility is limited

Engineering Contradiction:
Improveassembly speedVSAvoidnumber of fasteners
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The patent combines multiple fastening functions into a single integrated castellated flange structure. The interlocking teeth of the castellated flange replace the need for multiple individual bolts and nuts, merging the functions of alignment, positioning, and securing into one component that achieves the same reliable connection with significantly fewer fasteners.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The flange is segmented into multiple interlocking teeth or castellations rather than using a solid continuous flange design. This segmentation allows the flange to engage with corresponding teeth on the mating component, creating multiple contact points that distribute loads and provide secure connection while reducing the number of separate fastening elements needed.

Inventive Principle:
Principle #1Segmentation

2Adaptability or versatility

If 36 interface flanges are used around the component mating end, then the connection is secure, but the thrust reverser clocking is limited to 10-degree increments

Engineering Contradiction:
Improveclocking flexibilityVSAvoidnumber of interface flanges
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The castellated flange design incorporates asymmetric tooth configurations and varying spacing between teeth, allowing for continuous or finer angular adjustments rather than being constrained to fixed 10-degree increments. This asymmetric arrangement enables the thrust reverser to be clocked to precise angular positions while maintaining secure mechanical engagement.

Inventive Principle:
Principle #4Asymmetry

Data Source

PatentUS11421557B1Turbomachine components including castellation flanges and methods for coupling turbomachine components
Publication Date: 2022.08.23 HONEYWELL INTERNATIONAL INC
  • US11421557B1 patent drawing
  • US11421557B1 patent drawing
  • US11421557B1 patent drawing

AI summary

Turbomachines and methods for coupling first and second turbomachine components are provided. The components include castellated flange arrangements that provide an improved retention method for retaining the components that is far superior in than bolts and nuts, especially for massive unbalance loading.