Aircraft Engine Component Joint with Spring Beams Against Wobble

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Solution Overview

Problem

Existing aircraft engine joints lack effective mechanisms for providing a sealed and stable engagement between components, leading to potential movement and inefficiencies during operation.

Innovation Solution

A joint assembly featuring a case, housing, and a component with cantilevered spring beams that axially engage the case, providing a sealed and stable connection through elastic deflection, allowing for reduced movement and improved sealing.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If rigid mechanical joints are used between engine components, then structural strength is maintained, but movement and wobbling occur during operation due to manufacturing tolerances

Engineering Contradiction:
Improveengagement stabilityVSAvoidmovement control
Core Design Contradiction:
Stability of the object's compositionVSReliability

Solution Approach 1:

The patent applies the dynamics principle by replacing rigid mechanical joints with flexible spring beams that can dynamically adjust to operational movements and vibrations. The spring beams are designed to flex and deform elastically, allowing the joint to adapt to manufacturing tolerances and maintain stable engagement without rigid constraints that cause wobbling.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The patent implements parameter changes by utilizing the elastic properties of spring beams, where the physical state of the connecting element changes from rigid to flexible. The spring beams can change their degree of compression and extension based on operational conditions, enabling the joint to maintain reliable engagement while accommodating dimensional variations.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If conventional joints are used between components, then assembly is simple, but sealed engagement is not achieved leading to potential leaks

Engineering Contradiction:
Improveassembly simplicityVSAvoidsealing effectiveness
Core Design Contradiction:
Ease of manufactureVSObject-affected harmful factors

Solution Approach 1:

The patent applies flexible elements in the form of spring beams that act as compliant sealing surfaces. These flexible components can deform to conform to mating surfaces, creating effective seals without requiring complex gasket systems or precision machining, thus maintaining assembly simplicity while achieving reliable sealing.

Inventive Principle:
Principle #30Flexible shells and thin films

3Stability of the object's composition

If precision manufacturing is applied to reduce tolerances, then engagement stability improves, but manufacturing cost and complexity increase

Engineering Contradiction:
Improveengagement stabilityVSAvoidtolerance requirements
Core Design Contradiction:
Stability of the object's compositionVSManufacturing precision

Solution Approach 1:

The patent changes the physical parameters of the joint system by introducing flexible spring beams that can accommodate dimensional variations. This allows the use of less precise manufacturing processes while maintaining stable engagement, as the elastic elements absorb the effects of manufacturing tolerances through their ability to flex and adapt.

Inventive Principle:
Principle #35Parameter changes

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

The assembly ensures a stable and sealed engagement between engine components, reducing wobbling and enhancing operational stability while accommodating manufacturing tolerances and facilitating a mistake-proof assembly process.

Implementation Method 1

The spring beams are cantilevered from the rim, are axially spaced from the case and axially engage the housing such that the spring beams bias the rim axially towards the case to provide a sealed engagement axially between the mount and the case

Methodology Applied
Scientific EffectElastic deflection: Elasticity

Data Source

PatentUS12535034B1Joint between aircraft engine components with spring beams
Publication Date: 2026.01.27 PRATT & WHITNEY CANADA CORP
  • US12535034B1 patent drawing
  • US12535034B1 patent drawing
  • US12535034B1 patent drawing

AI summary

An assembly includes a case, a housing and a component. The case includes an aperture, an exterior side and an interior side. The aperture extends axially along an axis through the case from the exterior side to the interior side. The interior side forms a peripheral boundary of an internal volume of the aircraft engine. A cavity is formed by and extends axially between the housing and the case. The component includes a projection and a mount that is disposed within the cavity. The projection projects axially out from the mount, through the aperture, and into the internal volume to a distal end of the component. The mount includes a rim and a plurality of spring beams. The spring beams bias the rim axially towards the case to provide a sealed engagement axially between the mount and the case.