Underwing Heat Exchanger Bracket Assembly for Wing Bending

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Solution Overview

Problem

Existing aircraft propulsion system heat exchanger cooling assemblies lack efficient and resilient mounting solutions that accommodate wing bending during flight and potential disruptions, such as bird strikes, while maintaining effective thermal management.

Innovation Solution

A mounting assembly for underwing heat exchangers featuring pivotably mounted heat exchanger brackets to support brackets, allowing flexibility and resilience, with brackets fixedly attached to the wing body, and optionally incorporating an underwing fairing for airflow management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If rigid mounting is used to securely attach heat exchangers to the wing body, then the heat exchangers remain firmly fixed, but the mounting cannot accommodate wing bending during flight

Engineering Contradiction:
Improvesecure attachment of heat exchangersVSAvoidaccommodation of wing bending
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The mounting assembly incorporates pivotable brackets that allow dynamic adjustment and movement. The heat exchanger brackets can pivot relative to the support brackets, enabling the system to adapt to wing bending while maintaining secure attachment. This dynamic mechanism resolves the contradiction between rigid fixation and flexibility needed for wing deformation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The mounting assembly is divided into multiple independent components: support brackets fixed to the wing body, heat exchanger brackets attached to the heat exchangers, and pivot connections between them. This segmentation allows each component to perform its specific function while the overall system accommodates wing bending through the pivot joints.

Inventive Principle:
Principle #1Segmentation

2Adaptability or versatility

If the mounting assembly is made flexible to accommodate wing bending, then the heat exchangers can remain attached during flight, but the heat exchangers may become detached during disruptions like bird strikes

Engineering Contradiction:
Improveaccommodation of wing bendingVSAvoidattachment security during disruptions
Core Design Contradiction:
Adaptability or versatilityVSReliability

Solution Approach 1:

The pivotable mounting assembly is designed to absorb and distribute impact forces through its articulated joints. During disruptions like bird strikes, the pivot connections allow controlled movement that cushions the impact, preventing catastrophic detachment while maintaining attachment security. The design anticipates potential disruptions and incorporates force-distributing mechanisms in advance.

Inventive Principle:
Principle #11Beforehand cushioning (Prior cushioning)

3Reliability

If multiple support brackets are used to securely mount the heat exchanger brackets, then the attachment is more reliable, but the mounting assembly becomes more complex

Engineering Contradiction:
Improvemounting reliabilityVSAvoidmounting assembly structure
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The mounting assembly is segmented into modular support brackets and heat exchanger brackets connected by pivot joints. This segmentation allows the use of multiple brackets for enhanced reliability while keeping each individual component simple and manageable. The modular design reduces overall system complexity compared to a monolithic rigid structure.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP4650270A1Underwing heat exchanger assembly for an aircraft
Publication Date: 2025.11.19 PRATT & WHITNEY CANADA CORP
  • EP4650270A1 patent drawingFigure 1
  • EP4650270A1 patent drawingFigure 2A~2B
  • EP4650270A1 patent drawingFigure 3

AI summary

An assembly for an aircraft includes a wing assembly, a plurality of underwing heat exchangers (84), and a mounting assembly (86). The wing assembly includes a wing body. The plurality of underwing heat exchangers (84) are arranged along the wing body in a longitudinal direction. The plurality of underwing heat exchangers (84) includes a first underwing heat exchanger (84) and a second underwing heat exchanger (84). The first underwing heat exchanger (84) is longitudinally adjacent the second underwing heat exchanger (84). The mounting assembly (86) includes a first heat exchanger bracket (96), a second heat exchanger bracket (96), and a first support bracket (98). The first heat exchanger bracket (96) is fixedly mounted to the first underwing heat exchanger (84). The second heat exchanger bracket (96) is fixedly mounted to the second underwing heat exchanger (84). The first heat exchanger bracket (96) and the second heat exchanger bracket (96) are pivotably mounted to the first support bracket (98). The first support bracket (98) is fixedly mounted to the wing body.