Aircraft Engine Mount with Coat Hanger Shackle and Failsafe Securement

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Solution Overview

Problem

Aircraft engine mounts require fail-safe mechanisms to ensure safe operation in case of failure, while also being readily accessible for efficient installation, removal, and servicing, and must accommodate load distribution and thermal expansion without introducing internal stresses.

Innovation Solution

The engine mounting system includes a forward shackle assembly with a coat hanger bracket, center and spherical bearings, and a double wrench washer tool, along with an aft mount that reacts vertical, lateral, and rear loads, providing fail-safe features and statically determinant load paths under all conditions, including component failures, and accommodates installation tolerances and thermal expansion.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If fail-safe mechanisms are incorporated into engine mounts, then safety and reliability are improved, but device complexity increases

Engineering Contradiction:
ImprovesafetyVSAvoidcomplexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The engine mount system is divided into multiple independent securement points (primary and secondary) that can function independently. Each mounting point has its own bearing and fastening mechanism, allowing the system to maintain functionality even if one segment fails, thus improving reliability without requiring a completely complex integrated system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The design incorporates secondary securement points and fail-safe mechanisms in advance before any failure occurs. These backup elements are pre-positioned and ready to engage automatically upon failure of primary mounting points, providing beforehand protection against potential failures while maintaining a relatively simple overall structure.

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

2Reliability

If multiple securement points are used to ensure fail-safe operation, then reliability is improved, but ease of operation deteriorates

Engineering Contradiction:
Improvefail-safe operationVSAvoidinstallation and servicing
Core Design Contradiction:
ReliabilityVSEase of operation

Solution Approach 1:

The mounting system uses modular segmented components including individual bearings, pins, and fasteners that can be independently installed or removed. This segmentation allows maintenance personnel to access and service specific mounting points without having to disassemble the entire engine mount system, improving ease of operation while maintaining multiple securement points for reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The bearing assemblies are designed to be extractable from the mount structure, allowing quick removal and replacement during maintenance. This extraction capability enables efficient servicing of individual securement points without affecting other parts of the mounting system, thus improving ease of operation while preserving the fail-safe multi-point securement architecture.

Inventive Principle:
Principle #2Taking out (Extraction)

3Adaptability or versatility

If the mount system accommodates thermal expansion and installation tolerances, then adaptability is improved, but device complexity increases

Engineering Contradiction:
Improvethermal expansion accommodationVSAvoidstructural complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The bearing selections and mounting clearances are specifically chosen to accommodate thermal expansion parameters. By selecting appropriate bearing types with suitable clearance ranges and specifying tolerance ranges for mounting hole dimensions, the system naturally accommodates thermal growth and installation variations without requiring complex adjustment mechanisms or additional components.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The design incorporates slightly excessive clearance in the bearing fits and mounting tolerances to ensure that thermal expansion and installation variations are always accommodated. This partial excess in dimensional tolerances provides a buffer that absorbs thermal growth and tolerance stack-up without requiring the structure to be precisely controlled, thereby maintaining simplicity while improving adaptability.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS10752370B2Aircraft engine mount
Publication Date: 2020.08.25 LORD CORP
  • US10752370B2 patent drawing
  • US10752370B2 patent drawing
  • US10752370B2 patent drawing

AI summary

An engine mount system having failsafe securement points. The engine mount system includes a forward mount carrying a coat hanger shackle having a spherical bearing and a cylindrical bearing. Securement of the engine mount to a support utilizes pins and bolts with a retaining double wrench washer incorporated into the final mounting structure. The engine mount system additionally includes an aft mount.