Aircraft Engine Pylon Mounting with Pre-Inserted Shear Pins

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Solution Overview

Problem

The existing method for mounting an aircraft engine onto a pylon is labor-intensive due to the need for precise positioning of shear pins, requiring great accuracy and time, especially when attaching the front engine fastener to the lower face of the pylon, which results in a significant space between the engine and the pylon, affecting aerodynamics.

Innovation Solution

A method that pre-inserts two shear pins into the front engine fastener or the pylon's bores, allowing for attachment to the front face of the pylon, reducing the number of shear pins and simplifying the attachment process by positioning and inserting them before mounting, utilizing a system of ball and socket joints and connecting rods for alignment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Object-affected harmful factors

If the existing method of attaching the front engine fastener to the lower face of the pylon is used, then secure fastening is achieved, but a significant space between the engine and pylon is created, increasing aerodynamic drag

Engineering Contradiction:
Improveaerodynamic dragVSAvoidmounting complexity
Core Design Contradiction:
Object-affected harmful factorsVSEase of operation

Solution Approach 1:

The shear pins are pre-inserted into the front engine fastener or pylon bores before the mounting operation. This preliminary action eliminates the need for precise real-time positioning during attachment, reducing mounting complexity while enabling the engine to be positioned closer to the pylon front face, thereby reducing aerodynamic drag.

Inventive Principle:
Principle #10Preliminary action

2Reliability

If precise positioning of shear pins is required during attachment, then secure fastening is ensured, but the mounting process becomes labor-intensive and time-consuming

Engineering Contradiction:
Improvefastening securityVSAvoidmounting time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

Shear pins are pre-inserted into either the front engine fastener or the pylon bores before the mounting operation begins. This preliminary positioning ensures that when the engine is raised and attached, the shear pins are already in place to provide secure fastening, eliminating the need for time-consuming precise positioning during the actual attachment process.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If multiple shear pins are used for attachment, then secure fastening is achieved, but the number of components and mounting complexity increases

Engineering Contradiction:
Improvefastening securityVSAvoidattachment system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Multiple shear pins are pre-inserted into the front engine fastener or pylon bores before mounting. This preliminary action maintains the security provided by multiple pins while simplifying the overall attachment system, as the pins are already positioned and do not require complex positioning mechanisms or procedures during the actual attachment operation.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentUS9708982B2Method for mounting an aircraft engine on a pylon, and engine fastener for implementing said method
Publication Date: 2017.07.18 SAFRAN AIRCRAFT ENGINES SAS
  • US9708982B2 patent drawing
  • US9708982B2 patent drawing
  • US9708982B2 patent drawing

AI summary

A method for mounting an aircraft engine on a pylon includes positioning at least a first shear pin either in a first opening provided in a front engine fastener which is previously attached to the engine using connecting rods, or in a first bore provided in a front surface of the pylon; prepositioning the assembly including the engine and the front engine fastener relative to the pylon by placing the first shear pin opposite a receiving cavity, the receiving cavity being either the first bore, if the first shear pin has been positioned in the first opening, or the first opening, if the first shear pin has been positioned in the first bore; and inserting the first shear pin into the receiving cavity.