Through-Shaft Assembly for Approximate Hole Alignment

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Solution Overview

Problem

The assembly of mechanical connections between aircraft propellants and support masts is complicated by the need for precise alignment of orifices, which is challenging due to the lack of play and congestion of parts, especially in aeronautical applications where the alignment must be perfect to avoid mechanical interference and facilitate stress transmission.

Innovation Solution

A mechanical connection using a shaft with a constant section and an outer surface featuring two diametrically opposite arcs of extra thickness, allowing the shaft to adopt two angular positions to facilitate alignment and assembly, with orifices designed to accommodate these thickness variations for easy alignment and secure bonding without play.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a shaft is used to connect parts requiring perfect alignment, then the mechanical connection strength is improved, but the assembly difficulty increases due to alignment constraints

Engineering Contradiction:
Improvemechanical connection strengthVSAvoidassembly difficulty
Core Design Contradiction:
StrengthVSEase of operation

Solution Approach 1:

The shaft features non-uniform thickness distribution with thicker sections (arcs) at specific locations and thinner sections elsewhere. This local variation in geometry allows the shaft to accommodate misalignment during assembly while maintaining strong mechanical connection when properly positioned, resolving the contradiction between connection strength and assembly ease.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The shaft's cross-sectional parameters are changed along its circumference, creating zones of different thickness. This parameter variation enables the shaft to adapt to alignment tolerances by allowing peripheral gaps in misaligned positions while providing full contact in aligned positions, thus improving both assembly ease and connection strength.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If the shaft has uniform thickness, then the manufacturing is simplified, but the alignment tolerance is reduced

Engineering Contradiction:
Improveshaft manufacturing simplicityVSAvoidalignment precision
Core Design Contradiction:
Ease of manufactureVSManufacturing precision

Solution Approach 1:

Instead of uniform thickness, the shaft implements local quality variations with thicker arcs at specific angular positions. This allows the manufacturing process to focus precision on critical thick sections while tolerating variations in other areas, effectively balancing manufacturing simplicity with alignment precision requirements.

Inventive Principle:
Principle #3Local quality

3Ease of operation

If the orifices are perfectly aligned, then the shaft can be inserted easily, but the assembly time increases due to precise positioning requirements

Engineering Contradiction:
Improveshaft insertion easeVSAvoidassembly time
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The shaft's variable thickness profile creates a geometric feature that guides alignment during insertion. The thicker arcs engage with corresponding orifice features to automatically indicate and achieve proper alignment, reducing the time required for precise positioning while maintaining easy insertion capability.

Inventive Principle:
Principle #35Parameter changes

Data Source

PatentEP3699092B1Set of pieces assembled by a through-shaft mountable when the pieces are approximately lined up
Publication Date: 2021.04.21 AIRBUS OPERATIONS (SAS)
  • EP3699092B1 patent drawingFigure 1~2
  • EP3699092B1 patent drawingFigure 3~4
  • EP3699092B1 patent drawingFigure 5~7

AI summary

The invention relates to an assembly of parts joined together by a shaft (5) passing through holes formed in said parts. The shaft (5) has two diameters in cross-section, namely a base diameter (DB) and a thickened diameter (DE) on diametrically opposed arcs (11) of its cross-section. The holes are aligned with each other and each has a circumference having a first diameter (D1) on diametrically opposed first portions (13), the first diameter (D1) corresponding to the thickened diameter (DE), and a second diameter (D2) larger than the first diameter (D1) on second portions (14) of the circumference. This allows for easy assembly of the shaft even in the case of approximate alignment of the holes, and also facilitates its disassembly. Aeronautical assemblies, for example of an aircraft propulsion unit on a support mast, constitute a preferred application of the invention.