Aircraft Turbomachine Pylon With Adjustable Fluid Pipe Docking

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Solution Overview

Problem

The rigid connection of fluid pipes to turbomachines during docking poses a risk of damage to the turbomachine, as they are heavy and difficult to handle.

Innovation Solution

A pylon with a movable portion for the fluid pipe that can adjust its position along the axis, allowing the connection end to be moved between high and low positions, facilitating safe docking without damaging the turbomachine, and incorporating telescopic rods and locking mechanisms for precise adjustment.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If rigid fluid pipes are used for connection, then structural stability is improved, but the risk of damaging the turbomachine during docking increases

Engineering Contradiction:
Improvestructural stabilityVSAvoiddamage risk to turbomachine
Core Design Contradiction:
Stability of the object's compositionVSObject-affected harmful factors

Solution Approach 1:

The fluid pipe is divided into a fixed portion and a movable portion that can independently adjust. This segmentation allows the rigid fixed portion to maintain structural stability while the movable portion can be repositioned to avoid damaging the turbomachine during docking operations.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The fluid pipe incorporates a movable portion that can dynamically adjust its position along the axis between a first position (for connection) and a second position (for protection). This dynamic capability resolves the contradiction by allowing the pipe to be rigid when needed and repositionable when docking the turbomachine.

Inventive Principle:
Principle #15Dynamics

2Ease of manufacture

If the pipe position is fixed, then manufacturing simplicity is improved, but adaptability to different operational positions deteriorates

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidposition adjustability
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The pipe system transitions from a completely fixed structure to a dynamic system with a movable portion that can be repositioned along the axis. This maintains manufacturing simplicity while adding the necessary adaptability for different operational positions during turbomachine docking and testing.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The movable portion of the pipe can be nested within or alongside the fixed portion, allowing compact storage in a retracted position and extended positioning when needed. This nesting approach maintains ease of manufacture while providing position adaptability.

Inventive Principle:
Principle #7Nested doll (Nesting)

3Adaptability or versatility

If the movable portion is added to the pipe, then position adjustability is improved, but device complexity increases

Engineering Contradiction:
Improveposition adjustabilityVSAvoidpipe structure complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

By segmenting the pipe into fixed and movable portions, the complexity is localized to only the necessary moving components rather than the entire pipe system. This segmentation approach provides position adjustability while minimizing overall device complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A plate serves as an intermediary element that carries the movable portion and provides a simple interface for position adjustment. This intermediary structure simplifies the overall design by providing a single point of control for the movable portion rather than requiring complex adjustment mechanisms throughout the pipe.

Inventive Principle:
Principle #24Intermediary (Mediator)

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

Enables safe and efficient connection of fluid pipes to turbomachines, preventing damage during docking and allowing for freedom of movement due to thermal expansion or vibrations.

Implementation Method 1

a compression spring bearing on the second ring and on the plate to bias the second ring to move away from the plate

Methodology Applied
Scientific EffectSpring: Spring

Data Source

PatentUS11435263B2Pylon for supporting an aircraft turbomachine
Publication Date: 2022.09.06 SAFRAN AIRCRAFT ENGINES SAS
  • US11435263B2 patent drawing
  • US11435263B2 patent drawing
  • US11435263B2 patent drawing

AI summary

A pylon for supporting an aircraft turbomachine, in particular for a test bench, the pylon having a generally elongated shape along an axis and including, at a first longitudinal end, first members for fixing to a turbomachine and, at a second longitudinal end, second members for fixing to a base plate, the pylon being traversed by at least one fluid pipe including a first end for connecting to the turbomachine and a second end for connecting to a fluid supply circuit, wherein the at least one pipe includes a movable portion movable in translation along the axis so as to be able to adjust the position along the axis of the first connecting end relative to the first longitudinal end. It also concerns a method of mounting an aircraft turbomachine on such a pylon.