Variable-section nozzle flap alignment via radial offset

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Solution Overview

Problem

Conventional variable-section turbomachine nozzles with moving flaps experience leaks between adjacent flaps due to offset pivoting, leading to performance issues such as reduced thrust and increased specific consumption during operation.

Innovation Solution

Introducing a radial offset between moving flaps associated with follower and controlled levers, achieved by modifying the machining of follower levers, ensures that all flaps align on a common diameter during operation, preventing leaks and maintaining simplicity and cost-effectiveness.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If moving flaps are actuated by control levers with swivel-fork connections, then the nozzle can modify the primary stream profile, but large leaks occur between adjacent flaps due to offset pivoting

Engineering Contradiction:
Improveprimary stream profile modificationVSAvoidleakage between flaps
Core Design Contradiction:
Adaptability or versatilityVSObject-generated harmful factors

Solution Approach 1:

The patent applies preliminary action by pre-setting a radial offset between follower flaps and controlled flaps when the nozzle is at rest. This offset is built into the initial configuration of the control levers and transmission links, so that when the nozzle operates, the flaps automatically align on a common diameter without requiring active compensation during operation.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent changes the geometric parameter of the control lever system by introducing a radial offset between the pivot points of controlled flaps and follower flaps. This parameter modification transforms the kinematic behavior of the mechanism, ensuring that the flaps converge to the same diameter during operation, thereby eliminating leakage paths.

Inventive Principle:
Principle #35Parameter changes

2Object-generated harmful factors

If radial offset is introduced between follower and controlled flaps, then leakage is eliminated and flaps align on common diameter, but the machining complexity of control levers increases

Engineering Contradiction:
Improveleakage between flapsVSAvoidmachining of follower levers
Core Design Contradiction:
Object-generated harmful factorsVSEase of manufacture

Solution Approach 1:

The patent applies local quality by introducing the radial offset only to the follower levers while leaving the controlled levers unchanged. This localized modification means that only specific components (the follower levers and their associated transmission links) require altered machining, rather than redesigning the entire control system. The offset is implemented through modified pivot point positioning or adjusted link lengths in the follower lever assembly.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS7520135B2Variable-section turbomachine nozzle
Publication Date: 2009.04.21 SAFRAN AIRCRAFT ENGINES SAS
  • US7520135B2 patent drawing
  • US7520135B2 patent drawing
  • US7520135B2 patent drawing

AI summary

A variable-section turbomachine nozzle comprises a plurality of moving flaps, and a moving flap control system comprising control levers each associated with a respective moving flap, the control levers comprising both controlled levers that are actuated directly by actuators, and follower levers that are actuated by the controlled levers via transmission links. When the nozzle is at rest, the flaps associated with the follower levers present a radial offset relative to the flaps associated with the controlled levers.