Variable Pitch Airfoil Assembly With Balancing Insert for Vibration Stress
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Solution Overview
Problem
Turbine engines with variable pitch airfoils experience unbalance and vibration stresses due to the movement of the center of mass during operation, which can lead to mechanical stress and inefficiencies.
Innovation Solution
Incorporation of a balancing insert within the airfoil assembly, which balances the airfoil assembly by reducing unbalance and vibration stresses, ensuring consistent balance even with pitch variations.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If a variable pitch airfoil assembly is used to adjust fluid flow, then adaptability is improved, but unbalance and vibration stresses increase
Solution Approach 1:
A balancing insert is provided within the airfoil assembly to counterbalance the variable pitch airfoil assembly during rotation. The balancing insert offsets the unbalance caused by pitch variations, reducing vibration stresses and harmful forces while maintaining the adaptability of pitch adjustment.
2Adaptability or versatility
If pitch variation is increased to enhance performance, then adaptability is improved, but mechanical stress increases
Solution Approach 1:
The balancing insert acts as a counterweight that compensates for the mechanical stress and unbalance generated during pitch variations. This allows the airfoil assembly to operate through a wider pitch range without excessive mechanical stress on the structure.
3Adaptability or versatility
If variable pitch mechanism is added to adjust flow, then adaptability is improved, but device complexity increases
Solution Approach 1:
The balancing insert provides a relatively simple counterweight mechanism that addresses the complexity issue. By adding this single balancing component, the system achieves pitch adjustment capability without proportionally increasing overall device complexity, as the insert integrates into the existing airfoil assembly structure.
Data Source
AI summary
A turbine engine comprising a fan section, a compressor section, a combustion section, and a turbine section in serial flow arrangement and defining a stator portion and a rotor portion, which rotates about an engine centerline. The rotor portion comprising a variable pitch airfoil assembly. The variable pitch airfoil assembly having an airfoil and a balancing insert.


