Compliant Shaft Recursive Configuration Turbine Engine
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Solution Overview
Problem
Conventional turbine engine configurations face misalignments between shafts due to operational loads, leading to unfavorable operating conditions and premature failure of components, which are mitigated using multiple separate components like bolted flanges or splines, increasing complexity and weight.
Innovation Solution
A compliant shaft with a flexible body is integrated with the gear box, providing flexibility between the fan and low pressure turbine shafts to prevent misalignments and reduce the need for additional components, thereby reducing complexity and weight.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If multiple separate components (bolted flanges or splines) are used to provide flexibility and prevent misalignments, then reliability is improved, but device complexity and weight increase
Solution Approach 1:
The patent combines multiple separate components (flanges, bolts, splines) into a single integrated compliant shaft assembly. The compliant shaft incorporates flexible sections that provide the necessary compliance and misalignment correction functionality that previously required multiple discrete parts, thereby reducing device complexity while maintaining reliability
Solution Approach 2:
The compliant shaft includes flexible sections with controlled flexibility that allow the shaft to bend and accommodate misalignments. These flexible sections replace rigid connections with compliant ones, enabling the shaft to absorb misalignments without requiring additional corrective components
2Reliability
If multiple separate components (bolted flanges or splines) are used to provide flexibility and prevent misalignments, then reliability is improved, but weight increases
Solution Approach 1:
The patent combines multiple separate components (flanges, bolts, splines) into a single integrated compliant shaft assembly. The compliant shaft incorporates flexible sections that provide the necessary compliance and misalignment correction functionality that previously required multiple discrete parts, thereby reducing device complexity while maintaining reliability
Solution Approach 2:
The compliant shaft includes flexible sections with controlled flexibility that allow the shaft to bend and accommodate misalignments. These flexible sections replace rigid connections with compliant ones, enabling the shaft to absorb misalignments without requiring additional corrective components
3Adaptability or versatility
If a gear box is used to accommodate different rotational speeds, then adaptability is improved, but misalignments occur under operational loads
Solution Approach 1:
The compliant shaft includes flexible sections with controlled flexibility that allow the shaft to bend and accommodate misalignments. These flexible sections replace rigid connections with compliant ones, enabling the shaft to absorb misalignments without requiring additional corrective components
Solution Approach 2:
The compliant shaft transitions from a rigid static connection to a dynamic flexible connection that can adapt its shape under load. The flexible sections allow the shaft to dynamically adjust its configuration to maintain proper alignment between the gear box and turbine shaft under varying operational conditions
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
The compliant shaft effectively prevents misalignments and reduces component wear, eliminating the need for multiple separate components, thus enhancing the operational reliability and reducing the overall weight and complexity of the turbine engine.
Implementation Method 1
at least a portion of the body is flexible
Data Source
AI summary
Embodiments of a compliant shaft for engines are provided herein. In some embodiments, a compliant shaft for a turbine engine may include: a body having a first end configured to be coupled to a shaft of a turbine and a second end coupled to a gear of a gear box, wherein at least a portion of the body is flexible.


