Double Bellows Valve for Fail-Open Turbine Cooling Airflow
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Solution Overview
Problem
Valves in gas turbine engines can fail in undesirable positions, leading to undercooling or other undesirable effects in the turbine due to the inability to control cooling air effectively.
Innovation Solution
A double bellows valve design that ensures the valve remains in an open position by default, even in the event of failure, using a first and second bellows system to maintain airflow to the turbine, preventing failure in the closed position and ensuring continuous cooling.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a single bellows valve is used to control cooling air flow, then the device complexity is reduced, but the reliability deteriorates because the valve may fail in either open or closed position
Solution Approach 1:
The single bellows valve is divided into two separate bellows: a first bellows and a second bellows. Each bellows is responsible for controlling the valve stem position independently. This segmentation ensures that even if one bellows fails, the other can maintain the valve in the desired open position, thereby improving reliability without requiring a completely complex redundant system.
Solution Approach 2:
The dual bellows configuration provides a built-in fail-safe mechanism. The second bellows acts as a backup that can compensate for potential failures in the first bellows. This beforehand cushioning approach ensures that the valve will not fail in an undesirable closed position, as the second bellows can maintain airflow and keep the valve open even when the first bellows fails.
2Object-affected harmful factors
If the valve is designed to fail closed for safety, then harmful factors are reduced, but the productivity deteriorates due to turbine undercooling
Solution Approach 1:
Instead of designing the valve to fail closed (traditional safety approach), this invention inverts the fail-safe logic by designing the dual bellows system to ensure the valve fails open. The second bellows acts as a backup that maintains the open position even when the first bellows fails, ensuring continuous cooling airflow to the turbine and preventing productivity loss from undercooling.
Solution Approach 2:
The potential harm of valve failure is converted into a benefit through the dual bellows design. What would traditionally be a harmful failure mode (valve closing) is transformed into a beneficial fail-open behavior where the second bellows ensures continuous airflow, turning a potential safety issue into a reliability advantage that maintains both safety and productivity.
3Reliability
If a redundant bellows system is implemented to prevent failure, then reliability is improved, but the device complexity increases
Solution Approach 1:
The redundant actuator system is segmented into two independent but cooperative bellows. Each bellows is a simple, well-understood component that can be manufactured and maintained with existing technology. This segmentation allows the system to achieve high reliability through redundancy while keeping individual components simple and the overall architecture manageable.
Solution Approach 2:
The two bellows are merged into a single integrated actuator assembly that works together to control the valve stem. This merging approach consolidates the redundant components into a unified structure, reducing the overall system complexity compared to having completely separate backup systems. The bellows share common mounting and control mechanisms, simplifying installation and maintenance.
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 double bellows valve design guarantees continuous airflow to the turbine, preventing undercooling and ensuring reliable operation by maintaining the valve in an open position even if components fail, thus enhancing the engine's performance and safety.
Implementation Method 1
The actuator may include a first bellows coupled with the valve stem to define a working fluid chamber and a second bellows coupled with the valve stem and the valve body to define a supply fluid chamber
Data Source
AI summary
A gas turbine engine includes a combustor and a valve coupled to the combustor. The valve includes a valve body, a valve stem, and an actuator. The valve body is formed to define an air chamber. The valve stem is movable between a closed position and an open position. The actuator is configured to move selectively the valve stem between the closed position and the open position.


