Frame Segment Cooling Duct for Turbine Interface Sealing
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Solution Overview
Problem
Existing gas turbine transition piece and turbine interface designs face challenges with effective sealing and cooling, leading to leakage and inefficient use of cooling gas, which results in power losses, efficiency issues, and increased emissions due to uncontrolled cooling gas flows.
Innovation Solution
A frame segment with a picture frame receptacle and integrated cooling gas ducts, including effusion cooling holes and a heat shield, is designed to axially receive the transition piece, separating sealing from cooling requirements, thereby minimizing leakage and ensuring reliable cooling across all operating conditions.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If sealed slots are used to allow movement between transition piece and support frame, then movement is enabled, but sealing effectiveness deteriorates and cooling gas leakage increases
Solution Approach 1:
The support frame is divided into modular segments that can move independently relative to the transition piece, while each segment maintains its own sealing and cooling system. This segmentation allows movement to be decoupled from the sealing system, preventing leakage while maintaining adaptability.
Solution Approach 2:
A sealing medium is introduced as an intermediary element between the moving transition piece and support frame. This sealing medium fills the gap created by movement, maintaining effective sealing and preventing cooling gas leakage while allowing the necessary relative motion between components.
2Temperature
If cooling gas is used to cool the support frame, then cooling is achieved, but uncontrolled flows increase emissions
Solution Approach 1:
The cooling gas system incorporates feedback control mechanisms that monitor cooling gas flow and temperature conditions. This feedback control optimizes cooling gas usage, maintaining effective cooling while preventing uncontrolled flows that would increase emissions. The system adjusts cooling gas flow based on actual thermal conditions.
3Adaptability or versatility
If transition piece and support frame are made of different materials, then material properties are optimized, but thermal growth mismatch increases
Solution Approach 1:
The connection between the transition piece and support frame is designed to be dynamic rather than rigid. This dynamic connection accommodates the different thermal expansion rates of the various materials used, allowing each component to grow thermally at its own rate without creating excessive stress or misalignment.
4Stability of the object's composition
If relative movement is allowed between components, then thermal growth is accommodated, but dynamic pulsations increase
Solution Approach 1:
The design incorporates damping elements and cushioning features that are built into the connection structure between the transition piece and support frame. These elements are designed beforehand to absorb and dampen the dynamic pulsations that arise from relative movement, reducing the harmful effects of vibration and pulsation while still allowing necessary thermal growth accommodation.
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
This design enhances sealing, reduces dynamic pulsations, increases the lifetime of components, and minimizes power and efficiency losses by optimizing cooling gas usage and reducing emissions.
Implementation Method 1
the vertical web comprises a cooling gas duct for cooling the vertical web. Typically it is also supplying cooling gas to the downstream face of the vertical web
Implementation Method 2
the downstream face of the vertical web is exposed to hot gases during operation of the gas turbine
Data Source
AI summary
The disclosure relates Frame segment for a transition piece-turbine interface having a picture frame receptacle for axially receiving an aft end of a combustor transition piece. The frame segment can include an I-beam with an upper horizontal element, a lower horizontal element, and a vertical web, wherein the upper horizontal element has mounting face for fixation to a vane carrier. The vertical web has a downstream face, facing towards a first stage of a turbine when installed in a gas turbine. The vertical web includes a cooling gas duct for supplying cooling gas to the downstream face of the vertical web.


