Thermally Protected Seal Assembly for Turbine Engines
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Solution Overview
Problem
Turbine engine seals face challenges in sealing against leakage and accommodating relative movement and high temperatures, while also needing to withstand wear and vibration, due to thermal displacement and temperature differentials.
Innovation Solution
A thermally protected seal assembly featuring a convoluted seal with a porous, compliant shield that extends circumferentially between annular surfaces, including cooling fluid flow and a lip ring for thermal isolation, to minimize wear and enhance durability.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If a seal is placed in a high-temperature environment to seal gaps between turbine engine parts, then sealing effectiveness is improved, but thermal exposure and wear increase
Solution Approach 1:
A shield member is introduced as an intermediary component between the seal and the hot gas path. The shield blocks direct thermal exposure to the seal while allowing the seal to maintain its sealing function against the rotating and stationary surfaces. This mediator protects the seal from harmful thermal effects without compromising sealing effectiveness.
Solution Approach 2:
The seal assembly uses different materials with specific properties for different components: the seal is made of a material suitable for sealing contact, while the shield is made of a heat-resistant material capable of withstanding high temperatures. This local differentiation of material properties allows each component to optimize its function in its specific operational environment.
2Reliability
If a seal is compressed between surfaces to prevent leakage, then sealing integrity is improved, but wear from relative movement increases
Solution Approach 1:
The shield acts as a protective intermediary that absorbs wear and thermal exposure, allowing the seal to maintain its compressed sealing state without direct contact with the harshest environmental factors. This extends the service life of the seal while maintaining sealing integrity.
Solution Approach 2:
The shield is positioned in advance to protect the seal from wear and thermal damage before the seal degrades. This preventive protection allows the seal to operate in its optimal sealing state for an extended duration without direct exposure to damaging conditions.
3Adaptability or versatility
If a seal accommodates relative movement between parts, then adaptability is improved, but wear and vibration increase
Solution Approach 1:
The shield serves as a mediator that allows the seal to accommodate relative movement between rotating and stationary surfaces while protecting the seal from the full impact of wear and vibration. The shield absorbs some of the mechanical stress and thermal exposure.
Solution Approach 2:
The seal uses a flexible, convoluted geometry with bends and members that can deform and adapt to relative movement between surfaces. This flexibility allows the seal to maintain contact and sealing effectiveness while accommodating thermal expansion and mechanical displacement.
4Adaptability or versatility
If a seal is made resilient to accommodate movement, then adaptability is improved, but seal wear increases
Solution Approach 1:
The shield protects the resilient seal material from direct wear and thermal degradation, allowing the seal to maintain its resilient properties and adaptability over an extended service life. The shield acts as a sacrificial or protective element that preserves the seal's functional properties.
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 solution effectively reduces seal wear and thermal exposure, maintaining sealing integrity and durability under high-temperature and vibration conditions, while allowing for relative movement and thermal expansion.
Implementation Method 1
the shield is porous
Implementation Method 2
a seal resiliently compressed between the first and second surfaces
Implementation Method 3
temperature differentials that cause thermal displacement
Data Source
AI summary
A seal assembly that may be for turbine engine includes first and second rings with a convoluted seal resiliently compressed there-between. The seal may define a gap for receipt of a thermally resistant shield that may also reduce wear of the seal. The seal may include a hole for the flow of cooling air and the shield may be porous so as not to obstruct the cooling air flow for cooling of the seal.


