一种用于燃气轮机燃烧室密封件结构
By designing a gap structure in the inner and outer rings of the gas turbine combustion chamber seal, the rigidity of the seal is enhanced, solving the problems of easy deformation and vibration of the seal, and achieving higher sealing performance and durability.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- HARBIN ELECTRIC POWER GENERATION EQUIP NAT ENG RES CENT CO LTD
- Filing Date
- 2024-11-26
- Publication Date
- 2026-07-17
AI Technical Summary
Flexible spring clamp seals are prone to deformation and vibration in gas turbine combustion chambers due to insufficient rigidity, leading to seal failure and affecting the temperature and safety of combustion chamber components.
A gas turbine combustion chamber sealing structure is designed, which adopts a concentric fit between the inner and outer rings of the sealing element, with gaps evenly distributed on the inner and outer rings. The gaps are overlapping and staggered in multiples. The gaps on the outer ring are non-through gaps, while the gaps on the inner ring are partially through gaps. They are connected by welding holes to enhance the rigidity of the sealing element.
Increase the rigidity of the seals, reduce vibration and deformation, extend the life of the seals, reduce the risk in high-temperature areas, and ensure the effectiveness of the cooling airflow channels.
Smart Images
Figure CN119412727B_ABST