发明授权
US07007480B2 Multi-axial pivoting combustor liner in gas turbine engine 有权
燃气涡轮发动机中的多轴旋转燃烧器衬套

Multi-axial pivoting combustor liner in gas turbine engine
摘要:
A multi-axial pivoting liner within the combustion system of a turbine engine allows the system to work with minimum thermal interference, especially during system operation at transient conditions, by allowing the liner to pivot and slide about its centerline and relative to the turbine scroll. The pivoting liner has the ability to control and minimize air leakage from part to part, for example, from the liner to the turbine scroll and liner to the surrounding structures, during various operating conditions. Additionally, the liner provides for easy assembly with no flow path steps. Finally, the pivoting liner tolerates thermal and mechanical stresses and minimizes thermal wear.
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