发明授权
US5141393A Seal accommodating thermal expansion between adjacent casings in gas turbine engine 失效
密封容纳燃气涡轮发动机相邻壳体之间的热膨胀

Seal accommodating thermal expansion between adjacent casings in gas
turbine engine
摘要:
A casing around a turbine and a casing around discharge nozzles have a concentrically arranged shell portion. The seal contains internal pressure while accommodating eccentric, expansion and axial travel. Arcuate seal segments have one leg sealing against a radial surface extending from the inner shell and the other leg against the outer shell. A linkage guides travel of the segments.
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