Gas turbine including sealing band and anti-rotation device
AssigneeSiemens Energy, Inc.
InventorsDavid J. Mitchell, Michael J. Olejarski, Christopher J. Muller
Life of this patent
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AssigneeSiemens Energy, Inc.
InventorsDavid J. Mitchell, Michael J. Olejarski, Christopher J. Muller
Estimating the term…
A turbine is provided comprising a plurality of stages, each stage comprising a rotatable disk and blades carried thereby, at least one pair of adjacent rotatable disks defining an annular gap therebetween and having respective opposing sealing band receiving slots aligned with the annular gap A sealing band is located in the opposing receiving slots to seal the annular gap Disk engagement structure is defined in the pair of adjacent rotatable disks. A clip member is coupled to the sealing band and engaged with the pair of adjacent rotatable disks through the disk engagement structure The clip member may have an aperture extending only partially through the clip member for alignment with a hole in the sealing band for engagement with a tool To improve weld geometry, the clip member may have angled surfaces and notched areas, and the sealing band may have chamfered edges.
A turbine comprising:
A turbine comprising:
A process for coupling a clip member to a sealing band located in opposing sealing band receiving slots of a pair of adjacent rotatable disks of a turbine, the clip comprising a U-shaped member having first and second legs and a center portion provided with an aperture extending only part way through the clip member, the sealing band comprising a hole located between axially spaced-apart first and second edges of the sealing band, the process comprising:
Dependencies are inferred from the claim text.