Interstage seal assembly for gas turbine engine
AssigneeSiemens Energy, Inc.
InventorsMahesh Janarthanan, Jeffrey A. Kain, Mushtaq Kazi
Life of this patent
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AssigneeSiemens Energy, Inc.
InventorsMahesh Janarthanan, Jeffrey A. Kain, Mushtaq Kazi
Estimating the term…
A seal assembly is provided for a turbine engine and includes an annular labyrinth seal holder supported on a radially inner end of vanes A plurality of radially extending labyrinth seal elements are supported on the labyrinth seal holder, and a brush seal assembly is supported to the labyrinth seal holder downstream from the labyrinth seal elements. The brush seal assembly includes a brush seal holder and a brush seal located adjacent to an axially rearward one of the rotor arms. The brush seal holder is attached to an axially facing surface of the labyrinth seal holder. A seal plate defining a detachable labyrinth seal element extends radially inward from the axially facing surface of the labyrinth seal holder to the rearward rotor arm at a location upstream of the brush seal.
A seal assembly for a turbine engine including adjacent upstream and downstream rotating rotor disks supporting respective rows of blades, a row of stationary vanes located between said rows of blades, and an axially extending rotor arm supported on each said rotor disk and located radially inward from said blades, the seal assembly comprising:
A seal assembly for a turbine engine including adjacent upstream and downstream rotating rotor disks supporting respective rows of blades, a row of stationary vanes located between said rows of blades, and axially extending forward and rearward rotor arms supported on said upstream and downstream rotor disks, respectively, and located radially inward from said blades, the seal assembly comprising:
Dependencies are inferred from the claim text.