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System for sealing a shaft

Inactive Publication Date: 2013-04-18
GENERAL ELECTRIC CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The present invention relates to a system and a gas turbine made with a seal to prevent cooling flow from leaking through a shank pocket. The seal is placed between a rotating component and a stationary component to prevent cooling flow from leaking through a shank pocket and to secure the movement of the seal. The seal comprises an arm and a hook that are shaped to mate with a slot in the airfoil and shank, and an end of the slot is adjacent to the top portion of the mount. This system and gas turbine improve the efficiency and performance of the gas turbine.

Problems solved by technology

In addition, fluid flowing over the platform can leak into the shank pocket.
These sources of “cross-shank” leakage are detrimental to the performance of the turbomachine.

Method used

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  • System for sealing a shaft
  • System for sealing a shaft
  • System for sealing a shaft

Examples

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Embodiment Construction

[0016]One or more specific embodiments of the present invention will be described below. In an effort to provide a concise description of these embodiments, all features of an actual implementation may not be described in the specification. It should be appreciated that in the development of any such actual implementation, as in an engineering or design project, numerous implementation-specific decisions are made to achieve the specific goals, such as compliance with system-related and / or business-related constraints, which may vary from one implementation to another. Moreover, it should be appreciated that such effort might be complex and time consuming, but would nevertheless be a routine undertaking of design, fabrication, and manufacture for those of ordinary skill having the benefit of this disclosure.

[0017]Detailed example embodiments are disclosed herein. However, specific structural and functional details disclosed herein are merely representative for purposes of describing ...

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Abstract

An embodiment of the present invention takes the form of a seal that may substantially reduce cross-shank leakage between components mounted on a shaft. Embodiments of the seal may be connected to a wide variety of rotatable components including, but not limited to, compressor blades, turbine buckets, or the like.

Description

BACKGROUND OF THE INVENTION[0001]The present invention relates to seals for air-ingesting turbomachines; and more particularly to a seal for the shank region of a rotating component of the turbomachine.[0002]Conventional turbomachines includes compressor and turbine sections that each has a plurality of rotating components (compressor blades, turbine components, etc) attached about a circumference of a turbine rotor. Each rotating component is located at a distance away from an adjacent rotating component to allow movement and expansion during operation. Each rotatable component includes: a shank that attaches to the rotor, a platform, and an airfoil that extends radially outwardly from the platform.[0003]The area between the adjacent rotating components is considered the shank pocket. Generally, the cavities between the rotating components and adjacent stationary components forward and aft of the shank pocket are at different operating pressures. Fluid naturally flows from the high...

Claims

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Application Information

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IPC IPC(8): F01D5/30
CPCF01D11/006
Inventor AMARAL, SERGIO DANIEL MARQUESITZEL, GARY MICHAELZHANG, XIUZHANG JAMESMOORE, KENNETH DALE
Owner GENERAL ELECTRIC CO
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