Method and system for maintenance of turbomachinery

A turbomachinery and start-up system technology, applied in the field of turbomachinery, can solve problems such as high cost and ineffective maintenance

Inactive Publication Date: 2013-07-24
GENERAL ELECTRIC CO
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the maintenance applied can be ineffective and can be costly

Method used

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  • Method and system for maintenance of turbomachinery
  • Method and system for maintenance of turbomachinery
  • Method and system for maintenance of turbomachinery

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Embodiment Construction

[0015] One or more specific embodiments of the present invention will be described below. In order to provide a concise description of these embodiments, the specification may not describe all the features of the actual implementation. It should be understood that in the process of developing any such actual implementation, such as in any engineering or design project, a variety of implementation-specific determinations must be made to achieve the developer’s specific goals (such as complying with system-related and business-related Constraints), the specific target changes with implementation. In addition, it should be understood that such development work may be complicated and time-consuming, but in any case, it is a routine task of design, processing and manufacturing for those of ordinary skill in the art who benefit from the present invention.

[0016] When introducing elements of various embodiments of the present invention, the articles "a" and "said" are intended to mea...

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Abstract

A method and a system (62) for analysis of turbomachinery are provided. In one embodiment, a system includes a request initiation system (66) configured to initiate a departure request (44) for a turbomachinery. The system further includes a commercial screening system (68) configured to receive the departure request (44) and to derive a commercial evaluation (74) based on the departure request (44). The system also includes a technical evaluation system (76) configured to derive a technical evaluation profile (84) based on the departure request (44). The system additionally includes a request acceptance system (86) configured to derive at maintenance action (92) based on the commercial evaluation (74) and the technical evaluation profile (84), wherein the technical evaluation profile (84) comprises a technical analysis of the turbomachinery.

Description

Technical field [0001] The present invention relates generally to turbomachinery, and more specifically, to methods and systems for maintaining turbomachinery. Background technique [0002] Turbomachines may include devices such as turbines, compressors, or pumps. As the turbomachine operates, efficiency and performance may change over time. This change in performance may be due to various factors such as wear or component damage. Maintenance including replacement of certain turbomachinery components can be applied to turbomachinery to restore efficiency and operating performance. However, the maintenance applied may be ineffective and may be costly. Summary of the invention [0003] This specification will outline certain embodiments consistent with the scope of the originally claimed invention. These embodiments are not intended to limit the scope of the claimed invention, on the contrary, these embodiments are only intended to provide a brief summary of possible forms of th...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/00
CPCF01D21/00
Inventor J.V.保罗夫斯基T.B.贝达B.K.那亚克C.D.希金斯K.P.戈帕兰
Owner GENERAL ELECTRIC CO
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