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Sealing system for a turbomachine

  • US 4,193,603 A
  • Filed: 12/21/1978
  • Issued: 03/18/1980
  • Est. Priority Date: 12/21/1978
  • Status: Expired due to Term
First Claim
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1. A seal system for a turbomachine comprising:

  • a first pressure reducing seal for reducing the pressure of a process fluid flowing therethrough;

    first conduit means for delivering a first portion of the fluid to a first relatively low pressure operating region;

    second conduit means for delivering a second portion of the fluid to a sealing region operating at a pressure somewhat higher than the pressure of the first operating region;

    a second pressure reducing seal in fluid flow communication with the sealing region and a second operating region having a pressure intermediate the sealing region and the first operating region; and

    flow regulating means for selectively regulating the flow of fluid between the sealing region and the first operating region to maintain the fluid pressure differential between the sealing region and the second operating region at a substantially predetermined magnitude.

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