Simplified nozzle supporting device for gas turbine

Simplified nozzle supporting device for gas turbine

  • CN 1,495,339 A
  • Filed: 06/05/2003
  • Published: 05/12/2004
  • Est. Priority Date: 06/05/2002
  • Status: Active Application
First Claim
Patent Images

1. simplification support device (110) that is used for the nozzle (112) of combustion gas turbine level, described support device (110) places the rotor of described gas turbine, be positioned between the upstream blade mounting disc (122) and downstream blade mounting disc (124) of described nozzle (112), and be provided with honey-comb type bubble Sealing (120), the described nozzle (112) of described combustion gas turbine level comprises a circumferential body that is divided into some nozzle segments (112), it is characterized in that:

  • in the support device (110) of described simplification, described honey-comb type bubble Sealing (120) is fixed directly on the described nozzle segment (112).

View all claims
    ×
    ×

    Thank you for your feedback

    ×
    ×