AT291677T

Turbine blade with a hot gas suporting platform and a mechanical load suporting platform

Abstract

The invention claims a turbine blade (1), wherein a integrally formed; the blade of the blade axis (4) extended (2). To be is a high heat high-load mechanical and load at the same time, wherein the edges are ensure consumption of the coolant economic; based on the invention, (8) is formed with in a blade (2) is transversely (12) and hot working medium platform (12) on the hot working medium platform of the blade axis (4) of the bearing platform (14); the bearing platform (14) (12) is (2) and solderless joint through the blade between the hot working medium bed.

Term

No projected expiry on record.

  1. Priority and filed
  2. Granted
  3. Today

11 members in 6 offices

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Members11

Family members, oldest first
DocumentOfficeKind
US2003133802A1United States of AmericaA1
EP1329593A1European Patent Office (EPO)A1
JP2003214109AJapanA
CN1436920AChinaA
EP1329593B1European Patent Office (EPO)B1
AT291677TThis recordAustriaT
ATE291677T1AustriaT1
DE50202538D1GermanyD1
US6887040B2United States of AmericaB2
CN1313707CChinaC
JP4249990B2JapanB2