GB1234518A - - Google Patents

Info

Publication number
GB1234518A
GB1234518A GB1234518DA GB1234518A GB 1234518 A GB1234518 A GB 1234518A GB 1234518D A GB1234518D A GB 1234518DA GB 1234518 A GB1234518 A GB 1234518A
Authority
GB
United Kingdom
Prior art keywords
blade
welded
facing
hollow
shroud
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
Other languages
English (en)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Publication of GB1234518A publication Critical patent/GB1234518A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/182—Transpiration cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB1234518D 1968-05-22 1969-05-02 Expired GB1234518A (enExample)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US73100468A 1968-05-22 1968-05-22

Publications (1)

Publication Number Publication Date
GB1234518A true GB1234518A (enExample) 1971-06-03

Family

ID=24937664

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1234518D Expired GB1234518A (enExample) 1968-05-22 1969-05-02

Country Status (2)

Country Link
US (1) US3529902A (enExample)
GB (1) GB1234518A (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3610769A (en) * 1970-06-08 1971-10-05 Gen Motors Corp Porous facing attachment
DE2503285C2 (de) * 1975-01-28 1984-08-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Verfahren zur Herstellung eines einstückigen thermisch hochbeanspruchten gekühlten Bauteils, insbesondere einer Schaufel für Turbinentriebwerke
US4012167A (en) * 1975-10-14 1977-03-15 United Technologies Corporation Turbomachinery vane or blade with cooled platforms
US4017213A (en) * 1975-10-14 1977-04-12 United Technologies Corporation Turbomachinery vane or blade with cooled platforms
GB9224241D0 (en) * 1992-11-19 1993-01-06 Bmw Rolls Royce Gmbh A turbine blade arrangement
US5413458A (en) * 1994-03-29 1995-05-09 United Technologies Corporation Turbine vane with a platform cavity having a double feed for cooling fluid
US7841828B2 (en) * 2006-10-05 2010-11-30 Siemens Energy, Inc. Turbine airfoil with submerged endwall cooling channel
WO2015041963A1 (en) * 2013-09-23 2015-03-26 United Technologies Corporation Cmc airfoil with sharp trailing edge and method of making same

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2774566A (en) * 1947-12-12 1956-12-18 Richardson Edward Adams Fluid cooled permeable turbine blade
US2681788A (en) * 1951-05-23 1954-06-22 Solar Aircraft Co Gas turbine vane structure
GB740909A (en) * 1953-02-02 1955-11-23 Bristol Aeroplane Co Ltd Improvements in or relating to aerofoil blade assemblies
BE557503A (enExample) * 1956-05-15
US3269700A (en) * 1964-12-07 1966-08-30 United Aircraft Corp Heat shield for turbine strut
US3402914A (en) * 1965-02-10 1968-09-24 Curtiss Wright Corp Method of controlling the permeability of a porous material, and turbine blade formed thereby

Also Published As

Publication number Publication date
US3529902A (en) 1970-09-22

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]