CH562392A5 - - Google Patents

Info

Publication number
CH562392A5
CH562392A5 CH1635772A CH1635772A CH562392A5 CH 562392 A5 CH562392 A5 CH 562392A5 CH 1635772 A CH1635772 A CH 1635772A CH 1635772 A CH1635772 A CH 1635772A CH 562392 A5 CH562392 A5 CH 562392A5
Authority
CH
Switzerland
Application number
CH1635772A
Original Assignee
Penny Robert Noel
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 by Penny Robert Noel filed Critical Penny Robert Noel
Publication of CH562392A5 publication Critical patent/CH562392A5/xx

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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/021—Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH1635772A 1971-11-10 1972-11-09 CH562392A5 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5213371A GB1386590A (en) 1971-11-10 1971-11-10 Turbine rotor

Publications (1)

Publication Number Publication Date
CH562392A5 true CH562392A5 (de) 1975-05-30

Family

ID=10462762

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1635772A CH562392A5 (de) 1971-11-10 1972-11-09

Country Status (11)

Country Link
US (1) US3873234A (de)
JP (1) JPS5514242B2 (de)
AU (1) AU469736B2 (de)
BE (1) BE791162A (de)
CA (1) CA962601A (de)
CH (1) CH562392A5 (de)
DE (1) DE2254829A1 (de)
FR (1) FR2159460B1 (de)
GB (1) GB1386590A (de)
IT (1) IT975686B (de)
NL (1) NL7215255A (de)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4097276A (en) * 1975-07-17 1978-06-27 The Garrett Corporation Low cost, high temperature turbine wheel and method of making the same
DE2816791C3 (de) * 1977-05-03 1981-05-07 Vereinigte Edelstahlwerke Ag (Vew), Wien Gekühlter Läufer für eine axial durchströmte Turbine
US4236869A (en) * 1977-12-27 1980-12-02 United Technologies Corporation Gas turbine engine having bleed apparatus with dynamic pressure recovery
US4302148A (en) * 1979-01-02 1981-11-24 Rolls-Royce Limited Gas turbine engine having a cooled turbine
GB2057573A (en) * 1979-08-30 1981-04-01 Rolls Royce Turbine rotor assembly
US4335997A (en) * 1980-01-16 1982-06-22 General Motors Corporation Stress resistant hybrid radial turbine wheel
US4595340A (en) * 1984-07-30 1986-06-17 General Electric Company Gas turbine bladed disk assembly
US4864706A (en) * 1987-08-12 1989-09-12 United Technologies Corporation Fabrication of dual alloy integrally bladed rotors
US5106266A (en) * 1989-07-25 1992-04-21 Allied-Signal Inc. Dual alloy turbine blade
GB2239491B (en) * 1989-11-28 1993-09-29 Copermill Ltd Hot gas blower
FR2661946B1 (fr) * 1990-05-14 1994-06-10 Alsthom Gec Etage de turbine a action avec pertes secondaires reduites.
US5113583A (en) * 1990-09-14 1992-05-19 United Technologies Corporation Integrally bladed rotor fabrication
US5109606A (en) * 1991-03-04 1992-05-05 United Technologies Corporation Integrally bladed rotor fabrication or repair
US5197190A (en) * 1991-03-04 1993-03-30 United Technologies Corporation Fabrication of repair method for an integrally bladed rotor
JP3337393B2 (ja) * 1997-04-23 2002-10-21 三菱重工業株式会社 ガスタービン冷却動翼
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil
DE19854908A1 (de) * 1998-11-27 2000-05-31 Rolls Royce Deutschland Schaufel und Laufscheibe einer Strömungsmaschine
EP1426553A1 (de) * 2002-12-03 2004-06-09 Techspace Aero S.A. Gewichtsreduktion in Rotorschaufeln
DE102006013557B4 (de) * 2005-03-30 2015-09-24 Alstom Technology Ltd. Rotor für eine Dampfturbine
EP1724442A1 (de) * 2005-05-18 2006-11-22 Siemens Aktiengesellschaft Schaufelfuss für Turbinenschaufel
US7488157B2 (en) * 2006-07-27 2009-02-10 Siemens Energy, Inc. Turbine vane with removable platform inserts
US7581924B2 (en) * 2006-07-27 2009-09-01 Siemens Energy, Inc. Turbine vanes with airfoil-proximate cooling seam
US20090092494A1 (en) * 2007-10-04 2009-04-09 General Electric Company Disk rotor and method of manufacture
US8096758B2 (en) * 2008-09-03 2012-01-17 Siemens Energy, Inc. Circumferential shroud inserts for a gas turbine vane platform
US8935926B2 (en) 2010-10-28 2015-01-20 United Technologies Corporation Centrifugal compressor with bleed flow splitter for a gas turbine engine
US9366146B2 (en) * 2013-06-11 2016-06-14 General Electric Company Closure bucket for turbo-machine
DE102013220983A1 (de) * 2013-10-16 2015-04-16 MTU Aero Engines AG Laufschaufel für eine Turbomaschine
FR3014942B1 (fr) * 2013-12-18 2016-01-08 Snecma Aube, roue a aubes et turbomachine ; procede de fabrication de l'aube
US10458257B2 (en) * 2013-12-23 2019-10-29 Safran Aircraft Engines Blade comprising a shank, provided with a depressed portion
US10641113B2 (en) * 2015-04-08 2020-05-05 United Technologies Corporation Airfoils
EP3945033B1 (de) * 2020-07-27 2022-09-07 Airbus Operations (S.A.S.) Flugzeugantriebseinheit

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2448825A (en) * 1944-03-20 1948-09-07 Lockheed Aircraft Corp Turbine rotor
US2750147A (en) * 1947-10-28 1956-06-12 Power Jets Res & Dev Ltd Blading for turbines and like machines
BE530136A (de) * 1953-07-06
GB1053420A (de) * 1964-08-11
GB1040825A (en) * 1965-04-20 1966-09-01 Rolls Royce Improvements in rotor blades and/or stator blades for gas turbine engines
GB1266505A (de) * 1968-09-17 1972-03-08
GB1268911A (en) * 1969-09-26 1972-03-29 Rolls Royce Improvements in or relating to blades
US3635586A (en) * 1970-04-06 1972-01-18 Rolls Royce Method and apparatus for turbine blade cooling
US3661475A (en) * 1970-04-30 1972-05-09 Gen Electric Turbomachinery rotors
US3664766A (en) * 1970-06-01 1972-05-23 Ford Motor Co Turbine wheel
US3610769A (en) * 1970-06-08 1971-10-05 Gen Motors Corp Porous facing attachment
GB1302661A (de) * 1970-07-27 1973-01-10

Also Published As

Publication number Publication date
CA962601A (en) 1975-02-11
US3873234A (en) 1975-03-25
JPS5514242B2 (de) 1980-04-15
AU469736B2 (en) 1976-02-26
GB1386590A (en) 1975-03-12
FR2159460A1 (de) 1973-06-22
DE2254829A1 (de) 1973-05-17
IT975686B (it) 1974-08-10
NL7215255A (de) 1973-05-14
JPS49132406A (de) 1974-12-19
FR2159460B1 (de) 1977-09-02
BE791162A (fr) 1973-03-01
AU4867272A (en) 1974-05-09

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Legal Events

Date Code Title Description
PL Patent ceased
PL Patent ceased