FR1154121A - Perfectionnements à la fabrication d'ailettes pour turbines à gaz - Google Patents

Perfectionnements à la fabrication d'ailettes pour turbines à gaz

Info

Publication number
FR1154121A
FR1154121A FR1154121DA FR1154121A FR 1154121 A FR1154121 A FR 1154121A FR 1154121D A FR1154121D A FR 1154121DA FR 1154121 A FR1154121 A FR 1154121A
Authority
FR
France
Prior art keywords
fins
manufacture
gas turbines
turbines
gas
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)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bristol Aeroplane Co Ltd
Original Assignee
Bristol Aeroplane Co Ltd
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
Priority claimed from GB1546455A external-priority patent/GB817660A/en
Application filed by Bristol Aeroplane Co Ltd filed Critical Bristol Aeroplane Co Ltd
Application granted granted Critical
Publication of FR1154121A publication Critical patent/FR1154121A/fr
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
    • F01D5/187—Convection cooling
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/02—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
    • 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
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • Y10T29/49341—Hollow blade with cooling passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Forging (AREA)
FR1154121D 1955-05-27 1956-05-25 Perfectionnements à la fabrication d'ailettes pour turbines à gaz Expired FR1154121A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1546455A GB817660A (en) 1955-05-27 Improvements in or relating to blades for gas turbines

Publications (1)

Publication Number Publication Date
FR1154121A true FR1154121A (fr) 1958-04-02

Family

ID=10059589

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1154121D Expired FR1154121A (fr) 1955-05-27 1956-05-25 Perfectionnements à la fabrication d'ailettes pour turbines à gaz

Country Status (2)

Country Link
US (1) US2830357A (fr)
FR (1) FR1154121A (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3079681A (en) * 1956-01-18 1963-03-05 Fentiman & Sons Ltd F Method of making a joint
GB879981A (en) * 1956-09-13 1961-10-11 Wiggin & Co Ltd Henry Improvements in and relating to hollow turbine blades
FR1184195A (fr) * 1956-10-12 1959-07-17 Rolls Royce Fabrication par extrusion d'aubes de turbine
US2944327A (en) * 1956-10-17 1960-07-12 Curtiss Wright Corp Method of making hollow blades for turbine engines
US2965955A (en) * 1956-10-23 1960-12-27 Int Nickel Co Production of hollow turbine blades
GB846277A (en) * 1956-11-20 1960-08-31 Rolls Royce Turbine and compressor blades
US3039178A (en) * 1957-01-11 1962-06-19 Rolls Royce Manufacture by extrusion of turbine engine blades
US2972807A (en) * 1957-02-19 1961-02-28 Int Nickel Co Method of making hollow turbine or compressor blades
US2972182A (en) * 1957-02-22 1961-02-21 Rolls Royce Turbine and compressor blades
US2985953A (en) * 1957-12-13 1961-05-30 Rolls Royce Manufacture of blades of internal combustion turbine engines
US3107416A (en) * 1958-05-20 1963-10-22 Int Nickel Co Method of making turbine and compressor blades
US3066910A (en) * 1958-07-09 1962-12-04 Thompson Ramo Wooldridge Inc Cooled turbine blade
EP1730389B1 (fr) * 2004-03-30 2009-12-09 Alstom Technology Ltd Dispositif pour alimenter une aube en air de refroidissement

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB572916A (en) * 1944-04-18 1945-10-29 Armstrong Siddeley Motors Ltd Securing projections to a rotor
US2613058A (en) * 1945-11-30 1952-10-07 Atkinson Joseph Cooled bladed rotor
US2699917A (en) * 1946-08-24 1955-01-18 Thompson Prod Inc Turbine wheel and blade construction
US2684831A (en) * 1947-11-28 1954-07-27 Power Jets Res & Dev Ltd Turbine and like rotor
US2656146A (en) * 1948-04-08 1953-10-20 Curtiss Wright Corp Turbine blade construction

Also Published As

Publication number Publication date
US2830357A (en) 1958-04-15

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