CH384943A - Blade for a turbo machine - Google Patents

Blade for a turbo machine

Info

Publication number
CH384943A
CH384943A CH718060A CH718060A CH384943A CH 384943 A CH384943 A CH 384943A CH 718060 A CH718060 A CH 718060A CH 718060 A CH718060 A CH 718060A CH 384943 A CH384943 A CH 384943A
Authority
CH
Switzerland
Prior art keywords
blade
turbo machine
turbo
machine
Prior art date
Application number
CH718060A
Other languages
German (de)
Inventor
Bowmer Thomas
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH384943A publication Critical patent/CH384943A/en

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
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH718060A 1959-04-27 1960-06-24 Blade for a turbo machine CH384943A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB14219/59A GB884409A (en) 1959-04-27 1959-04-27 Improvements relating to blades such as axial flow gas turbine blades

Publications (1)

Publication Number Publication Date
CH384943A true CH384943A (en) 1965-02-26

Family

ID=39576466

Family Applications (1)

Application Number Title Priority Date Filing Date
CH718060A CH384943A (en) 1959-04-27 1960-06-24 Blade for a turbo machine

Country Status (6)

Country Link
BE (1) BE588601A (en)
CH (1) CH384943A (en)
DE (1) DE1204021B (en)
FR (1) FR1253480A (en)
GB (1) GB884409A (en)
NL (1) NL250945A (en)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1210253B (en) * 1961-05-02 1966-02-03 Rolls Royce Blade for flow machines, especially for gas turbines
GB960071A (en) * 1961-08-30 1964-06-10 Rolls Royce Improvements relating to cooled blades such as axial flow gas turbine blades
DE1210254B (en) * 1962-03-26 1966-02-03 Rolls Royce Gas turbine engine with cooled turbine blades
GB1034260A (en) * 1964-12-02 1966-06-29 Rolls Royce Aerofoil-shaped blade for use in a fluid flow machine
DE3603350A1 (en) * 1986-02-04 1987-08-06 Walter Prof Dipl Ph Sibbertsen METHOD FOR COOLING THERMALLY LOADED COMPONENTS OF FLOWING MACHINES, DEVICE FOR CARRYING OUT THE METHOD AND TRAINING THERMALLY LOADED BLADES
JPS62228603A (en) * 1986-03-31 1987-10-07 Toshiba Corp Gas turbine blade
GB2365079B (en) * 2000-07-29 2004-09-22 Rolls Royce Plc Blade platform cooling
EP1571296A1 (en) * 2004-03-01 2005-09-07 Alstom Technology Ltd Cooled blade of a turbomachine and method of cooling
EP2957724A1 (en) * 2014-06-17 2015-12-23 Siemens Aktiengesellschaft Turbine blade and turbine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH225231A (en) * 1940-11-16 1943-01-15 Sulzer Ag Cooled hollow blade.
CH218976A (en) * 1940-12-24 1942-01-15 Sulzer Ag Gas turbine blade with air film cooling.
DE904610C (en) * 1944-04-22 1954-02-22 Siemens Ag Air-cooled hollow blade for gas turbines, in which the cooling air enters the blade from the blade root
US2858100A (en) * 1952-02-01 1958-10-28 Stalker Dev Company Blade structure for turbines and the like
US2866618A (en) * 1953-02-13 1958-12-30 Thomas W Jackson Reverse flow air cooled turbine blade
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
NL198161A (en) * 1955-06-17
FR1147239A (en) * 1956-03-28 1957-11-20 Improvements to gas turbines
FR1177035A (en) * 1957-05-28 1959-04-20 Snecma Method and device for cooling machine parts

Also Published As

Publication number Publication date
DE1204021B (en) 1965-10-28
BE588601A (en) 1960-07-01
NL250945A (en)
GB884409A (en) 1961-12-13
FR1253480A (en) 1961-02-10

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