GB884409A - Improvements relating to blades such as axial flow gas turbine blades - Google Patents

Improvements relating to blades such as axial flow gas turbine blades

Info

Publication number
GB884409A
GB884409A GB14219/59A GB1421959A GB884409A GB 884409 A GB884409 A GB 884409A GB 14219/59 A GB14219/59 A GB 14219/59A GB 1421959 A GB1421959 A GB 1421959A GB 884409 A GB884409 A GB 884409A
Authority
GB
United Kingdom
Prior art keywords
blades
cooling fluid
orifices
gas turbine
blade
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
GB14219/59A
Inventor
Thomas Bowmer
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 to DER27825A priority Critical patent/DE1204021B/en
Priority to NL250945D priority patent/NL250945A/xx
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB14219/59A priority patent/GB884409A/en
Priority to FR820843A priority patent/FR1253480A/en
Priority to BE588601A priority patent/BE588601A/en
Priority to CH718060A priority patent/CH384943A/en
Publication of GB884409A publication Critical patent/GB884409A/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
    • F01D5/187—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)

Abstract

884,409. Turbine blades. ROLLS-ROYCE Ltd. April 19, 1960 [April 27, 1959], No. 14219/59. Class 110 (3). A turbine blade has a duct therein adapted to be supplied with cooling fluid which passes in streams from the duct through a plurality of slots in the blade arranged so that the streams intermingle over the external surface. In the hollow gas turbine inlet guide vane, Fig. 2, cooling fluid enters a tube 25 disposed forwardly of a dividing wall 22 and issues in a jet from an aperture 30 to strike the internal surface of the vane at the centre of the leading edge where the peak temperature occurs. The coolant subsequently passes to the rear chamber and issues from the orifices 29. In other embodiments some of the cooling fluid is allowed to escape through apertures in the leading edge of the blade as well a through orifices corresponding to the orifices 29.
GB14219/59A 1959-04-27 1959-04-27 Improvements relating to blades such as axial flow gas turbine blades Expired GB884409A (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
DER27825A DE1204021B (en) 1959-04-27 Blade for axial flow machines, especially gas turbines
NL250945D NL250945A (en) 1959-04-27
GB14219/59A GB884409A (en) 1959-04-27 1959-04-27 Improvements relating to blades such as axial flow gas turbine blades
FR820843A FR1253480A (en) 1959-04-27 1960-03-09 Improvements to blades, fins and similar turbine parts
BE588601A BE588601A (en) 1959-04-27 1960-03-14 Improvements to blades, vanes and similar turbine elements.
CH718060A CH384943A (en) 1959-04-27 1960-06-24 Blade for a turbo machine

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
GB884409A true GB884409A (en) 1961-12-13

Family

ID=39576466

Family Applications (1)

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

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)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1210254B (en) * 1962-03-26 1966-02-03 Rolls Royce Gas turbine engine with cooled turbine blades
DE1210253B (en) * 1961-05-02 1966-02-03 Rolls Royce Blade for flow machines, especially for gas turbines
DE1280618B (en) * 1964-12-02 1968-10-17 Rolls Royce Double-walled guide vane for gas turbine engines
GB2365079A (en) * 2000-07-29 2002-02-13 Rolls Royce Plc Turbine blade platform cooling
EP1571296A1 (en) * 2004-03-01 2005-09-07 Alstom Technology Ltd Cooled blade of a turbomachine and method of cooling

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB960071A (en) * 1961-08-30 1964-06-10 Rolls Royce Improvements relating to cooled blades such as axial flow gas turbine blades
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
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
NL86599C (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

Cited By (7)

* 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
DE1210254B (en) * 1962-03-26 1966-02-03 Rolls Royce Gas turbine engine with cooled turbine blades
DE1280618B (en) * 1964-12-02 1968-10-17 Rolls Royce Double-walled guide vane for gas turbine engines
GB2365079A (en) * 2000-07-29 2002-02-13 Rolls Royce Plc Turbine blade platform cooling
US6506020B2 (en) 2000-07-29 2003-01-14 Rolls-Royce Plc Blade platform cooling
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

Also Published As

Publication number Publication date
NL250945A (en)
CH384943A (en) 1965-02-26
BE588601A (en) 1960-07-01
FR1253480A (en) 1961-02-10
DE1204021B (en) 1965-10-28

Similar Documents

Publication Publication Date Title
GB925388A (en) Improvements relating to turbine nozzle vane mounting means
GB895077A (en) Blades for fluid flow machines such as axial flow turbines
GB853328A (en) Method of and device for cooling the component elements of machines
GB695482A (en) Improvements in or relating to gas-turbine engines
GB884409A (en) Improvements relating to blades such as axial flow gas turbine blades
GB1034260A (en) Aerofoil-shaped blade for use in a fluid flow machine
GB1151177A (en) Improvements in and relating to Gas Turbine Engines
GB587513A (en) Improvements relating to gas turbine cooling systems
GB938247A (en) Gas turbine engine having cooled turbine blading
GB1524956A (en) Gas tubine engine
GB1027415A (en) Jet propulsion engine
GB922069A (en) Combustion chamber for a gas turbine engine
GB1193587A (en) Nozzle Guide Vanes for Gas Turbine Engines.
GB1070130A (en) Aeofoil shaped blade for a fluid flow machine such as a gas turbine engine
GB579316A (en) Improvements in gas turbines, axial flow or turbine type gas compressors and the like machines
GB1070480A (en) Aerofoil shaped blade for a fluid flow machine such as a gas turbine engine
GB861632A (en) Method and apparatus for cooling a member such, for example, as a turbine blade of agas turbine engine
GB641146A (en) Improvements in turbine blades
GB627396A (en) Improvements in or relating to aircraft gas-turbine power-plant installations
GB766883A (en) Improvements relating to gas turbines
GB664628A (en) Improvements in or relating to cooled rotors for gas turbines
GB737081A (en) Improvements relating to jet propulsion engines
GB861101A (en) Combination power plant for an aircraft
GB1041048A (en) Improvements in aircraft having jet-propulsion power-plants
GB701320A (en) Improvements in or relating to combustion equipment of gas-turbine engines