GB741508A - Air cooled turbine blade - Google Patents

Air cooled turbine blade

Info

Publication number
GB741508A
GB741508A GB1929753A GB1929753A GB741508A GB 741508 A GB741508 A GB 741508A GB 1929753 A GB1929753 A GB 1929753A GB 1929753 A GB1929753 A GB 1929753A GB 741508 A GB741508 A GB 741508A
Authority
GB
United Kingdom
Prior art keywords
blade
parts
root
united
boss
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
GB1929753A
Inventor
Horace Sinclair Rainbow
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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 to BE530261D priority Critical patent/BE530261A/xx
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB1929753A priority patent/GB741508A/en
Priority to FR1106326D priority patent/FR1106326A/en
Publication of GB741508A publication Critical patent/GB741508A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

741,508. Turbine blades. ARMSTRONG SIDDELEY MOTORS, Ltd. June 18, 1954 [July 11, 1953], No. 19297/53. Class 110(3) An air-cooled turbine rotor or stator blade of a gas turbine engine is formed of two parts 34, 35, one 34 constituting the concave surface of the blade and the other 35 the convex surface, and each part is formed with internal ribs 37. 38 which are subsequently permanently united to one another to provide internal cooling passages. Each of the blade parts may also be formed integrally with a portion of the root, the root portions also being permanently united to one another. The two blade parts are shaped so as to provide a shallow internal chamber 16 at the root end of the blade to which cooling air is supplied through ducts 20, 21. The blade shown in Figs. 1, 2 and 3 is a rotor blade whereas that in Fig. 8 is a stator blade, the the root end of which is formed with flanges 26, 27 and a boss 28, a hole 29 for a securing bolt being provided through the flanges and boss. 'The parts may be united by brazing.
GB1929753A 1953-07-11 1953-07-11 Air cooled turbine blade Expired GB741508A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
BE530261D BE530261A (en) 1953-07-11
GB1929753A GB741508A (en) 1953-07-11 1953-07-11 Air cooled turbine blade
FR1106326D FR1106326A (en) 1953-07-11 1954-06-28 Air-cooled turbine blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1929753A GB741508A (en) 1953-07-11 1953-07-11 Air cooled turbine blade

Publications (1)

Publication Number Publication Date
GB741508A true GB741508A (en) 1955-12-07

Family

ID=10127057

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1929753A Expired GB741508A (en) 1953-07-11 1953-07-11 Air cooled turbine blade

Country Status (3)

Country Link
BE (1) BE530261A (en)
FR (1) FR1106326A (en)
GB (1) GB741508A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017159A (en) * 1956-11-23 1962-01-16 Curtiss Wright Corp Hollow blade construction
EP0194883A2 (en) * 1985-03-13 1986-09-17 Westinghouse Electric Corporation Fabricated blade with spanwise cooling passages for gas turbine
EP1944468A3 (en) * 2007-01-11 2012-07-18 Rolls-Royce plc Gas turbine blade
EP2141326A3 (en) * 2008-07-03 2013-12-25 United Technologies Corporation Airfoil with tapered radial cooling passage
US9777575B2 (en) 2014-01-20 2017-10-03 Honeywell International Inc. Turbine rotor assemblies with improved slot cavities

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017159A (en) * 1956-11-23 1962-01-16 Curtiss Wright Corp Hollow blade construction
EP0194883A2 (en) * 1985-03-13 1986-09-17 Westinghouse Electric Corporation Fabricated blade with spanwise cooling passages for gas turbine
EP0194883A3 (en) * 1985-03-13 1989-01-18 Westinghouse Electric Corporation Fabricated blade with spanwise cooling passages for gas turbine
EP1944468A3 (en) * 2007-01-11 2012-07-18 Rolls-Royce plc Gas turbine blade
US8297925B2 (en) 2007-01-11 2012-10-30 Rolls-Royce Plc Aerofoil configuration
EP2141326A3 (en) * 2008-07-03 2013-12-25 United Technologies Corporation Airfoil with tapered radial cooling passage
US9777575B2 (en) 2014-01-20 2017-10-03 Honeywell International Inc. Turbine rotor assemblies with improved slot cavities

Also Published As

Publication number Publication date
BE530261A (en)
FR1106326A (en) 1955-12-16

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