GB574545A - Improvements in and relating to cooling arrangements for gas turbines - Google Patents

Improvements in and relating to cooling arrangements for gas turbines

Info

Publication number
GB574545A
GB574545A GB10341/41A GB1034141A GB574545A GB 574545 A GB574545 A GB 574545A GB 10341/41 A GB10341/41 A GB 10341/41A GB 1034141 A GB1034141 A GB 1034141A GB 574545 A GB574545 A GB 574545A
Authority
GB
United Kingdom
Prior art keywords
gas turbines
relating
cooling arrangements
wheel
houston
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
GB10341/41A
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston 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
Application filed by British Thomson Houston Co Ltd filed Critical British Thomson Houston Co Ltd
Priority to GB10341/41A priority Critical patent/GB574545A/en
Publication of GB574545A publication Critical patent/GB574545A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/085Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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

574,545. Gas turbines. BRITISH THOMSON-HOUSTON CO., Ltd., (General Electric Co.). Aug. 14,1941, No. 10341. [Class 110 (iii)] A turbine wheel 10 receiving the exhaust from an aircraft I.C. engine is cooled by a flow of air taken in at 23, passed through the space between the wheel and a dished disc 24 and discharged into the slip stream at 29. Specification 567,546 is referred to.
GB10341/41A 1941-08-14 1941-08-14 Improvements in and relating to cooling arrangements for gas turbines Expired GB574545A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB10341/41A GB574545A (en) 1941-08-14 1941-08-14 Improvements in and relating to cooling arrangements for gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB10341/41A GB574545A (en) 1941-08-14 1941-08-14 Improvements in and relating to cooling arrangements for gas turbines

Publications (1)

Publication Number Publication Date
GB574545A true GB574545A (en) 1946-01-10

Family

ID=9966070

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10341/41A Expired GB574545A (en) 1941-08-14 1941-08-14 Improvements in and relating to cooling arrangements for gas turbines

Country Status (1)

Country Link
GB (1) GB574545A (en)

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