GB375643A - Improvements in and relating to combustion turbines - Google Patents

Improvements in and relating to combustion turbines

Info

Publication number
GB375643A
GB375643A GB27873/31A GB2787331A GB375643A GB 375643 A GB375643 A GB 375643A GB 27873/31 A GB27873/31 A GB 27873/31A GB 2787331 A GB2787331 A GB 2787331A GB 375643 A GB375643 A GB 375643A
Authority
GB
United Kingdom
Prior art keywords
cooling
relating
turbines
rotor
combustion turbines
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
GB27873/31A
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.)
FABRICATION DES MOTEURS ET TUR
Original Assignee
FABRICATION DES MOTEURS ET TUR
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 FABRICATION DES MOTEURS ET TUR filed Critical FABRICATION DES MOTEURS ET TUR
Publication of GB375643A publication Critical patent/GB375643A/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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • F01D5/082—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades on the side of the rotor disc

Landscapes

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

Abstract

375,643. Gas turbines. SOC. POUR LA FABRICATION DES MOTEURS ET TURBINES, 38, Rue des Haies, Paris. Oct. 7, 1931, No. 27873. Convention date, June 9. [Class 110 (iii).] Cooling is effected by fan blades 4 mounted on the rotor 2. They pass air through the rotor blades 1 in regions which are free of combustion products. The discharged air passing through the openings 10 may be used for cooling the distributers, or may be passed to the carburetter.
GB27873/31A 1931-06-09 1931-10-07 Improvements in and relating to combustion turbines Expired GB375643A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR375643X 1931-06-09

Publications (1)

Publication Number Publication Date
GB375643A true GB375643A (en) 1932-06-30

Family

ID=8894984

Family Applications (1)

Application Number Title Priority Date Filing Date
GB27873/31A Expired GB375643A (en) 1931-06-09 1931-10-07 Improvements in and relating to combustion turbines

Country Status (1)

Country Link
GB (1) GB375643A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2434134A (en) * 1939-12-19 1948-01-06 Power Jets Res & Dev Ltd Cooling means for internal-combustion turbine wheels of jet propulsion engines
US2626502A (en) * 1947-05-29 1953-01-27 Lagelbauer Ernest Cooling system for gas turbine blading

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2434134A (en) * 1939-12-19 1948-01-06 Power Jets Res & Dev Ltd Cooling means for internal-combustion turbine wheels of jet propulsion engines
US2626502A (en) * 1947-05-29 1953-01-27 Lagelbauer Ernest Cooling system for gas turbine blading

Similar Documents

Publication Publication Date Title
GB731292A (en) Improvements in processes of making turbine and compressor blades
GB586570A (en) Improvements in internal combustion turbine plant for propulsion
GB375643A (en) Improvements in and relating to combustion turbines
GB452412A (en) Improvements relating to apparatus for cooling the rotors of turbines
GB457574A (en) Improvements in bearings for air circulating fans
GB419440A (en) Improvements in or relating to ventilating apparatus
GB502727A (en) Improvements in and relating to the charging of internal combustion engines
GB712633A (en) Improvements relating to gas-turbine engines
GB439773A (en) Improvements in steam and gas turbines
GB659569A (en) Improvements in or relating to lubrication systems for aviation power plants
GB350712A (en) Improvements in or relating to turbines with two or more peripheral intakes and with branched distributors
GB358425A (en) Improvements in and relating to internal combustion motor power plant
GB443504A (en) Improvements in superchargers for internal combustion engines
GB536061A (en) Improvements in or relating to gas turbine installations
GB491333A (en) Improvements in or relating to means for cooling and silencing the exhaust of internal combustion engines
GB431989A (en) Improvements in or relating to exhaust manifolds of internal combustion engines
GB288161A (en)
GB349628A (en) Means for withdrawing the exhaust from internal combustion engines
GB513046A (en) Improvements relating to exhaust systems for internal combustion engines
GB411095A (en) Improvements in and relating to air or gas compressors
GB355080A (en) Improvements in or relating to the cooling of internal combustion engines
GB285747A (en) Improvements in turbines driven by the exhaust from internal combustion engines
GB529714A (en) Improvements in and relating to gas turbine plants
SE47531C1 (en)
GB463390A (en) Improvements in and relating to elastic fluid turbines