BE431387A - - Google Patents

Info

Publication number
BE431387A
BE431387A BE431387DA BE431387A BE 431387 A BE431387 A BE 431387A BE 431387D A BE431387D A BE 431387DA BE 431387 A BE431387 A BE 431387A
Authority
BE
Belgium
Prior art keywords
rotor
emi
walls
annular
casing
Prior art date
Application number
Other languages
English (en)
French (fr)
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.)
Publication of BE431387A publication Critical patent/BE431387A/fr
Priority claimed from GB23413/38A external-priority patent/GB508436A/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
    • F01D5/02—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
BE431387D 1936-07-01 BE431387A (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE2141401X 1936-07-01
GB23413/38A GB508436A (en) 1938-08-08 1938-08-08 Improvements in or relating to gas turbines

Publications (1)

Publication Number Publication Date
BE431387A true BE431387A (de)

Family

ID=32044209

Family Applications (1)

Application Number Title Priority Date Filing Date
BE431387D BE431387A (de) 1936-07-01

Country Status (2)

Country Link
US (1) US2141401A (de)
BE (1) BE431387A (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2540991A (en) * 1942-03-06 1951-02-06 Lockheed Aircraft Corp Gas reaction aircraft power plant
US2563269A (en) * 1943-05-22 1951-08-07 Lockheed Aircraft Corp Gas turbine
US2479046A (en) * 1944-08-23 1949-08-16 United Aircraft Corp Limiting heat transfer to the turbine rotor
US2479057A (en) * 1945-03-27 1949-08-16 United Aircraft Corp Turbine rotor
US2628066A (en) * 1946-10-02 1953-02-10 Rolls Royce Turbine disk
GB612097A (en) * 1946-10-09 1948-11-08 English Electric Co Ltd Improvements in and relating to the cooling of gas turbine rotors
US2684831A (en) * 1947-11-28 1954-07-27 Power Jets Res & Dev Ltd Turbine and like rotor
US2618461A (en) * 1948-10-05 1952-11-18 English Electric Co Ltd Gas turbine
US2625366A (en) * 1948-11-18 1953-01-13 Packard Motor Car Co Turbine rotor construction
US2722101A (en) * 1948-12-21 1955-11-01 Solar Aircraft Co Gas turbine sealing and cooling structure
US2839268A (en) * 1950-01-18 1958-06-17 Allis Chalmers Mfg Co Gas turbine
BE530135A (de) * 1953-07-06
NL214188A (de) * 1956-02-03
US2957675A (en) * 1956-05-07 1960-10-25 Gen Electric Damping means
US2990156A (en) * 1956-08-17 1961-06-27 Gen Electric Blade damping means
US3034764A (en) * 1959-12-18 1962-05-15 Gen Electric Damping means
US3269703A (en) * 1960-08-30 1966-08-30 Sundstrand Corp Gas turbine engine starter
FR2098558A5 (de) * 1970-07-20 1972-03-10 Onera (Off Nat Aerospatiale)
US3834831A (en) * 1973-01-23 1974-09-10 Westinghouse Electric Corp Blade shank cooling arrangement
US20120321441A1 (en) * 2011-06-20 2012-12-20 Kenneth Moore Ventilated compressor rotor for a turbine engine and a turbine engine incorporating same
RU2553049C2 (ru) * 2011-07-01 2015-06-10 Альстом Текнолоджи Лтд Лопатка ротора турбины, ротор турбины и турбина

Also Published As

Publication number Publication date
US2141401A (en) 1938-12-27

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