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SE7602652L - TURBINE COOLING - Google Patents

TURBINE COOLING

Info

Publication number
SE7602652L
SE7602652L SE7602652A SE7602652A SE7602652L SE 7602652 L SE7602652 L SE 7602652L SE 7602652 A SE7602652 A SE 7602652A SE 7602652 A SE7602652 A SE 7602652A SE 7602652 L SE7602652 L SE 7602652L
Authority
SE
Sweden
Prior art keywords
turbine cooling
turbine
cooling
Prior art date
Application number
SE7602652A
Other languages
Swedish (sv)
Other versions
SE411931B (en
Inventor
G J Vollinger
H B Brown
E Cantor
F L Detolla
Original Assignee
United Technologies Corp
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 claimed from US05/561,713 external-priority patent/US3957391A/en
Priority claimed from US05/561,712 external-priority patent/US3992126A/en
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of SE7602652L publication Critical patent/SE7602652L/en
Publication of SE411931B publication Critical patent/SE411931B/en

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
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SE7602652A 1975-03-25 1976-02-27 DEVICE AT THE TURBINE NOZZLE FOR GAS TURBINE ENGINE SE411931B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US05/561,713 US3957391A (en) 1975-03-25 1975-03-25 Turbine cooling
US05/561,712 US3992126A (en) 1975-03-25 1975-03-25 Turbine cooling

Publications (2)

Publication Number Publication Date
SE7602652L true SE7602652L (en) 1976-09-26
SE411931B SE411931B (en) 1980-02-11

Family

ID=27072720

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7602652A SE411931B (en) 1975-03-25 1976-02-27 DEVICE AT THE TURBINE NOZZLE FOR GAS TURBINE ENGINE

Country Status (6)

Country Link
JP (1) JPS51119417A (en)
DE (1) DE2612729A1 (en)
FR (1) FR2305596A1 (en)
GB (1) GB1538614A (en)
IL (1) IL49165A (en)
SE (1) SE411931B (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5127793A (en) * 1990-05-31 1992-07-07 General Electric Company Turbine shroud clearance control assembly

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB701101A (en) * 1950-06-29 1953-12-16 Rolls Royce Improvements in or relating to gas-turbine engines
FR1297645A (en) * 1960-08-16 1962-06-29 United Aircraft Corp Improvements to gas turbines
US3314648A (en) * 1961-12-19 1967-04-18 Gen Electric Stator vane assembly
GB1085335A (en) * 1966-04-18 1967-09-27 Rolls Royce A fluid flow machine, such as, for example, a gas turbine engine
US3295824A (en) * 1966-05-06 1967-01-03 United Aircraft Corp Turbine vane seal
US3423071A (en) * 1967-07-17 1969-01-21 United Aircraft Corp Turbine vane retention
US3730640A (en) * 1971-06-28 1973-05-01 United Aircraft Corp Seal ring for gas turbine
US3781125A (en) * 1972-04-07 1973-12-25 Westinghouse Electric Corp Gas turbine nozzle vane structure
US3807891A (en) * 1972-09-15 1974-04-30 United Aircraft Corp Thermal response turbine shroud
US3836279A (en) * 1973-02-23 1974-09-17 United Aircraft Corp Seal means for blade and shroud
GB1483532A (en) * 1974-09-13 1977-08-24 Rolls Royce Stator structure for a gas turbine engine

Also Published As

Publication number Publication date
DE2612729A1 (en) 1976-10-14
GB1538614A (en) 1979-01-24
FR2305596B1 (en) 1982-04-09
IL49165A0 (en) 1976-05-31
SE411931B (en) 1980-02-11
IL49165A (en) 1977-12-30
FR2305596A1 (en) 1976-10-22
JPS51119417A (en) 1976-10-20

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