JPS51119417A - Gas turbine engine with cooling structure - Google Patents

Gas turbine engine with cooling structure

Info

Publication number
JPS51119417A
JPS51119417A JP51032053A JP3205376A JPS51119417A JP S51119417 A JPS51119417 A JP S51119417A JP 51032053 A JP51032053 A JP 51032053A JP 3205376 A JP3205376 A JP 3205376A JP S51119417 A JPS51119417 A JP S51119417A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
cooling structure
cooling
engine
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.)
Pending
Application number
JP51032053A
Other languages
Japanese (ja)
Inventor
Bisuhamu Buraun Henrii
Kantaa Yuujin
Ruisu Detoora Furanshisu
Jiyoon Boringaa Geirii
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.)
Raytheon Technologies Corp
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 JPS51119417A publication Critical patent/JPS51119417A/en
Pending 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; 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)
JP51032053A 1975-03-25 1976-03-25 Gas turbine engine with cooling structure Pending JPS51119417A (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 (1)

Publication Number Publication Date
JPS51119417A true JPS51119417A (en) 1976-10-20

Family

ID=27072720

Family Applications (1)

Application Number Title Priority Date Filing Date
JP51032053A Pending JPS51119417A (en) 1975-03-25 1976-03-25 Gas turbine engine with cooling structure

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
IL49165A (en) 1977-12-30
GB1538614A (en) 1979-01-24
SE411931B (en) 1980-02-11
DE2612729A1 (en) 1976-10-14
IL49165A0 (en) 1976-05-31
SE7602652L (en) 1976-09-26
FR2305596A1 (en) 1976-10-22
FR2305596B1 (en) 1982-04-09

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