GB1538614A - Turbine cooling - Google Patents

Turbine cooling

Info

Publication number
GB1538614A
GB1538614A GB11614/76A GB1161476A GB1538614A GB 1538614 A GB1538614 A GB 1538614A GB 11614/76 A GB11614/76 A GB 11614/76A GB 1161476 A GB1161476 A GB 1161476A GB 1538614 A GB1538614 A GB 1538614A
Authority
GB
United Kingdom
Prior art keywords
turbine cooling
turbine
cooling
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
GB11614/76A
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 GB1538614A publication Critical patent/GB1538614A/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
    • 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)
GB11614/76A 1975-03-25 1976-03-23 Turbine cooling Expired GB1538614A (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
GB1538614A true GB1538614A (en) 1979-01-24

Family

ID=27072720

Family Applications (1)

Application Number Title Priority Date Filing Date
GB11614/76A Expired GB1538614A (en) 1975-03-25 1976-03-23 Turbine cooling

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
FR2305596B1 (en) 1982-04-09
IL49165A0 (en) 1976-05-31
DE2612729A1 (en) 1976-10-14
JPS51119417A (en) 1976-10-20
SE7602652L (en) 1976-09-26
SE411931B (en) 1980-02-11
FR2305596A1 (en) 1976-10-22

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee