USB561712I5 - - Google Patents

Info

Publication number
USB561712I5
USB561712I5 US56171275A USB561712I5 US B561712 I5 USB561712 I5 US B561712I5 US 56171275 A US56171275 A US 56171275A US B561712 I5 USB561712 I5 US B561712I5
Authority
US
United States
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
Other languages
English (en)
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 filed Critical
Priority to US05/561,712 priority Critical patent/US3992126A/en
Publication of USB561712I5 publication Critical patent/USB561712I5/en
Priority to SE7602652A priority patent/SE411931B/xx
Priority to IL49165A priority patent/IL49165A/en
Priority to GB11614/76A priority patent/GB1538614A/en
Priority to FR7608460A priority patent/FR2305596A1/fr
Priority to DE19762612729 priority patent/DE2612729A1/de
Priority to JP51032053A priority patent/JPS51119417A/ja
Application granted granted Critical
Publication of US3992126A publication Critical patent/US3992126A/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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)
US05/561,712 1975-03-25 1975-03-25 Turbine cooling Expired - Lifetime US3992126A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
US05/561,712 US3992126A (en) 1975-03-25 1975-03-25 Turbine cooling
SE7602652A SE411931B (sv) 1975-03-25 1976-02-27 Anordning vid turbinmunstycken for gasturbinmotor
IL49165A IL49165A (en) 1975-03-25 1976-03-05 Turbine cooling structure
GB11614/76A GB1538614A (en) 1975-03-25 1976-03-23 Turbine cooling
FR7608460A FR2305596A1 (fr) 1975-03-25 1976-03-24 Systeme de refroidissement pour turbine
DE19762612729 DE2612729A1 (de) 1975-03-25 1976-03-25 Turbinenkuehlung
JP51032053A JPS51119417A (en) 1975-03-25 1976-03-25 Gas turbine engine with cooling structure

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
USB561712I5 true USB561712I5 (enrdf_load_stackoverflow) 1976-02-17
US3992126A US3992126A (en) 1976-11-16

Family

ID=24243108

Family Applications (1)

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

Country Status (1)

Country Link
US (1) US3992126A (enrdf_load_stackoverflow)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4314792A (en) * 1978-12-20 1982-02-09 United Technologies Corporation Turbine seal and vane damper
US4279123A (en) * 1978-12-20 1981-07-21 United Technologies Corporation External gas turbine engine cooling for clearance control
US4525997A (en) * 1983-08-01 1985-07-02 United Technologies Corporation Stator assembly for bounding the flow path of a gas turbine engine
US4721433A (en) * 1985-12-19 1988-01-26 United Technologies Corporation Coolable stator structure for a gas turbine engine
US4725199A (en) * 1985-12-23 1988-02-16 United Technologies Corporation Snap ring construction
US5022816A (en) * 1989-10-24 1991-06-11 United Technologies Corporation Gas turbine blade shroud support
US5197852A (en) * 1990-05-31 1993-03-30 General Electric Company Nozzle band overhang cooling
US5848874A (en) * 1997-05-13 1998-12-15 United Technologies Corporation Gas turbine stator vane assembly
DE10223655B3 (de) * 2002-05-28 2004-02-12 Mtu Aero Engines Gmbh Anordnung zum axialen und radialen Fixieren der Leitschaufeln eines Leitschaufelkranzes einer Gasturbine
CN101832154B (zh) * 2009-03-11 2013-03-27 中国科学院工程热物理研究所 一种航空发动机涡轮叶片气膜冷却方法
US20200072070A1 (en) * 2018-09-05 2020-03-05 United Technologies Corporation Unified boas support and vane platform

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2427244A (en) * 1944-03-07 1947-09-09 Gen Electric Gas turbine
CA590506A (en) * 1960-01-12 Rolls Royce Limited Axial-flow fluid machines
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
US3836279A (en) * 1973-02-23 1974-09-17 United Aircraft Corp Seal means for blade and shroud

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA590506A (en) * 1960-01-12 Rolls Royce Limited Axial-flow fluid machines
US2427244A (en) * 1944-03-07 1947-09-09 Gen Electric Gas turbine
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
US3836279A (en) * 1973-02-23 1974-09-17 United Aircraft Corp Seal means for blade and shroud

Also Published As

Publication number Publication date
US3992126A (en) 1976-11-16

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