NL104794C - - Google Patents

Info

Publication number
NL104794C
NL104794C NL104794DA NL104794C NL 104794 C NL104794 C NL 104794C NL 104794D A NL104794D A NL 104794DA NL 104794 C NL104794 C NL 104794C
Authority
NL
Netherlands
Application number
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 NL104794C publication Critical patent/NL104794C/xx

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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
NL104794D 1957-08-16 NL104794C (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US678693A US2937000A (en) 1957-08-16 1957-08-16 Stator units

Publications (1)

Publication Number Publication Date
NL104794C true NL104794C (en:Method)

Family

ID=24723873

Family Applications (1)

Application Number Title Priority Date Filing Date
NL104794D NL104794C (en:Method) 1957-08-16

Country Status (7)

Country Link
US (1) US2937000A (en:Method)
BE (1) BE570267A (en:Method)
CH (1) CH362268A (en:Method)
DE (1) DE1185865B (en:Method)
FR (1) FR1201329A (en:Method)
GB (1) GB879337A (en:Method)
NL (1) NL104794C (en:Method)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741667A (en) * 1986-05-28 1988-05-03 United Technologies Corporation Stator vane

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB904138A (en) * 1959-01-23 1962-08-22 Bristol Siddeley Engines Ltd Improvements in or relating to stator structures, for example for axial flow gas turbine engines
US3038652A (en) * 1959-10-21 1962-06-12 United Aircraft Corp Intermediate compressor case
US3062499A (en) * 1960-05-18 1962-11-06 United Aircraft Corp Vane mounting and seal
US3075744A (en) * 1960-08-16 1963-01-29 United Aircraft Corp Turbine nozzle vane mounting means
US3314648A (en) * 1961-12-19 1967-04-18 Gen Electric Stator vane assembly
GB1086432A (en) * 1965-09-21 1967-10-11 Bristol Siddeley Engines Ltd Gas turbine engines
FR1339521A (fr) * 1966-06-10 1963-10-11 Rolls Royce Machine à circulation de fluide
US3423071A (en) * 1967-07-17 1969-01-21 United Aircraft Corp Turbine vane retention
US3511577A (en) * 1968-04-10 1970-05-12 Caterpillar Tractor Co Turbine nozzle construction
US4184689A (en) * 1978-10-02 1980-01-22 United Technologies Corporation Seal structure for an axial flow rotary machine
US4566851A (en) * 1984-05-11 1986-01-28 United Technologies Corporation First stage turbine vane support structure
CA2070511C (en) * 1991-07-22 2001-08-21 Steven Milo Toborg Turbine nozzle support
US7025563B2 (en) 2003-12-19 2006-04-11 United Technologies Corporation Stator vane assembly for a gas turbine engine
US9702252B2 (en) * 2012-12-19 2017-07-11 Honeywell International Inc. Turbine nozzles with slip joints and methods for the production thereof
US11002147B2 (en) 2018-08-28 2021-05-11 Raytheon Technologies Corporation Fixed vane pack retaining ring
US12312979B1 (en) 2024-02-21 2025-05-27 Rolls-Royce North American Technologies Inc. Retainer rings for vane assemblies used in gas turbine engines

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB277663A (en) * 1926-09-20 1928-01-26 Lorenzen Turbinen Ag Improvements in or relating to turbines
GB589542A (en) * 1941-09-22 1947-06-24 Karl Baumann Improvements in internal combustion turbines
BE487115A (en:Method) * 1946-04-05
GB618525A (en) * 1946-06-18 1949-02-23 Adrian Albert Lombard Improvements in or relating to gas-turbine engines
FR965713A (en:Method) * 1947-05-07 1950-09-20
CH267782A (de) * 1947-08-29 1950-04-15 Westinghouse Electric Corp Leitvorrichtung für eine Gasturbine.
US2625013A (en) * 1948-11-27 1953-01-13 Gen Electric Gas turbine nozzle structure
US2609176A (en) * 1950-01-21 1952-09-02 A V Roe Canada Ltd Turbine nozzle guide vane construction

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4741667A (en) * 1986-05-28 1988-05-03 United Technologies Corporation Stator vane

Also Published As

Publication number Publication date
FR1201329A (fr) 1959-12-29
GB879337A (en) 1961-10-11
US2937000A (en) 1960-05-17
DE1185865B (de) 1965-01-21
BE570267A (en:Method)
CH362268A (de) 1962-05-31

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