CH369250A - Axial turbo compressor - Google Patents

Axial turbo compressor

Info

Publication number
CH369250A
CH369250A CH7444859A CH7444859A CH369250A CH 369250 A CH369250 A CH 369250A CH 7444859 A CH7444859 A CH 7444859A CH 7444859 A CH7444859 A CH 7444859A CH 369250 A CH369250 A CH 369250A
Authority
CH
Switzerland
Prior art keywords
turbo compressor
axial turbo
axial
compressor
turbo
Prior art date
Application number
CH7444859A
Other languages
German (de)
Inventor
William Welsh Harvey
Original Assignee
Gen Motors 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
Application filed by Gen Motors Corp filed Critical Gen Motors Corp
Publication of CH369250A publication Critical patent/CH369250A/en

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
    • F01D9/044—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators permanently, e.g. by welding, brazing, casting or the like
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH7444859A 1958-06-16 1959-06-15 Axial turbo compressor CH369250A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US74220558A 1958-06-16 1958-06-16

Publications (1)

Publication Number Publication Date
CH369250A true CH369250A (en) 1963-05-15

Family

ID=24983890

Family Applications (1)

Application Number Title Priority Date Filing Date
CH7444859A CH369250A (en) 1958-06-16 1959-06-15 Axial turbo compressor

Country Status (3)

Country Link
CH (1) CH369250A (en)
FR (1) FR1227668A (en)
GB (1) GB856599A (en)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3269702A (en) * 1964-01-13 1966-08-30 United Aircraft Corp Nozzle vane assembly
US3798899A (en) * 1971-12-29 1974-03-26 Power Technology Corp Gas turbine engine
GB1335145A (en) * 1972-01-12 1973-10-24 Rolls Royce Turbine casing for a gas turbine engine
GB2043798B (en) * 1979-03-14 1983-01-12 Rolls Royce Gas turbine stator vane assembly
DE3315914A1 (en) * 1983-05-02 1984-11-08 MTU Motoren- und Turbinen-Union München GmbH, 8000 München GAS TURBINE ENGINE WITH DEVICES FOR VANIZING GAPS
GB9306719D0 (en) * 1993-03-31 1993-06-02 Rolls Royce Plc A turbine assembly for a gas turbine engine
FR2817285B1 (en) 2000-11-30 2003-06-13 Snecma Moteurs STATOR INTERNAL OIL
FR2829525B1 (en) 2001-09-13 2004-03-12 Snecma Moteurs ASSEMBLY OF SECTORS OF A TURBINE DISTRIBUTOR TO A CRANKCASE
FR2835563B1 (en) * 2002-02-07 2004-04-02 Snecma Moteurs ARRANGEMENT FOR HANGING SECTORS IN A CIRCLE OF A CIRCLE OF A BLADE-BEARING DISTRIBUTOR
DE10214569A1 (en) * 2002-04-02 2003-10-16 Rolls Royce Deutschland Stator blade segment attachment for a gas turbine
FR2852053B1 (en) * 2003-03-06 2007-12-28 Snecma Moteurs HIGH PRESSURE TURBINE FOR TURBOMACHINE
GB2425155B (en) * 2005-04-13 2007-09-19 Rolls Royce Plc A mounting arrangement
FR2887939B1 (en) 2005-06-29 2016-09-30 Soc Nat D'etude Et De Construction De Moteurs D'aviation Snecma TURBOMACHINE MULTI-STAGE COMPRESSOR
US10428832B2 (en) 2012-08-06 2019-10-01 United Technologies Corporation Stator anti-rotation lug
DE102022124843A1 (en) 2022-09-27 2024-03-28 Audi Aktiengesellschaft Connection device and electrical machine comprising it

Also Published As

Publication number Publication date
GB856599A (en) 1960-12-21
FR1227668A (en) 1960-08-22

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