FR1227668A - Axial flow compressor - Google Patents

Axial flow compressor

Info

Publication number
FR1227668A
FR1227668A FR797640A FR797640A FR1227668A FR 1227668 A FR1227668 A FR 1227668A FR 797640 A FR797640 A FR 797640A FR 797640 A FR797640 A FR 797640A FR 1227668 A FR1227668 A FR 1227668A
Authority
FR
France
Prior art keywords
axial flow
flow compressor
compressor
axial
flow
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
FR797640A
Other languages
French (fr)
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Application granted granted Critical
Publication of FR1227668A publication Critical patent/FR1227668A/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
    • 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)
FR797640A 1958-06-16 1959-06-16 Axial flow compressor Expired FR1227668A (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
FR1227668A true FR1227668A (en) 1960-08-22

Family

ID=24983890

Family Applications (1)

Application Number Title Priority Date Filing Date
FR797640A Expired FR1227668A (en) 1958-06-16 1959-06-16 Axial flow compressor

Country Status (3)

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

Cited By (4)

* 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
US3824031A (en) * 1972-01-12 1974-07-16 Rolls Royce 1971 Ltd Turbine casing for a gas turbine engine
EP0017306A1 (en) * 1979-03-14 1980-10-15 Rolls-Royce Plc Stator vane assembly for a gas turbine engine
EP1455055A1 (en) * 2003-03-06 2004-09-08 Snecma Moteurs Turbomachine with cooled shroud segments

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3798899A (en) * 1971-12-29 1974-03-26 Power Technology Corp Gas turbine engine
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
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

Cited By (6)

* 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
US3824031A (en) * 1972-01-12 1974-07-16 Rolls Royce 1971 Ltd Turbine casing for a gas turbine engine
EP0017306A1 (en) * 1979-03-14 1980-10-15 Rolls-Royce Plc Stator vane assembly for a gas turbine engine
EP1455055A1 (en) * 2003-03-06 2004-09-08 Snecma Moteurs Turbomachine with cooled shroud segments
FR2852053A1 (en) * 2003-03-06 2004-09-10 Snecma Moteurs HIGH PRESSURE TURBINE FOR TURBOMACHINE
US7011493B2 (en) 2003-03-06 2006-03-14 Snecma Moteurs Turbomachine with cooled ring segments

Also Published As

Publication number Publication date
CH369250A (en) 1963-05-15
GB856599A (en) 1960-12-21

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