FR2280812A1 - Stator pour compresseur a courant axial - Google Patents

Stator pour compresseur a courant axial

Info

Publication number
FR2280812A1
FR2280812A1 FR7523244A FR7523244A FR2280812A1 FR 2280812 A1 FR2280812 A1 FR 2280812A1 FR 7523244 A FR7523244 A FR 7523244A FR 7523244 A FR7523244 A FR 7523244A FR 2280812 A1 FR2280812 A1 FR 2280812A1
Authority
FR
France
Prior art keywords
stator
current compressor
axial current
axial
compressor
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.)
Granted
Application number
FR7523244A
Other languages
English (en)
Other versions
FR2280812B1 (fr
Inventor
Richmond George Shuttleworth
Donald Leo Williams
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
Application filed by United Technologies Corp filed Critical United Technologies Corp
Publication of FR2280812A1 publication Critical patent/FR2280812A1/fr
Application granted granted Critical
Publication of FR2280812B1 publication Critical patent/FR2280812B1/fr
Granted 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Fats And Perfumes (AREA)
  • Polysaccharides And Polysaccharide Derivatives (AREA)
FR7523244A 1974-07-29 1975-07-25 Stator pour compresseur a courant axial Granted FR2280812A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US492574A US3918832A (en) 1974-07-29 1974-07-29 Stator construction for an axial flow compressor

Publications (2)

Publication Number Publication Date
FR2280812A1 true FR2280812A1 (fr) 1976-02-27
FR2280812B1 FR2280812B1 (fr) 1980-09-26

Family

ID=23956790

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7523244A Granted FR2280812A1 (fr) 1974-07-29 1975-07-25 Stator pour compresseur a courant axial

Country Status (11)

Country Link
US (1) US3918832A (fr)
JP (1) JPS6050999B2 (fr)
BR (1) BR7504846A (fr)
CA (1) CA1027870A (fr)
CH (1) CH589229A5 (fr)
DE (1) DE2532554C2 (fr)
FR (1) FR2280812A1 (fr)
GB (1) GB1511019A (fr)
IT (1) IT1040063B (fr)
NO (1) NO149010C (fr)
SE (1) SE419260B (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5167488A (en) * 1991-07-03 1992-12-01 General Electric Company Clearance control assembly having a thermally-controlled one-piece cylindrical housing for radially positioning shroud segments
DE69521806D1 (de) * 1995-09-13 2001-08-23 Hurel Dubois Avions Strahlumkehrgitter für eine Schubumkehrvorrichtungsklappe
US6234750B1 (en) * 1999-03-12 2001-05-22 General Electric Company Interlocked compressor stator
US7743497B2 (en) * 2005-10-06 2010-06-29 General Electric Company Method of providing non-uniform stator vane spacing in a compressor
EP3044424B1 (fr) 2013-09-10 2020-05-27 United Technologies Corporation Joint d'obturation étanche destiné à un moteur à turbine à gaz
US10287905B2 (en) 2013-11-11 2019-05-14 United Technologies Corporation Segmented seal for gas turbine engine
US10634055B2 (en) 2015-02-05 2020-04-28 United Technologies Corporation Gas turbine engine having section with thermally isolated area
US9920652B2 (en) 2015-02-09 2018-03-20 United Technologies Corporation Gas turbine engine having section with thermally isolated area
US11248622B2 (en) * 2016-09-02 2022-02-15 Raytheon Technologies Corporation Repeating airfoil tip strong pressure profile
US10550725B2 (en) * 2016-10-19 2020-02-04 United Technologies Corporation Engine cases and associated flange
US11629606B2 (en) * 2021-05-26 2023-04-18 General Electric Company Split-line stator vane assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2857093A (en) * 1954-12-02 1958-10-21 Cincinnati Testing & Res Lab Stator casing and blade assembly
GB800098A (en) * 1955-10-31 1958-08-20 Rolls Royce Improvements in or relating to multi-stage axial-flow compressors
US2997275A (en) * 1959-03-23 1961-08-22 Westinghouse Electric Corp Stator structure for axial-flow fluid machine
US3326523A (en) * 1965-12-06 1967-06-20 Gen Electric Stator vane assembly having composite sectors
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US3773430A (en) * 1972-03-17 1973-11-20 Ingersoll Rand Co Gas compressor

Also Published As

Publication number Publication date
IT1040063B (it) 1979-12-20
BR7504846A (pt) 1976-07-06
SE7508371L (sv) 1976-01-30
NO149010B (no) 1983-10-17
DE2532554A1 (de) 1976-02-19
FR2280812B1 (fr) 1980-09-26
DE2532554C2 (de) 1985-05-23
GB1511019A (en) 1978-05-17
US3918832A (en) 1975-11-11
SE419260B (sv) 1981-07-20
CH589229A5 (fr) 1977-06-30
NO149010C (no) 1984-01-25
JPS5138112A (fr) 1976-03-30
CA1027870A (fr) 1978-03-14
JPS6050999B2 (ja) 1985-11-11
NO752644L (fr) 1976-01-30

Similar Documents

Publication Publication Date Title
BR7506800A (pt) Estator hermetico para motor
OA05154A (fr) Turbine hydraulique à courant moteur
IT1041674B (it) Macchina elettrica
FR2310012A1 (fr) Rotor pour machine electrique
FR2280996A1 (fr) Rotor pour machines dynamoelectriques
IT1034733B (it) Macchina elettrica
SE408249B (sv) Foerfarande foer montering av en statorlindning
SE399491B (sv) Stator for permanentmagnet-magnetiserade maskiner
BE829475A (fr) Machine a courant alternatif polyphasee
BE825905A (fr) Machine dynamo electrique
FR2280812A1 (fr) Stator pour compresseur a courant axial
FR2335980A1 (fr) Rotor pour turbogeneratrice
FR2306558A1 (fr) Rotor pour moteur a courant alternatif
FR2280230A1 (fr) Perfectionnements apportes aux machines dynamo-electriques
BE824263A (fr) Induit pour un moteur a courant continu
FR2288410A2 (fr) Machine a courant continu
IT1049981B (it) Macchina elettrica
SE7414502L (sv) Genomforing for elektrisk forbindelse
BE828516A (fr) Disjoncteur-limiteur de courant
FR2284213A2 (fr) Perfectionnements apportes aux machines dynamo-electriques
SE7512856L (sv) Rotor for en elektrisk maskin
FR2280188A1 (fr) Disjoncteur-limiteur de courant
FR2288409A1 (fr) Machine electrique
ATA663574A (de) Luftspaltwicklung fur elektrische maschinen
SE7509336L (sv) Holje for elektrod

Legal Events

Date Code Title Description
ST Notification of lapse