CA1027870A - Stator construction for an axial flow compressor - Google Patents

Stator construction for an axial flow compressor

Info

Publication number
CA1027870A
CA1027870A CA230,590A CA230590A CA1027870A CA 1027870 A CA1027870 A CA 1027870A CA 230590 A CA230590 A CA 230590A CA 1027870 A CA1027870 A CA 1027870A
Authority
CA
Canada
Prior art keywords
axial flow
flow compressor
stator construction
stator
construction
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
CA230,590A
Other languages
English (en)
French (fr)
Inventor
Richmond G. Shuttleworth
Donald L. 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.)
RTX 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
Application granted granted Critical
Publication of CA1027870A publication Critical patent/CA1027870A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Fats And Perfumes (AREA)
  • Polysaccharides And Polysaccharide Derivatives (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CA230,590A 1974-07-29 1975-07-02 Stator construction for an axial flow compressor Expired CA1027870A (en)

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 (1)

Publication Number Publication Date
CA1027870A true CA1027870A (en) 1978-03-14

Family

ID=23956790

Family Applications (1)

Application Number Title Priority Date Filing Date
CA230,590A Expired CA1027870A (en) 1974-07-29 1975-07-02 Stator construction for an axial flow compressor

Country Status (11)

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

Families Citing this family (12)

* 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
EP0763653B1 (en) * 1995-09-13 2001-07-18 SOCIETE DE CONSTRUCTION DES AVIONS HUREL-DUBOIS (société anonyme) Thrust reverser door with jet deflection cascade
US6234750B1 (en) 1999-03-12 2001-05-22 General Electric Company Interlocked compressor stator
RU2232303C1 (ru) * 2002-11-10 2004-07-10 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Силовой корпус компрессора гтд
US7743497B2 (en) * 2005-10-06 2010-06-29 General Electric Company Method of providing non-uniform stator vane spacing in a compressor
EP3044424B1 (en) 2013-09-10 2020-05-27 United Technologies Corporation Plug seal for gas turbine engine
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
US3302926A (en) * 1965-12-06 1967-02-07 Gen Electric Segmented nozzle diaphragm for high temperature turbine
US3326523A (en) * 1965-12-06 1967-06-20 Gen Electric Stator vane assembly having composite sectors
US3773430A (en) * 1972-03-17 1973-11-20 Ingersoll Rand Co Gas compressor

Also Published As

Publication number Publication date
BR7504846A (pt) 1976-07-06
NO149010B (no) 1983-10-17
IT1040063B (it) 1979-12-20
JPS6050999B2 (ja) 1985-11-11
SE419260B (sv) 1981-07-20
NO752644L (OSRAM) 1976-01-30
FR2280812A1 (fr) 1976-02-27
JPS5138112A (OSRAM) 1976-03-30
GB1511019A (en) 1978-05-17
DE2532554A1 (de) 1976-02-19
CH589229A5 (OSRAM) 1977-06-30
US3918832A (en) 1975-11-11
FR2280812B1 (OSRAM) 1980-09-26
DE2532554C2 (de) 1985-05-23
SE7508371L (sv) 1976-01-30
NO149010C (no) 1984-01-25

Similar Documents

Publication Publication Date Title
CA1018069A (en) Stators of axial turbomachines
CA1034929A (en) Axial-flow fan
CA1008422A (en) Air compressor
CA1010368A (en) Gas turbine rotor construction
CA1022900A (en) Variable pitch axial fan
CA1024822A (en) Pumping assembly
CA1008774A (en) Slidable stator seal
CA1034791A (en) Flow meter having self-centering rotor assembly
AU502657B2 (en) Turbine system operation
SE7506130L (sv) Axialkompressor
CA1027870A (en) Stator construction for an axial flow compressor
AU499912B2 (en) Inlet duct
CA1030119A (en) Axial flow fan assembly
AU474305B2 (en) Centrifugal gas compressor unit
CA1011997A (en) Motor-pump assembly
CA1018952A (en) Axial flow fan apparatus
CA1029004A (en) Ring compressor
CA977563A (en) Shaft liner assembly
AU502658B2 (en) Turbine operation
AU491864B2 (en) Axial flow fans
AU8007275A (en) Axial flow fans
AU465887B2 (en) Gas turbo-generator
SU566967A1 (ru) Осевой компрессор
CA985636A (en) Axial flow gas compressor
AU490937B2 (en) Housing ASSEMBLY FOR AIR COMPRESSOR ANDTHE LIKE