JPS6050999B2 - 軸流圧縮機のステ−タ構造 - Google Patents

軸流圧縮機のステ−タ構造

Info

Publication number
JPS6050999B2
JPS6050999B2 JP50091848A JP9184875A JPS6050999B2 JP S6050999 B2 JPS6050999 B2 JP S6050999B2 JP 50091848 A JP50091848 A JP 50091848A JP 9184875 A JP9184875 A JP 9184875A JP S6050999 B2 JPS6050999 B2 JP S6050999B2
Authority
JP
Japan
Prior art keywords
vane
compressor
case
compressor case
vanes
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
JP50091848A
Other languages
English (en)
Japanese (ja)
Other versions
JPS5138112A (no
Inventor
ジヨ−ジ シヤツトルウオ−ス リツチモンド
レオ ウイリアムス ドナルド
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
Publication of JPS5138112A publication Critical patent/JPS5138112A/ja
Publication of JPS6050999B2 publication Critical patent/JPS6050999B2/ja
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; 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)
JP50091848A 1974-07-29 1975-07-28 軸流圧縮機のステ−タ構造 Expired JPS6050999B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US492574 1974-07-29
US492574A US3918832A (en) 1974-07-29 1974-07-29 Stator construction for an axial flow compressor

Publications (2)

Publication Number Publication Date
JPS5138112A JPS5138112A (no) 1976-03-30
JPS6050999B2 true JPS6050999B2 (ja) 1985-11-11

Family

ID=23956790

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50091848A Expired JPS6050999B2 (ja) 1974-07-29 1975-07-28 軸流圧縮機のステ−タ構造

Country Status (11)

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

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 (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
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
BR7504846A (pt) 1976-07-06
IT1040063B (it) 1979-12-20
CA1027870A (en) 1978-03-14
FR2280812A1 (fr) 1976-02-27
CH589229A5 (no) 1977-06-30
NO149010C (no) 1984-01-25
FR2280812B1 (no) 1980-09-26
GB1511019A (en) 1978-05-17
NO752644L (no) 1976-01-30
DE2532554A1 (de) 1976-02-19
JPS5138112A (no) 1976-03-30
SE419260B (sv) 1981-07-20
US3918832A (en) 1975-11-11
DE2532554C2 (de) 1985-05-23
SE7508371L (sv) 1976-01-30
NO149010B (no) 1983-10-17

Similar Documents

Publication Publication Date Title
EP1502009B1 (en) Attachment of a ceramic shroud in a metal housing
EP0770761B1 (en) Rotor blade outer tip seal apparatus
EP3232005B1 (en) Turbine vane with load distribution system having a compliant layer
US4884950A (en) Segmented interstage seal assembly
US3079128A (en) Sealing and securing means for turbomachine blading
US6048170A (en) Turbine shroud ring
US5785492A (en) Method and apparatus for sealing a gas turbine stator vane assembly
US4621976A (en) Integrally cast vane and shroud stator with damper
US4863345A (en) Turbine blade shroud structure
US5653581A (en) Case-tied joint for compressor stators
US4716721A (en) Improvements in or relating to gas turbine engines
US8388310B1 (en) Turbine disc sealing assembly
US8167313B2 (en) Seal member, assembly and method
JP5427398B2 (ja) ターボ機械のセクタ化されたノズル
US7013652B2 (en) Gas turbo set
GB2058245A (en) Alleviating abnormal loadings in bearings
US9127559B2 (en) Diaphragm for turbomachines and method of manufacture
JP2013151936A (ja) 後付け可能な、段間の傾斜シール
US20030095865A1 (en) Rotor platform modification and methods using brush seals in diaphragm packing area of steam turbines to eliminate rotor bowing
JPS6050999B2 (ja) 軸流圧縮機のステ−タ構造
US6742987B2 (en) Cradle mounted turbine nozzle
US20100209233A1 (en) Catenary turbine seal systems
US4568247A (en) Balanced blade vibration damper
EP1040256B1 (en) Support for a turbine stator assembly
US6155788A (en) Rotor assembly