IL91326A0 - Axial compressor blade assembly - Google Patents

Axial compressor blade assembly

Info

Publication number
IL91326A0
IL91326A0 IL91326A IL9132689A IL91326A0 IL 91326 A0 IL91326 A0 IL 91326A0 IL 91326 A IL91326 A IL 91326A IL 9132689 A IL9132689 A IL 9132689A IL 91326 A0 IL91326 A0 IL 91326A0
Authority
IL
Israel
Prior art keywords
blade assembly
compressor blade
axial compressor
axial
assembly
Prior art date
Application number
IL91326A
Other languages
English (en)
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 IL91326A0 publication Critical patent/IL91326A0/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/34—Blade mountings
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F01D11/006—Sealing the gap between rotor blades or blades and rotor
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides

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)
IL91326A 1988-11-14 1989-08-15 Axial compressor blade assembly IL91326A0 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/270,994 US4878811A (en) 1988-11-14 1988-11-14 Axial compressor blade assembly

Publications (1)

Publication Number Publication Date
IL91326A0 true IL91326A0 (en) 1990-03-19

Family

ID=23033744

Family Applications (1)

Application Number Title Priority Date Filing Date
IL91326A IL91326A0 (en) 1988-11-14 1989-08-15 Axial compressor blade assembly

Country Status (6)

Country Link
US (1) US4878811A (ja)
EP (1) EP0369926B1 (ja)
JP (1) JP2644598B2 (ja)
KR (1) KR970005865B1 (ja)
DE (1) DE68900932D1 (ja)
IL (1) IL91326A0 (ja)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2644524A1 (fr) * 1989-03-15 1990-09-21 Snecma Aubes a pied marteau a positionnement angulaire ameliore
US5299915A (en) * 1992-07-15 1994-04-05 General Electric Corporation Bucket for the last stage of a steam turbine
US5217348A (en) * 1992-09-24 1993-06-08 United Technologies Corporation Turbine vane assembly with integrally cast cooling fluid nozzle
US5267834A (en) * 1992-12-30 1993-12-07 General Electric Company Bucket for the last stage of a steam turbine
KR20020005747A (ko) 1999-05-14 2002-01-17 칼 하인쯔 호르닝어 터보 엔진의 회전자용 밀봉 시스템
CN1252376C (zh) * 1999-05-14 2006-04-19 西门子公司 带有转子密封系统的流体机械
US6152698A (en) * 1999-08-02 2000-11-28 General Electric Company Kit of articles and method for assembling articles along a holder distance
US6499959B1 (en) * 2000-08-15 2002-12-31 General Electric Company Steam turbine high strength tangential entry closure bucket and retrofitting methods therefor
JP2002201913A (ja) * 2001-01-09 2002-07-19 Mitsubishi Heavy Ind Ltd ガスタービンの分割壁およびシュラウド
US6375429B1 (en) * 2001-02-05 2002-04-23 General Electric Company Turbomachine blade-to-rotor sealing arrangement
US6755618B2 (en) 2002-10-23 2004-06-29 General Electric Company Steam turbine closure bucket attachment
US7708528B2 (en) * 2005-09-06 2010-05-04 United Technologies Corporation Platform mate face contours for turbine airfoils
FR2897099B1 (fr) * 2006-02-08 2012-08-17 Snecma Roue de rotor de turbomachine
CN100517205C (zh) * 2006-04-21 2009-07-22 邱波 用于it领域的同时多维、增速、省空间的系统显示方法
US7517195B2 (en) * 2006-04-25 2009-04-14 General Electric Company Nested turbine bucket closure group
CH704825A1 (de) 2011-03-31 2012-10-15 Alstom Technology Ltd Turbomaschinenrotor.
US8961135B2 (en) 2011-06-29 2015-02-24 Siemens Energy, Inc. Mateface gap configuration for gas turbine engine
US9097131B2 (en) 2012-05-31 2015-08-04 United Technologies Corporation Airfoil and disk interface system for gas turbine engines
US9140136B2 (en) 2012-05-31 2015-09-22 United Technologies Corporation Stress-relieved wire seal assembly for gas turbine engines
EP2738356B1 (fr) * 2012-11-29 2019-05-01 Safran Aero Boosters SA Aube de redresseur de turbomachine, redresseur de turbomachine et procédé de montage associé
US20150330300A1 (en) * 2013-03-14 2015-11-19 United Technologies Corporation Two spool engine core with a starter
EP2818641A1 (de) * 2013-06-26 2014-12-31 Siemens Aktiengesellschaft Turbinenschaufel mit gestufter und abgeschrägter Plattformkante
US9670781B2 (en) * 2013-09-17 2017-06-06 Honeywell International Inc. Gas turbine engines with turbine rotor blades having improved platform edges
EP2918784A1 (de) * 2014-03-13 2015-09-16 Siemens Aktiengesellschaft Schaufelfuß für eine Turbinenschaufel
US10030530B2 (en) * 2014-07-31 2018-07-24 United Technologies Corporation Reversible blade rotor seal
US10190595B2 (en) 2015-09-15 2019-01-29 General Electric Company Gas turbine engine blade platform modification
CN112096653B (zh) * 2020-11-18 2021-01-19 中国航发上海商用航空发动机制造有限责任公司 叶片缘板、叶片环、叶轮盘以及燃气涡轮发动机

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA564048A (en) * 1958-09-30 A. Dean George Axial flow fans and compressors
US787907A (en) * 1903-12-04 1905-04-25 Edwin H Ludeman Turbine-engine.
GB137379A (en) * 1919-01-16 1920-01-15 Vickers Ltd Improvements relating to turbine blades
DE436567C (de) * 1924-01-19 1926-11-04 Waggon Und Maschb Akt Ges Leitschaufelkranz fuer Dampf- und Gasturbinen
US2148653A (en) * 1937-02-27 1939-02-28 Westinghouse Electric & Mfg Co Turbine blade
CH228272A (de) * 1942-03-14 1943-08-15 Sulzer Ag Dampf- oder Gasturbinenschaufel.
US2398140A (en) * 1943-12-08 1946-04-09 Armstrong Siddeley Motors Ltd Bladed rotor
GB706618A (en) * 1950-06-22 1954-03-31 Power Jets Res & Dev Ltd Improvements in or relating to rotors for turbines and similarly bladed fluid flow machines
US2955799A (en) * 1957-02-11 1960-10-11 United Aircraft Corp Blade damping means
DE1085643B (de) * 1959-04-13 1960-07-21 Ehrhardt & Sehmer Ag Maschf Laufschaufelbefestigung bei Axialstroemungsmaschinen
US3014695A (en) * 1960-02-03 1961-12-26 Gen Electric Turbine bucket retaining means
US3810711A (en) * 1972-09-22 1974-05-14 Gen Motors Corp Cooled turbine blade and its manufacture
US3923420A (en) * 1973-04-30 1975-12-02 Gen Electric Blade platform with friction damping interlock
FR2361531A1 (fr) * 1976-08-13 1978-03-10 Europ Turb Vapeur Turbine a fluide compressible
US4280795A (en) * 1979-12-26 1981-07-28 United Technologies Corporation Interblade seal for axial flow rotary machines
SU985327A1 (ru) * 1980-03-24 1982-12-30 Всесоюзное Научно-Производственное Объединение "Союзтурбогаз" Рабочее колесо осевой турбомашины
FR2517739A1 (fr) * 1981-12-09 1983-06-10 Snecma Dispositif de montage et de fixation d'aubes a pied marteau de compresseur et de turbine et procede de montage
US4460316A (en) * 1982-12-29 1984-07-17 Westinghouse Electric Corp. Blade group with pinned root
GB2156908A (en) * 1984-03-30 1985-10-16 Rolls Royce Bladed rotor assembly for gas turbine engine
US4688992A (en) * 1985-01-25 1987-08-25 General Electric Company Blade platform
JPS62267598A (ja) * 1986-05-16 1987-11-20 Hitachi Ltd ガスタ−ビン圧縮機動翼
US4767273A (en) * 1987-02-24 1988-08-30 Westinghouse Electric Corp. Apparatus and method for reducing blade flop in steam turbine

Also Published As

Publication number Publication date
EP0369926B1 (en) 1992-03-04
KR900008180A (ko) 1990-06-02
EP0369926A1 (en) 1990-05-23
KR970005865B1 (ko) 1997-04-21
JP2644598B2 (ja) 1997-08-25
DE68900932D1 (de) 1992-04-09
US4878811A (en) 1989-11-07
JPH02181098A (ja) 1990-07-13

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Legal Events

Date Code Title Description
RH Patent void
NE Application for restoration - patent lapsed through non-payment of renewal fees (section 60, patents law, 5727-1967)
KB Patent renewed