AR208122A1 - Una construccion de rotor de paletas - Google Patents

Una construccion de rotor de paletas

Info

Publication number
AR208122A1
AR208122A1 AR264123A AR26412376A AR208122A1 AR 208122 A1 AR208122 A1 AR 208122A1 AR 264123 A AR264123 A AR 264123A AR 26412376 A AR26412376 A AR 26412376A AR 208122 A1 AR208122 A1 AR 208122A1
Authority
AR
Argentina
Prior art keywords
vane rotor
rotor construction
construction
vane
rotor
Prior art date
Application number
AR264123A
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
Application granted granted Critical
Publication of AR208122A1 publication Critical patent/AR208122A1/es

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
    • 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
    • F01D11/008—Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/322—Arrangement of components according to their shape tangential

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)
AR264123A 1975-08-04 1976-01-01 Una construccion de rotor de paletas AR208122A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/601,741 US3972645A (en) 1975-08-04 1975-08-04 Platform seal-tangential blade

Publications (1)

Publication Number Publication Date
AR208122A1 true AR208122A1 (es) 1976-11-30

Family

ID=24408589

Family Applications (1)

Application Number Title Priority Date Filing Date
AR264123A AR208122A1 (es) 1975-08-04 1976-01-01 Una construccion de rotor de paletas

Country Status (9)

Country Link
US (1) US3972645A (es)
JP (1) JPS5912879B2 (es)
AR (1) AR208122A1 (es)
BR (1) BR7605038A (es)
CA (1) CA1039197A (es)
DE (1) DE2634888C2 (es)
FR (1) FR2320439A1 (es)
GB (1) GB1510242A (es)
IT (1) IT1067779B (es)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2620762C2 (de) * 1976-05-11 1977-11-17 Motoren- und Turbinen-Union München GmbH, 8000 München Spaltdichtung für Strömungsmaschinen, insbesondere Gasturbinenstrahltriebwerke
US4326835A (en) * 1979-10-29 1982-04-27 General Motors Corporation Blade platform seal for ceramic/metal rotor assembly
US4464096A (en) * 1979-11-01 1984-08-07 United Technologies Corporation Self-actuating rotor seal
GB2119026B (en) * 1981-03-25 1984-06-20 Rolls Royce Aerofoil blade mounting
US4482297A (en) * 1981-11-16 1984-11-13 Terry Corporation Bladed rotor assembly
FR2527260A1 (fr) * 1982-05-18 1983-11-25 Snecma Dispositif d'amortissement escamotable pour aubes d'une turbomachine
US4541778A (en) * 1984-05-18 1985-09-17 The United States Of America As Represented By The Secretary Of The Navy Pin rooted blade biaxial air seal
JPS6116374U (ja) * 1984-06-29 1986-01-30 敷島紡績株式会社 切断検知付スライバ−ガイド
US4743166A (en) * 1984-12-20 1988-05-10 General Electric Company Blade root seal
US4875830A (en) * 1985-07-18 1989-10-24 United Technologies Corporation Flanged ladder seal
US4743164A (en) * 1986-12-29 1988-05-10 United Technologies Corporation Interblade seal for turbomachine rotor
GB2220251A (en) * 1988-07-01 1990-01-04 Luk Lamellen & Kupplungsbau Fluid clutch
FR2664944B1 (fr) * 1990-07-18 1992-09-25 Snecma Compresseur forme notamment de redresseurs en couronne et procede de montage de ce compresseur.
US5281097A (en) * 1992-11-20 1994-01-25 General Electric Company Thermal control damper for turbine rotors
FR2776012B1 (fr) * 1998-03-12 2000-04-07 Snecma Joint d'etancheite d'un etage d'aubes circulaire
EP2075417B1 (fr) * 2007-12-27 2016-04-06 Techspace Aero Plateforme pour une roue aubagée de turbomachine, roue aubagée et compresseur ou turbomachine comportant une telle roue aubagée
US9097131B2 (en) * 2012-05-31 2015-08-04 United Technologies Corporation Airfoil and disk interface system for gas turbine engines
US8905716B2 (en) * 2012-05-31 2014-12-09 United Technologies Corporation Ladder seal system for gas turbine engines

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR378584A (fr) * 1906-10-12 1907-10-09 Belliss & Morcom Système d'aubes et de vannages pour turbines
FR398666A (fr) * 1909-04-19 1909-06-11 Thomson Houston Ateliers Dispositif de montage des aubes d'une turbine à fluide élastique
US1003892A (en) * 1910-03-09 1911-09-19 Gen Electric Turbine-bucket.
US1276405A (en) * 1917-03-01 1918-08-20 Charles Algernon Parsons Blade-shrouding for steam-turbines.
US2299429A (en) * 1941-03-08 1942-10-20 Westinghouse Electric & Mfg Co Turbine blade shrouding
US2912222A (en) * 1952-08-02 1959-11-10 Gen Electric Turbomachine blading and method of manufacture thereof
DE1024198B (de) * 1955-02-03 1958-02-13 Maschf Augsburg Nuernberg Ag Trommellaeufer fuer axial beaufschlagte Kreiselradmaschinen und Verfahren zu dessen Herstellung
US2948505A (en) * 1956-12-26 1960-08-09 Gen Electric Gas turbine rotor
US3367629A (en) * 1966-12-19 1968-02-06 Westinghouse Electric Corp Continuous shroud for rotor blades
FR1520600A (fr) * 1967-02-27 1968-04-12 Snecma Perfectionnements aux turbo-machines à flux axial, et en particulier aux compresseurs axiaux à deux rotors imbriqués contrarotatifs

Also Published As

Publication number Publication date
FR2320439B1 (es) 1981-12-18
FR2320439A1 (fr) 1977-03-04
GB1510242A (en) 1978-05-10
IT1067779B (it) 1985-03-16
CA1039197A (en) 1978-09-26
JPS5219310A (en) 1977-02-14
DE2634888C2 (de) 1985-05-23
BR7605038A (pt) 1977-08-09
DE2634888A1 (de) 1977-02-17
US3972645A (en) 1976-08-03
JPS5912879B2 (ja) 1984-03-26

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