DE2640830A1 - Verfahren und vorrichtung zum abdichten des stroemungskanales in einer stroemungsmaschine - Google Patents

Verfahren und vorrichtung zum abdichten des stroemungskanales in einer stroemungsmaschine

Info

Publication number
DE2640830A1
DE2640830A1 DE19762640830 DE2640830A DE2640830A1 DE 2640830 A1 DE2640830 A1 DE 2640830A1 DE 19762640830 DE19762640830 DE 19762640830 DE 2640830 A DE2640830 A DE 2640830A DE 2640830 A1 DE2640830 A1 DE 2640830A1
Authority
DE
Germany
Prior art keywords
air
cavity
nozzles
tangential
radially
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.)
Withdrawn
Application number
DE19762640830
Other languages
German (de)
English (en)
Inventor
David Edward Crow
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 DE2640830A1 publication Critical patent/DE2640830A1/de
Withdrawn legal-status Critical Current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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
DE19762640830 1975-10-20 1976-09-10 Verfahren und vorrichtung zum abdichten des stroemungskanales in einer stroemungsmaschine Withdrawn DE2640830A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/624,205 US3980411A (en) 1975-10-20 1975-10-20 Aerodynamic seal for a rotary machine

Publications (1)

Publication Number Publication Date
DE2640830A1 true DE2640830A1 (de) 1977-04-21

Family

ID=24501094

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19762640830 Withdrawn DE2640830A1 (de) 1975-10-20 1976-09-10 Verfahren und vorrichtung zum abdichten des stroemungskanales in einer stroemungsmaschine

Country Status (13)

Country Link
US (1) US3980411A (OSRAM)
JP (1) JPS5252014A (OSRAM)
BE (1) BE846327A (OSRAM)
CA (1) CA1039327A (OSRAM)
CH (1) CH610059A5 (OSRAM)
DE (1) DE2640830A1 (OSRAM)
FR (1) FR2328846A1 (OSRAM)
GB (1) GB1510250A (OSRAM)
IL (1) IL50537A (OSRAM)
IT (1) IT1073083B (OSRAM)
NL (1) NL7610726A (OSRAM)
NO (1) NO763537L (OSRAM)
SE (1) SE410643B (OSRAM)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4236869A (en) * 1977-12-27 1980-12-02 United Technologies Corporation Gas turbine engine having bleed apparatus with dynamic pressure recovery
US4291531A (en) * 1978-04-06 1981-09-29 Rolls-Royce Limited Gas turbine engine
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
US4534701A (en) * 1982-06-29 1985-08-13 Gerhard Wisser Rotor or guide wheel of a turbine engine with shroud ring
US4627233A (en) * 1983-08-01 1986-12-09 United Technologies Corporation Stator assembly for bounding the working medium flow path of a gas turbine engine
US4708588A (en) * 1984-12-14 1987-11-24 United Technologies Corporation Turbine cooling air supply system
US4882902A (en) * 1986-04-30 1989-11-28 General Electric Company Turbine cooling air transferring apparatus
US4752185A (en) * 1987-08-03 1988-06-21 General Electric Company Non-contacting flowpath seal
US5181826A (en) * 1990-11-23 1993-01-26 General Electric Company Attenuating shroud support
US5245821A (en) * 1991-10-21 1993-09-21 General Electric Company Stator to rotor flow inducer
US6735956B2 (en) 2001-10-26 2004-05-18 Pratt & Whitney Canada Corp. High pressure turbine blade cooling scoop
US7591631B2 (en) * 2006-06-30 2009-09-22 United Technologies Corporation Flow delivery system for seals
US8935926B2 (en) 2010-10-28 2015-01-20 United Technologies Corporation Centrifugal compressor with bleed flow splitter for a gas turbine engine
US20140099190A1 (en) * 2012-10-05 2014-04-10 Solar Turbines Incorporated Gas turbine engine turbine housing with enlongated holes

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2463898A (en) * 1944-11-24 1949-03-08 Wright Aeronautical Corp Turbine sealing construction
US2919104A (en) * 1953-12-02 1959-12-29 Napier & Son Ltd Interstage seals and cooling means in axial flow turbines
GB766883A (en) * 1953-12-23 1957-01-30 Rolls Royce Improvements relating to gas turbines
US2988325A (en) * 1957-07-18 1961-06-13 Rolls Royce Rotary fluid machine with means supplying fluid to rotor blade passages
US3174719A (en) * 1962-06-12 1965-03-23 Dominion Eng Works Ltd Francis turbines and centrifugal pumps
FR1548541A (OSRAM) * 1967-10-24 1968-12-06
US3565545A (en) * 1969-01-29 1971-02-23 Melvin Bobo Cooling of turbine rotors in gas turbine engines
US3619076A (en) * 1970-02-02 1971-11-09 Gen Electric Liquid-cooled turbine bucket
US3635586A (en) * 1970-04-06 1972-01-18 Rolls Royce Method and apparatus for turbine blade cooling
US3826084A (en) * 1970-04-28 1974-07-30 United Aircraft Corp Turbine coolant flow system
GB1350471A (en) * 1971-05-06 1974-04-18 Secr Defence Gas turbine engine
CH529914A (de) * 1971-08-11 1972-10-31 Mo Energeticheskij Institut Turbinenstufe
US3768921A (en) * 1972-02-24 1973-10-30 Aircraft Corp Chamber pressure control using free vortex flow
US3832090A (en) * 1972-12-01 1974-08-27 Avco Corp Air cooling of turbine blades
US3936215A (en) * 1974-12-20 1976-02-03 United Technologies Corporation Turbine vane cooling

Also Published As

Publication number Publication date
NL7610726A (nl) 1977-04-22
SE410643B (sv) 1979-10-22
SE7610388L (sv) 1977-04-21
IL50537A (en) 1979-03-12
NO763537L (OSRAM) 1977-04-21
IL50537A0 (en) 1976-11-30
FR2328846B1 (OSRAM) 1982-05-14
CH610059A5 (OSRAM) 1979-03-30
CA1039327A (en) 1978-09-26
US3980411A (en) 1976-09-14
JPS5252014A (en) 1977-04-26
BE846327A (fr) 1977-01-17
GB1510250A (en) 1978-05-10
IT1073083B (it) 1985-04-13
FR2328846A1 (fr) 1977-05-20

Similar Documents

Publication Publication Date Title
DE2640830A1 (de) Verfahren und vorrichtung zum abdichten des stroemungskanales in einer stroemungsmaschine
DE3825744A1 (de) Fluiddichtungs- und gasturbinenanordnung sowie verfahren zum verhindern des entweichens von arbeitsfluid aus einer turbomaschine
DE69305326T2 (de) Ejektor für kühlfluid
DE1601564A1 (de) Mantelring fuer Gasturbinenanlagen
DE2147537A1 (de) Kühleinrichtung für die Enden von Turbinenlaufschaufeln mit Luftexpansion
DE3210626C2 (OSRAM)
DE1964057A1 (de) Kompressor
DE4003802A1 (de) Spaltregulierung für die Turbine eines Gasturbinentriebwerks
DE2812051A1 (de) Ringdichtung fuer ein gasturbinentriebwerk
WO2004090291A1 (de) Turbomaschine
DE102015210385A1 (de) Vorrichtung zur Kühlung einer Wandung eines Bauteils einer Gasturbine
DE3507578A1 (de) Turbinenlaufschaufel ohne deckband
DE2833220C2 (OSRAM)
DE102019211669A1 (de) Dichtungsvorrichtung und turbomaschine
DE3116923A1 (de) "turbinenkuehlluft-umlenkeinrichtung"
AT395264B (de) Dampf- oder gasdurchstroemte turbine oder verdichter
DE112015005131B4 (de) Kühlstruktur für Turbine, und Gasturbine
DE19735172A1 (de) Verbessertes Turbinenscheiben-Eintrittsverhinderungsverfahren und -vorrichtung
DE3116762C2 (de) Fluidgesperrte Wellendichtung mit reduzierter Gleitgeschwindigkeit
DE112019006779T5 (de) Rotationsmaschine
DE1942346A1 (de) Vorrichtung zur Abdichtung des Rotors gegenueber dem Stator bei einer zu einem Gasturbinentriebwerk gehoerigen Turbine
DE4331779A1 (de) Verfahren und Vorrichtung zur Reduktion der Spaltstrommischverluste und der Spaltanregung von rotierenden thermischen Maschinen
EP1734292A1 (de) Dichtungsmittel für eine Strömungsmaschine
DE3026558A1 (de) Radiale turbomaschinen, insbesondere abgasturbolader fuer brennkraftmaschinen
DE1106557B (de) Gasturbine, deren Laeuferschaufeln innere Kuehlkanaele aufweisen

Legal Events

Date Code Title Description
8139 Disposal/non-payment of the annual fee