IL50537A - Aerodynamic seal for a rotary machine particularly for a gas turbine - Google Patents

Aerodynamic seal for a rotary machine particularly for a gas turbine

Info

Publication number
IL50537A
IL50537A IL50537A IL5053776A IL50537A IL 50537 A IL50537 A IL 50537A IL 50537 A IL50537 A IL 50537A IL 5053776 A IL5053776 A IL 5053776A IL 50537 A IL50537 A IL 50537A
Authority
IL
Israel
Prior art keywords
gas turbine
rotary machine
machine particularly
aerodynamic seal
aerodynamic
Prior art date
Application number
IL50537A
Other languages
English (en)
Other versions
IL50537A0 (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 IL50537A0 publication Critical patent/IL50537A0/xx
Publication of IL50537A publication Critical patent/IL50537A/xx

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
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing 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)
IL50537A 1975-10-20 1976-09-23 Aerodynamic seal for a rotary machine particularly for a gas turbine IL50537A (en)

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 (2)

Publication Number Publication Date
IL50537A0 IL50537A0 (en) 1976-11-30
IL50537A true IL50537A (en) 1979-03-12

Family

ID=24501094

Family Applications (1)

Application Number Title Priority Date Filing Date
IL50537A IL50537A (en) 1975-10-20 1976-09-23 Aerodynamic seal for a rotary machine particularly for a gas turbine

Country Status (13)

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

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 (no) * 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
GB1364511A (en) * 1971-08-11 1974-08-21 Mo Energeticheskij Institut Turbines
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
IL50537A0 (en) 1976-11-30
JPS5252014A (en) 1977-04-26
IT1073083B (it) 1985-04-13
SE410643B (sv) 1979-10-22
GB1510250A (en) 1978-05-10
CH610059A5 (no) 1979-03-30
US3980411A (en) 1976-09-14
DE2640830A1 (de) 1977-04-21
NO763537L (no) 1977-04-21
NL7610726A (nl) 1977-04-22
SE7610388L (sv) 1977-04-21
BE846327A (fr) 1977-01-17
CA1039327A (en) 1978-09-26
FR2328846A1 (fr) 1977-05-20
FR2328846B1 (no) 1982-05-14

Similar Documents

Publication Publication Date Title
CA1012066A (en) Cooling system for a gas turbine
CA1034509A (en) Vane rotator assembly for a gas turbine
CA982829A (en) Combustor for a gas turbine engine
IL51008A0 (en) Clearance control for gas turbine engine
IT1048628B (it) Paletta direttrice per turbine a gas
SE433519B (sv) Rotor for en gasturbin
IL46764A (en) Valve for a rotary valve engine
JPS5277913A (en) Gas turbine combustor
FR2292866A1 (fr) Rotor perfectionne pour turbine a gaz
GB1549152A (en) Rotor stage for a gas trubine engine
CA979810A (en) Cooled rotor blade for a gas turbine
IT1041775B (it) Paletta rotorica raffreddata peruna turbina a gas
JPS51120310A (en) Stator blade for gas turbine
IT1074030B (it) Disposizione di combistore per turbina a gas
IL50537A (en) Aerodynamic seal for a rotary machine particularly for a gas turbine
JPS5248713A (en) Gas turbine engine blade
CA1023973A (en) Apparatus for intermittently turning a turbine shaft
CH612486A5 (en) Process for sealing a shaft
GB1552536A (en) Rotor blade for a gas turbine engine
CA971995A (en) Static seal for a gas turbine
IT1073797B (it) Perfezionamento nelle macchine rotanti a flusso in particolare turbine a gas
GB1539790A (en) Rotor assemblies for gas turbine engines
GB1540419A (en) Rotary heat-accumulator type heat exchanger for a gas turbine engine having a sealing member
GB1546674A (en) Rotary blade and mounting ring assembly for a gas trubine engine
CA1029760A (en) Multi-piece apex seal for a rotary engine