CH541066A - Gas turbine - Google Patents

Gas turbine

Info

Publication number
CH541066A
CH541066A CH977871A CH977871A CH541066A CH 541066 A CH541066 A CH 541066A CH 977871 A CH977871 A CH 977871A CH 977871 A CH977871 A CH 977871A CH 541066 A CH541066 A CH 541066A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine
gas
Prior art date
Application number
CH977871A
Other languages
French (fr)
Inventor
J Rahaim Thomas
M Mierley George
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of CH541066A publication Critical patent/CH541066A/en

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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH977871A 1970-07-02 1971-07-02 Gas turbine CH541066A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5197070A 1970-07-02 1970-07-02

Publications (1)

Publication Number Publication Date
CH541066A true CH541066A (en) 1973-08-31

Family

ID=21974553

Family Applications (1)

Application Number Title Priority Date Filing Date
CH977871A CH541066A (en) 1970-07-02 1971-07-02 Gas turbine

Country Status (8)

Country Link
US (1) US3656862A (en)
JP (1) JPS5020201B1 (en)
BE (1) BE769254A (en)
CH (1) CH541066A (en)
DE (1) DE2131855A1 (en)
FR (1) FR2103007A5 (en)
GB (1) GB1306575A (en)
NL (1) NL7109117A (en)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3756741A (en) * 1971-12-17 1973-09-04 Jacuzzi Bros Inc Jet propulsion pump assembly
US3981609A (en) * 1975-06-02 1976-09-21 United Technologies Corporation Coolable blade tip shroud
GB1501916A (en) * 1975-06-20 1978-02-22 Rolls Royce Matching thermal expansions of components of turbo-machines
FR2401310A1 (en) * 1977-08-26 1979-03-23 Snecma REACTION ENGINE TURBINE CASE
US4346904A (en) * 1980-11-26 1982-08-31 Watkins Jr Shelton Honeycomb structure for use in abradable seals
US4553901A (en) * 1983-12-21 1985-11-19 United Technologies Corporation Stator structure for a gas turbine engine
US4643638A (en) * 1983-12-21 1987-02-17 United Technologies Corporation Stator structure for supporting an outer air seal in a gas turbine engine
US4687412A (en) * 1985-07-03 1987-08-18 Pratt & Whitney Canada Inc. Impeller shroud
GB2226365B (en) * 1988-12-22 1993-03-10 Rolls Royce Plc Turbomachine clearance control
US5001483A (en) * 1989-10-23 1991-03-19 Westinghouse Electric Corp. Digital to analog converter for an acoustic charge transport device
US5176495A (en) * 1991-07-09 1993-01-05 General Electric Company Thermal shielding apparatus or radiositor for a gas turbine engine
US5165848A (en) * 1991-07-09 1992-11-24 General Electric Company Vane liner with axially positioned heat shields
US5195868A (en) * 1991-07-09 1993-03-23 General Electric Company Heat shield for a compressor/stator structure
US5174714A (en) * 1991-07-09 1992-12-29 General Electric Company Heat shield mechanism for turbine engines
US5238365A (en) * 1991-07-09 1993-08-24 General Electric Company Assembly for thermal shielding of low pressure turbine
WO1994008143A1 (en) * 1992-10-07 1994-04-14 University Of Alabama At Birmingham Inlet clearance gap seal
US5524846A (en) * 1993-12-21 1996-06-11 The Boeing Company Fire protection system for airplanes
US6382905B1 (en) * 2000-04-28 2002-05-07 General Electric Company Fan casing liner support
GB2382380A (en) * 2001-11-24 2003-05-28 Rolls Royce Plc A removable abradable lining for the casing assembly of a gas turbine engine
US6682298B2 (en) 2002-05-17 2004-01-27 David George Demontmorency Rotating shaft confinement system
FR2859002A1 (en) * 2003-08-18 2005-02-25 Snecma Moteurs Abradable surface for gas turbine engine housing surrounding fan, is made from a resin with glass balls over a layer of thermoformable foam
US20050200080A1 (en) * 2004-03-10 2005-09-15 Siemens Westinghouse Power Corporation Seal for a turbine engine
WO2007035698A2 (en) * 2005-09-19 2007-03-29 Ingersoll-Rand Company Centrifugal compressor including a seal system
ES2357754T3 (en) * 2005-09-19 2011-04-29 Ingersoll Rand Company DRIVER FOR A CENTRIFUGAL COMPRESSOR.
CN101297118B (en) * 2005-09-19 2011-09-28 英格索尔-兰德公司 Stationary seal ring for a centrifugal compressor
US20080063508A1 (en) * 2006-09-08 2008-03-13 Barry Barnett Fan case abradable
US8998565B2 (en) * 2011-04-18 2015-04-07 General Electric Company Apparatus to seal with a turbine blade stage in a gas turbine
EP2719869A1 (en) 2012-10-12 2014-04-16 MTU Aero Engines GmbH Axial sealing in a housing structure for a turbomachine
ES2679343T3 (en) * 2013-04-24 2018-08-24 MTU Aero Engines AG Sealing gasket
EP2835500A1 (en) 2013-08-09 2015-02-11 Siemens Aktiengesellschaft Insert element and gas turbine
EP2853685A1 (en) * 2013-09-25 2015-04-01 Siemens Aktiengesellschaft Insert element and gas turbine
US10167727B2 (en) * 2014-08-13 2019-01-01 United Technologies Corporation Gas turbine engine blade containment system
EP3228826B1 (en) * 2016-04-05 2021-03-17 MTU Aero Engines GmbH Seal segment arrangement having a connector, corresponding gas turbine engine and method of manufacturing
DE102019110671A1 (en) * 2019-04-25 2020-10-29 Man Energy Solutions Se turbocharger
CN110284929B (en) * 2019-07-19 2021-10-22 中国航发沈阳发动机研究所 Turbine cartridge receiver structure of obturaging

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA611004A (en) * 1960-12-20 S. Broffitt Wilgus Turbine nozzle
US3126149A (en) * 1964-03-24 Foamed aluminum honeycomb motor
US2994472A (en) * 1958-12-29 1961-08-01 Gen Electric Tip clearance control system for turbomachines
US3056583A (en) * 1960-11-10 1962-10-02 Gen Electric Retaining means for turbine shrouds and nozzle diaphragms of turbine engines
CH397360A (en) * 1961-11-28 1965-08-15 Licentia Gmbh Rotor seal with radially movable sealing ring segments, especially for turbo machines
US3314648A (en) * 1961-12-19 1967-04-18 Gen Electric Stator vane assembly
US3227418A (en) * 1963-11-04 1966-01-04 Gen Electric Variable clearance seal

Also Published As

Publication number Publication date
NL7109117A (en) 1972-01-04
JPS5020201B1 (en) 1975-07-12
FR2103007A5 (en) 1972-04-07
DE2131855A1 (en) 1972-01-05
BE769254A (en) 1971-12-29
GB1306575A (en) 1973-02-14
US3656862A (en) 1972-04-18

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Legal Events

Date Code Title Description
PL Patent ceased