IT975912B - Elemento composito allungato avente un predeterminato coefficente effet tivo di dilatazione lineare parti colarmente anello statorico atto a circondare il rotore di una turbina a gas - Google Patents

Elemento composito allungato avente un predeterminato coefficente effet tivo di dilatazione lineare parti colarmente anello statorico atto a circondare il rotore di una turbina a gas

Info

Publication number
IT975912B
IT975912B IT70781/72A IT7078172A IT975912B IT 975912 B IT975912 B IT 975912B IT 70781/72 A IT70781/72 A IT 70781/72A IT 7078172 A IT7078172 A IT 7078172A IT 975912 B IT975912 B IT 975912B
Authority
IT
Italy
Prior art keywords
colarly
surround
rotor
gas turbine
linear expansion
Prior art date
Application number
IT70781/72A
Other languages
English (en)
Italian (it)
Original Assignee
Penny R
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 Penny R filed Critical Penny R
Application granted granted Critical
Publication of IT975912B publication Critical patent/IT975912B/it

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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion

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)
IT70781/72A 1971-12-01 1972-11-30 Elemento composito allungato avente un predeterminato coefficente effet tivo di dilatazione lineare parti colarmente anello statorico atto a circondare il rotore di una turbina a gas IT975912B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5566571A GB1363897A (en) 1971-12-01 1971-12-01 Composite elongate member having a predetermined effective coeffi cient of linear expansion

Publications (1)

Publication Number Publication Date
IT975912B true IT975912B (it) 1974-08-10

Family

ID=10474529

Family Applications (1)

Application Number Title Priority Date Filing Date
IT70781/72A IT975912B (it) 1971-12-01 1972-11-30 Elemento composito allungato avente un predeterminato coefficente effet tivo di dilatazione lineare parti colarmente anello statorico atto a circondare il rotore di una turbina a gas

Country Status (12)

Country Link
US (1) US3854843A (enrdf_load_html_response)
JP (1) JPS5138371B2 (enrdf_load_html_response)
AU (1) AU463454B2 (enrdf_load_html_response)
BE (1) BE792224A (enrdf_load_html_response)
CA (1) CA989312A (enrdf_load_html_response)
CH (1) CH561354A5 (enrdf_load_html_response)
DE (1) DE2258480A1 (enrdf_load_html_response)
FR (1) FR2164215A5 (enrdf_load_html_response)
GB (1) GB1363897A (enrdf_load_html_response)
IT (1) IT975912B (enrdf_load_html_response)
NL (1) NL7216110A (enrdf_load_html_response)
SE (1) SE385941B (enrdf_load_html_response)

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JPS5242906U (enrdf_load_html_response) * 1975-09-22 1977-03-26
JPS52127105U (enrdf_load_html_response) * 1976-03-25 1977-09-27
JPS52143312A (en) * 1976-05-24 1977-11-29 Hitachi Ltd Steam seal ring
US4087199A (en) * 1976-11-22 1978-05-02 General Electric Company Ceramic turbine shroud assembly
US4411594A (en) * 1979-06-30 1983-10-25 Rolls-Royce Limited Support member and a component supported thereby
US4522559A (en) * 1982-02-19 1985-06-11 General Electric Company Compressor casing
US4485630A (en) * 1982-12-08 1984-12-04 General Electric Company Combustor liner
GB2165590B (en) * 1984-10-09 1988-05-05 Rolls Royce Improvements in or relating to rotor tip clearance control devices
FR2572394B1 (fr) * 1984-10-30 1986-12-19 Snecma Procede de fabrication d'un anneau de turbine en ceramique integre a un support metallique annulaire
FR2576301B1 (fr) * 1985-01-24 1992-03-13 Europ Propulsion Procede de preparation de materiaux refractaires poreux, produits nouveaux ainsi obtenus et leurs applications a la preparation d'anneaux de turbine abradables
FR2577281B1 (fr) * 1985-02-13 1987-03-20 Snecma Carter de turbomachine associe a un dispositif pour ajuster le jeu entre aubes mobiles et carter
US4768924A (en) * 1986-07-22 1988-09-06 Pratt & Whitney Canada Inc. Ceramic stator vane assembly
GB8921003D0 (en) * 1989-09-15 1989-11-01 Rolls Royce Plc Improvements in or relating to shroud rings
CA2039756A1 (en) * 1990-05-31 1991-12-01 Larry Wayne Plemmons Stator having selectively applied thermal conductivity coating
US5332358A (en) * 1993-03-01 1994-07-26 General Electric Company Uncoupled seal support assembly
DE4309199A1 (de) * 1993-03-22 1994-09-29 Abb Management Ag Vorrichtung zur Befestigung von Wärmestausegmenten und Leitschaufeln in axialdurchströmten Turbinen
US5388959A (en) * 1993-08-23 1995-02-14 General Electric Company Seal including a non-metallic abradable material
FR2794816B1 (fr) 1999-06-10 2001-07-06 Snecma Stator de compresseur a haute pression
US6382905B1 (en) * 2000-04-28 2002-05-07 General Electric Company Fan casing liner support
GB0015207D0 (en) * 2000-06-21 2000-08-09 Neyrfor Weir Ltd A turbine
US6896483B2 (en) * 2001-07-02 2005-05-24 Allison Advanced Development Company Blade track assembly
US6733235B2 (en) * 2002-03-28 2004-05-11 General Electric Company Shroud segment and assembly for a turbine engine
US7013718B2 (en) * 2003-04-28 2006-03-21 Watson Cogeneration Company Method for monitoring the performance of a turbine
NZ585538A (en) * 2004-05-17 2011-09-30 Carlton Forge Works Turbine case reinforcement in a gas turbine jet engine
GB2416194B (en) * 2004-07-15 2006-08-16 Rolls Royce Plc A spacer arrangement
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
US7484927B2 (en) * 2006-04-14 2009-02-03 General Electric Company Steam turbine variable clearance packing
US7686569B2 (en) * 2006-12-04 2010-03-30 Siemens Energy, Inc. Blade clearance system for a turbine engine
US8231338B2 (en) 2009-05-05 2012-07-31 General Electric Company Turbine shell with pin support
CA2860928C (en) * 2012-01-26 2016-10-18 Alstom Technology Ltd. Stator component with segmented inner ring for a turbomachine
US9587507B2 (en) * 2013-02-23 2017-03-07 Rolls-Royce North American Technologies, Inc. Blade clearance control for gas turbine engine
DE102013210876B4 (de) * 2013-06-11 2015-02-26 MTU Aero Engines AG Verbundbauteil zur thermischen Spaltsteuerung in einer Strömungsmaschine sowie dieses enthaltende Strömungsmaschine
DE102013212741A1 (de) * 2013-06-28 2014-12-31 Siemens Aktiengesellschaft Gasturbine und Hitzeschild für eine Gasturbine
FR3011608B1 (fr) * 2013-10-09 2016-05-27 Snecma Joint a labyrinthe et machine tournante comprenant un tel joint
US10696906B2 (en) 2017-09-29 2020-06-30 Marathon Petroleum Company Lp Tower bottoms coke catching device
US12000720B2 (en) 2018-09-10 2024-06-04 Marathon Petroleum Company Lp Product inventory monitoring
US10815816B2 (en) * 2018-09-24 2020-10-27 General Electric Company Containment case active clearance control structure
US12031676B2 (en) 2019-03-25 2024-07-09 Marathon Petroleum Company Lp Insulation securement system and associated methods
US11008882B2 (en) * 2019-04-18 2021-05-18 Rolls-Royce North American Technologies Inc. Blade tip clearance assembly
US11975316B2 (en) 2019-05-09 2024-05-07 Marathon Petroleum Company Lp Methods and reforming systems for re-dispersing platinum on reforming catalyst
US20200378600A1 (en) 2019-05-30 2020-12-03 Marathon Petroleum Company Lp Methods and systems for minimizing NOx and CO emissions in natural draft heaters
US11384301B2 (en) 2020-02-19 2022-07-12 Marathon Petroleum Company Lp Low sulfur fuel oil blends for stability enhancement and associated methods
US11898109B2 (en) 2021-02-25 2024-02-13 Marathon Petroleum Company Lp Assemblies and methods for enhancing control of hydrotreating and fluid catalytic cracking (FCC) processes using spectroscopic analyzers
US20220268694A1 (en) 2021-02-25 2022-08-25 Marathon Petroleum Company Lp Methods and assemblies for determining and using standardized spectral responses for calibration of spectroscopic analyzers
US11702600B2 (en) 2021-02-25 2023-07-18 Marathon Petroleum Company Lp Assemblies and methods for enhancing fluid catalytic cracking (FCC) processes during the FCC process using spectroscopic analyzers
US11905468B2 (en) 2021-02-25 2024-02-20 Marathon Petroleum Company Lp Assemblies and methods for enhancing control of fluid catalytic cracking (FCC) processes using spectroscopic analyzers
US11692141B2 (en) 2021-10-10 2023-07-04 Marathon Petroleum Company Lp Methods and systems for enhancing processing of hydrocarbons in a fluid catalytic cracking unit using a renewable additive
US11802257B2 (en) 2022-01-31 2023-10-31 Marathon Petroleum Company Lp Systems and methods for reducing rendered fats pour point
US12311305B2 (en) 2022-12-08 2025-05-27 Marathon Petroleum Company Lp Removable flue gas strainer and associated methods
US12306076B2 (en) 2023-05-12 2025-05-20 Marathon Petroleum Company Lp Systems, apparatuses, and methods for sample cylinder inspection, pressurization, and sample disposal

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US2555256A (en) * 1948-04-14 1951-05-29 Nat Tube Co Pipe-line pipe
NL202529A (enrdf_load_html_response) * 1954-12-16
US2962256A (en) * 1956-03-28 1960-11-29 Napier & Son Ltd Turbine blade shroud rings
FR1247283A (fr) * 1959-02-09 1960-11-25 Westinghouse Electric Corp Appareillage de turbine
US3085398A (en) * 1961-01-10 1963-04-16 Gen Electric Variable-clearance shroud structure for gas turbine engines
US3430898A (en) * 1967-05-01 1969-03-04 Us Navy Leading edge for hypersonic vehicle

Also Published As

Publication number Publication date
JPS4863111A (enrdf_load_html_response) 1973-09-03
SE385941B (sv) 1976-07-26
DE2258480A1 (de) 1973-06-07
US3854843A (en) 1974-12-17
AU463454B2 (en) 1975-07-24
BE792224A (fr) 1973-03-30
CH561354A5 (enrdf_load_html_response) 1975-04-30
NL7216110A (enrdf_load_html_response) 1973-06-05
FR2164215A5 (enrdf_load_html_response) 1973-07-27
JPS5138371B2 (enrdf_load_html_response) 1976-10-21
AU4931272A (en) 1974-06-06
CA989312A (en) 1976-05-18
GB1363897A (en) 1974-08-21

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