GB1363897A - Composite elongate member having a predetermined effective coeffi cient of linear expansion - Google Patents
Composite elongate member having a predetermined effective coeffi cient of linear expansionInfo
- Publication number
- GB1363897A GB1363897A GB5566571A GB5566571A GB1363897A GB 1363897 A GB1363897 A GB 1363897A GB 5566571 A GB5566571 A GB 5566571A GB 5566571 A GB5566571 A GB 5566571A GB 1363897 A GB1363897 A GB 1363897A
- Authority
- GB
- United Kingdom
- Prior art keywords
- segments
- ring
- elongate member
- composite
- turbine
- 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.)
- Expired
Links
- 239000002131 composite material Substances 0.000 title abstract 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 abstract 4
- 239000000956 alloy Substances 0.000 abstract 2
- 229910045601 alloy Inorganic materials 0.000 abstract 2
- 239000000463 material Substances 0.000 abstract 2
- 229910052759 nickel Inorganic materials 0.000 abstract 2
- 229910052581 Si3N4 Inorganic materials 0.000 abstract 1
- 239000000919 ceramic Substances 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 abstract 1
- 210000002105 tongue Anatomy 0.000 abstract 1
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)
Priority Applications (12)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE792224D BE792224A (fr) | 1971-12-01 | Element composite long ayant un coefficient de dilatation lineaire effectif predetermine | |
GB5566571A GB1363897A (en) | 1971-12-01 | 1971-12-01 | Composite elongate member having a predetermined effective coeffi cient of linear expansion |
SE7215218A SE385941B (sv) | 1971-12-01 | 1972-11-22 | Statorholjesringenhet |
CA157,308A CA989312A (en) | 1971-12-01 | 1972-11-23 | Stator shroud ring assembly |
AU49312/72A AU463454B2 (en) | 1971-12-01 | 1972-11-27 | Composite elongate member having a predetermined effective coefficient of linear expansion |
US00309790A US3854843A (en) | 1971-12-01 | 1972-11-27 | Composite elongate member having a predetermined effective coefficient of linear expansion |
NL7216110A NL7216110A (enrdf_load_stackoverflow) | 1971-12-01 | 1972-11-28 | |
DE19722258480 DE2258480A1 (de) | 1971-12-01 | 1972-11-29 | Zusammengesetztes dehnungsteil |
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 |
CH1746672A CH561354A5 (enrdf_load_stackoverflow) | 1971-12-01 | 1972-11-30 | |
FR7242682A FR2164215A5 (enrdf_load_stackoverflow) | 1971-12-01 | 1972-11-30 | |
JP47119419A JPS5138371B2 (enrdf_load_stackoverflow) | 1971-12-01 | 1972-11-30 |
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 |
---|---|
GB1363897A true GB1363897A (en) | 1974-08-21 |
Family
ID=10474529
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5566571A Expired GB1363897A (en) | 1971-12-01 | 1971-12-01 | Composite elongate member having a predetermined effective coeffi cient of linear expansion |
Country Status (12)
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4411594A (en) * | 1979-06-30 | 1983-10-25 | Rolls-Royce Limited | Support member and a component supported thereby |
US4657479A (en) * | 1984-10-09 | 1987-04-14 | Rolls-Royce Plc | Rotor tip clearance control devices |
US5137421A (en) * | 1989-09-15 | 1992-08-11 | Rolls-Royce Plc | Shroud rings |
US6896483B2 (en) * | 2001-07-02 | 2005-05-24 | Allison Advanced Development Company | Blade track assembly |
CN110939517A (zh) * | 2018-09-24 | 2020-03-31 | 通用电气公司 | 包壳主动间隙控制结构 |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3986720A (en) * | 1975-04-14 | 1976-10-19 | General Electric Company | Turbine shroud structure |
JPS5242906U (enrdf_load_stackoverflow) * | 1975-09-22 | 1977-03-26 | ||
JPS52127105U (enrdf_load_stackoverflow) * | 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 |
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 |
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 |
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 |
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 |
EP2314831A1 (en) * | 2004-05-17 | 2011-04-27 | 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 |
KR20150002595A (ko) * | 2012-01-26 | 2015-01-07 | 알스톰 테크놀러지 리미티드 | 터보 기계를 위한 분할된 내부 링을 갖는 스테터 부품 |
WO2014130159A1 (en) * | 2013-02-23 | 2014-08-28 | Ottow Nathan W | 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 |
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 |
CA3081520C (en) | 2019-05-30 | 2023-10-31 | Marathon Petroleum Company Lp | Methods and systems for minimizing nox and co emissions in natural draft heaters |
US11352578B2 (en) | 2020-02-19 | 2022-06-07 | Marathon Petroleum Company Lp | Low sulfur fuel oil blends for stabtility enhancement and associated methods |
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 |
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 |
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 |
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 |
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 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2555256A (en) * | 1948-04-14 | 1951-05-29 | Nat Tube Co | Pipe-line pipe |
NL202529A (enrdf_load_stackoverflow) * | 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 |
-
0
- BE BE792224D patent/BE792224A/xx unknown
-
1971
- 1971-12-01 GB GB5566571A patent/GB1363897A/en not_active Expired
-
1972
- 1972-11-22 SE SE7215218A patent/SE385941B/xx unknown
- 1972-11-23 CA CA157,308A patent/CA989312A/en not_active Expired
- 1972-11-27 AU AU49312/72A patent/AU463454B2/en not_active Expired
- 1972-11-27 US US00309790A patent/US3854843A/en not_active Expired - Lifetime
- 1972-11-28 NL NL7216110A patent/NL7216110A/xx unknown
- 1972-11-29 DE DE19722258480 patent/DE2258480A1/de active Pending
- 1972-11-30 JP JP47119419A patent/JPS5138371B2/ja not_active Expired
- 1972-11-30 FR FR7242682A patent/FR2164215A5/fr not_active Expired
- 1972-11-30 IT IT70781/72A patent/IT975912B/it active
- 1972-11-30 CH CH1746672A patent/CH561354A5/xx not_active IP Right Cessation
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4411594A (en) * | 1979-06-30 | 1983-10-25 | Rolls-Royce Limited | Support member and a component supported thereby |
US4657479A (en) * | 1984-10-09 | 1987-04-14 | Rolls-Royce Plc | Rotor tip clearance control devices |
US5137421A (en) * | 1989-09-15 | 1992-08-11 | Rolls-Royce Plc | Shroud rings |
US6896483B2 (en) * | 2001-07-02 | 2005-05-24 | Allison Advanced Development Company | Blade track assembly |
CN110939517A (zh) * | 2018-09-24 | 2020-03-31 | 通用电气公司 | 包壳主动间隙控制结构 |
Also Published As
Publication number | Publication date |
---|---|
IT975912B (it) | 1974-08-10 |
CH561354A5 (enrdf_load_stackoverflow) | 1975-04-30 |
AU4931272A (en) | 1974-06-06 |
CA989312A (en) | 1976-05-18 |
SE385941B (sv) | 1976-07-26 |
JPS4863111A (enrdf_load_stackoverflow) | 1973-09-03 |
US3854843A (en) | 1974-12-17 |
BE792224A (fr) | 1973-03-30 |
AU463454B2 (en) | 1975-07-24 |
FR2164215A5 (enrdf_load_stackoverflow) | 1973-07-27 |
JPS5138371B2 (enrdf_load_stackoverflow) | 1976-10-21 |
DE2258480A1 (de) | 1973-06-07 |
NL7216110A (enrdf_load_stackoverflow) | 1973-06-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1363897A (en) | Composite elongate member having a predetermined effective coeffi cient of linear expansion | |
GB1512882A (en) | Bladed rotor assembly for a gas turbine engine | |
GB1195012A (en) | Rotor for Bladed Fluid Flow Machines. | |
GB1460714A (en) | Bladed rotor for a gas turbine engine | |
US5181827A (en) | Gas turbine engine shroud ring mounting | |
GB1506360A (en) | Ceramic turbine structures | |
GB1263857A (en) | Improvements relating to pivotal guide vanes | |
GB2042646B (en) | Rotor blade tip clearance control for gas turbine engine | |
GB1008526A (en) | Axial flow bladed rotor, e.g. for a turbine | |
GB1505534A (en) | Turbines and compressors | |
GB1507596A (en) | Partially divided turbine housing for example for turbochargers | |
GB1377788A (en) | Arrangement for retaining a ceramic turbine blade in a slotted steel rotor or blade seating ring | |
SE8904237L (sv) | Bultloes balansvikt till turbinrotorer | |
SE8502035D0 (sv) | Roterande tetning | |
GB2043796B (en) | Bladed rotor for gas turbine engine | |
GB1491556A (en) | Rotor blades for turbomachines | |
US5154575A (en) | Thermal blade tip clearance control for gas turbine engines | |
GB712112A (en) | Improvements in or relating to blade-locking means for turbine and the like rotor assemblies | |
GB1503453A (en) | Rotor of a turbomachine | |
GB1432994A (en) | Compressor for gas turbine engines | |
GB1187978A (en) | Improvements in or relating to Gas-Turbine Rotors. | |
GB749577A (en) | Improvements in or relating to blade ring assemblies for axial flow compressors or turbines | |
GB1491480A (en) | Fixing blades for fluid flow machines | |
GB1533556A (en) | Turbo-machine rotor wheel | |
GB1141280A (en) | Bladed rotor for a fluid flow machine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |