JPS61142334A - ガスタービン構造 - Google Patents
ガスタービン構造Info
- Publication number
- JPS61142334A JPS61142334A JP60280866A JP28086685A JPS61142334A JP S61142334 A JPS61142334 A JP S61142334A JP 60280866 A JP60280866 A JP 60280866A JP 28086685 A JP28086685 A JP 28086685A JP S61142334 A JPS61142334 A JP S61142334A
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- seal
- disk
- compressor
- rotor
- 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.)
- Granted
Links
- 238000002485 combustion reaction Methods 0.000 description 10
- 238000001816 cooling Methods 0.000 description 10
- 238000007789 sealing Methods 0.000 description 5
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 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
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Supercharger (AREA)
- Separation By Low-Temperature Treatments (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US681332 | 1984-12-13 | ||
| US06/681,332 US4697981A (en) | 1984-12-13 | 1984-12-13 | Rotor thrust balancing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS61142334A true JPS61142334A (ja) | 1986-06-30 |
| JPH0580574B2 JPH0580574B2 (enExample) | 1993-11-09 |
Family
ID=24734825
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP60280866A Granted JPS61142334A (ja) | 1984-12-13 | 1985-12-13 | ガスタービン構造 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US4697981A (enExample) |
| EP (1) | EP0184975B1 (enExample) |
| JP (1) | JPS61142334A (enExample) |
| CA (1) | CA1225334A (enExample) |
| DE (2) | DE184975T1 (enExample) |
| IL (1) | IL77318A (enExample) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007184187A (ja) * | 2006-01-10 | 2007-07-19 | Mitsubishi Cable Ind Ltd | 可撓グロメット管 |
| JP2010151133A (ja) * | 2008-12-23 | 2010-07-08 | General Electric Co <Ge> | 遠心圧縮機前方スラスト及びタービン冷却装置 |
Families Citing this family (43)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA1326476C (en) * | 1988-09-30 | 1994-01-25 | Vaclav Kulle | Gas compressor having dry gas seals for balancing end thrust |
| CA1309996C (en) * | 1988-12-13 | 1992-11-10 | Vaclav Kulle | Axial thrust reducing arrangement for gas compressor having an overhung impeller shaft |
| US5150567A (en) * | 1989-06-05 | 1992-09-29 | General Electric Company | Gas turbine powerplant |
| US5051637A (en) * | 1990-03-20 | 1991-09-24 | Nova Corporation Of Alberta | Flux control techniques for magnetic bearing |
| US5154048A (en) * | 1990-10-01 | 1992-10-13 | General Electric Company | Apparatus for thrust balancing and frame heating |
| US5167484A (en) * | 1990-10-01 | 1992-12-01 | General Electric Company | Method for thrust balancing and frame heating |
| FR2708044B1 (fr) * | 1993-07-21 | 1995-09-01 | Snecma | Turbomachine comportant un dispositif de mesure de la poussée axiale d'un rotor. |
| US5760289A (en) * | 1996-01-02 | 1998-06-02 | General Electric Company | System for balancing loads on a thrust bearing of a gas turbine engine rotor and process for calibrating control therefor |
| US5862666A (en) * | 1996-12-23 | 1999-01-26 | Pratt & Whitney Canada Inc. | Turbine engine having improved thrust bearing load control |
| US6035627A (en) * | 1998-04-21 | 2000-03-14 | Pratt & Whitney Canada Inc. | Turbine engine with cooled P3 air to impeller rear cavity |
| US6227801B1 (en) | 1999-04-27 | 2001-05-08 | Pratt & Whitney Canada Corp. | Turbine engine having improved high pressure turbine cooling |
| US6457933B1 (en) | 2000-12-22 | 2002-10-01 | General Electric Company | Methods and apparatus for controlling bearing loads within bearing assemblies |
| RU2224905C2 (ru) * | 2001-07-27 | 2004-02-27 | Открытое акционерное общество "Авиадвигатель" | Двухконтурный газотурбинный двигатель |
| DE10358625A1 (de) * | 2003-12-11 | 2005-07-07 | Rolls-Royce Deutschland Ltd & Co Kg | Anordnung zur Lagerentlastung in einer Gasturbine |
| US20070122265A1 (en) * | 2005-11-30 | 2007-05-31 | General Electric Company | Rotor thrust balancing apparatus and method |
| US8087249B2 (en) * | 2008-12-23 | 2012-01-03 | General Electric Company | Turbine cooling air from a centrifugal compressor |
| EP2419621A4 (en) | 2009-04-17 | 2015-03-04 | Echogen Power Systems | SYSTEM AND METHOD FOR MANAGING HEAT PROBLEMS IN GAS TURBINE ENGINES |
| US8182201B2 (en) * | 2009-04-24 | 2012-05-22 | Pratt & Whitney Canada Corp. | Load distribution system for gas turbine engine |
| EP2446122B1 (en) | 2009-06-22 | 2017-08-16 | Echogen Power Systems, Inc. | System and method for managing thermal issues in one or more industrial processes |
| US8434994B2 (en) | 2009-08-03 | 2013-05-07 | General Electric Company | System and method for modifying rotor thrust |
| WO2011017476A1 (en) | 2009-08-04 | 2011-02-10 | Echogen Power Systems Inc. | Heat pump with integral solar collector |
| US8813497B2 (en) | 2009-09-17 | 2014-08-26 | Echogen Power Systems, Llc | Automated mass management control |
| US9115605B2 (en) | 2009-09-17 | 2015-08-25 | Echogen Power Systems, Llc | Thermal energy conversion device |
| US8613195B2 (en) | 2009-09-17 | 2013-12-24 | Echogen Power Systems, Llc | Heat engine and heat to electricity systems and methods with working fluid mass management control |
| US8869531B2 (en) | 2009-09-17 | 2014-10-28 | Echogen Power Systems, Llc | Heat engines with cascade cycles |
| US8857186B2 (en) | 2010-11-29 | 2014-10-14 | Echogen Power Systems, L.L.C. | Heat engine cycles for high ambient conditions |
| US8616001B2 (en) | 2010-11-29 | 2013-12-31 | Echogen Power Systems, Llc | Driven starter pump and start sequence |
| US10119476B2 (en) * | 2011-09-16 | 2018-11-06 | United Technologies Corporation | Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
| WO2013055391A1 (en) | 2011-10-03 | 2013-04-18 | Echogen Power Systems, Llc | Carbon dioxide refrigeration cycle |
| US9447695B2 (en) * | 2012-03-01 | 2016-09-20 | United Technologies Corporation | Diffuser seal for geared turbofan or turboprop engines |
| CA2882290A1 (en) | 2012-08-20 | 2014-02-27 | Echogen Power Systems, L.L.C. | Supercritical working fluid circuit with a turbo pump and a start pump in series configuration |
| US9118226B2 (en) | 2012-10-12 | 2015-08-25 | Echogen Power Systems, Llc | Heat engine system with a supercritical working fluid and processes thereof |
| US9341084B2 (en) | 2012-10-12 | 2016-05-17 | Echogen Power Systems, Llc | Supercritical carbon dioxide power cycle for waste heat recovery |
| WO2014117068A1 (en) | 2013-01-28 | 2014-07-31 | Echogen Power Systems, L.L.C. | Methods for reducing wear on components of a heat engine system at startup |
| EP2948649B8 (en) | 2013-01-28 | 2021-02-24 | Echogen Power Systems (Delaware), Inc | Process for controlling a power turbine throttle valve during a supercritical carbon dioxide rankine cycle |
| CA2903784C (en) | 2013-03-04 | 2021-03-16 | Echogen Power Systems, L.L.C. | Heat engine systems with high net power supercritical carbon dioxide circuits |
| EP2971607B1 (en) | 2013-03-13 | 2019-06-26 | United Technologies Corporation | Fan drive thrust balance |
| WO2015076896A2 (en) * | 2013-09-10 | 2015-05-28 | United Technologies Corporation | Dual anti surge and anti rotation feature on first vane support |
| WO2016073252A1 (en) | 2014-11-03 | 2016-05-12 | Echogen Power Systems, L.L.C. | Active thrust management of a turbopump within a supercritical working fluid circuit in a heat engine system |
| US10883388B2 (en) | 2018-06-27 | 2021-01-05 | Echogen Power Systems Llc | Systems and methods for generating electricity via a pumped thermal energy storage system |
| US11435120B2 (en) | 2020-05-05 | 2022-09-06 | Echogen Power Systems (Delaware), Inc. | Split expansion heat pump cycle |
| US11629638B2 (en) | 2020-12-09 | 2023-04-18 | Supercritical Storage Company, Inc. | Three reservoir electric thermal energy storage system |
| AU2024289421A1 (en) | 2023-02-07 | 2025-09-11 | Supercritical Storage Company, Inc. | Waste heat integration into pumped thermal energy storage |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2647684A (en) * | 1947-03-13 | 1953-08-04 | Rolls Royce | Gas turbine engine |
| US2746671A (en) * | 1950-04-14 | 1956-05-22 | United Aircraft Corp | Compressor deicing and thrust balancing arrangement |
| US2791091A (en) * | 1950-05-15 | 1957-05-07 | Gen Motors Corp | Power plant cooling and thrust balancing systems |
| US2966296A (en) * | 1954-08-13 | 1960-12-27 | Rolls Royce | Gas-turbine engines with load balancing means |
| US3433020A (en) * | 1966-09-26 | 1969-03-18 | Gen Electric | Gas turbine engine rotors |
| GB1095109A (en) * | 1966-10-03 | 1967-12-13 | Rolls Royce | Improvements in or relating to gas turbine engines |
| US3505813A (en) * | 1968-05-31 | 1970-04-14 | Rolls Royce | Turbine engine with axial load balancing means for thrust bearing |
| US4268220A (en) * | 1979-03-05 | 1981-05-19 | General Motors Corporation | Thrust balancing |
| US4306834A (en) * | 1979-06-25 | 1981-12-22 | Westinghouse Electric Corp. | Balance piston and seal for gas turbine engine |
| US4483149A (en) * | 1982-05-20 | 1984-11-20 | United Technologies Corporation | Diffuser case for a gas turbine engine |
| US4542623A (en) * | 1983-12-23 | 1985-09-24 | United Technologies Corporation | Air cooler for providing buffer air to a bearing compartment |
-
1984
- 1984-12-13 US US06/681,332 patent/US4697981A/en not_active Expired - Lifetime
-
1985
- 1985-12-12 IL IL77318A patent/IL77318A/xx unknown
- 1985-12-12 DE DE198585630220T patent/DE184975T1/de active Pending
- 1985-12-12 DE DE8585630220T patent/DE3578001D1/de not_active Expired - Lifetime
- 1985-12-12 EP EP85630220A patent/EP0184975B1/en not_active Expired
- 1985-12-13 JP JP60280866A patent/JPS61142334A/ja active Granted
- 1985-12-13 CA CA000497631A patent/CA1225334A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2007184187A (ja) * | 2006-01-10 | 2007-07-19 | Mitsubishi Cable Ind Ltd | 可撓グロメット管 |
| JP2010151133A (ja) * | 2008-12-23 | 2010-07-08 | General Electric Co <Ge> | 遠心圧縮機前方スラスト及びタービン冷却装置 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0184975A1 (en) | 1986-06-18 |
| DE3578001D1 (de) | 1990-07-05 |
| EP0184975B1 (en) | 1990-05-30 |
| JPH0580574B2 (enExample) | 1993-11-09 |
| IL77318A (en) | 1991-06-30 |
| US4697981A (en) | 1987-10-06 |
| CA1225334A (en) | 1987-08-11 |
| DE184975T1 (de) | 1986-12-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS61142334A (ja) | ガスタービン構造 | |
| US4719747A (en) | Apparatus for optimizing the blade and sealing slots of a compressor of a gas turbine | |
| US5311734A (en) | System and method for improved engine cooling in conjunction with an improved gas bearing face seal assembly | |
| US5593277A (en) | Smart turbine shroud | |
| US5816776A (en) | Labyrinth disk with built-in stiffener for turbomachine rotor | |
| US5333993A (en) | Stator seal assembly providing improved clearance control | |
| US6883303B1 (en) | Aircraft engine with inter-turbine engine frame | |
| JP4204310B2 (ja) | タービン間エンジンフレームによって支持された二重反転式低圧タービンロータを備える航空機用エンジン | |
| US4329113A (en) | Temperature control device for gas turbines | |
| JP3105277B2 (ja) | 軸流式のガスタービン | |
| US3656862A (en) | Segmented seal assembly | |
| US8511986B2 (en) | Bearing mounting system in a low pressure turbine | |
| US4961309A (en) | Apparatus for venting the rotor structure of a compressor of a gas turbine power plant | |
| US4541775A (en) | Clearance control in turbine seals | |
| US2744722A (en) | Turbine bearing support | |
| EP0141770A1 (en) | Active clearance control | |
| US4668163A (en) | Automatic control device of a labyrinth seal clearance in a turbo-jet engine | |
| JPH06102988B2 (ja) | ガスタービン機関ケーシングの温度制御装置 | |
| JPS63134823A (ja) | 高圧圧縮機を備えたガスタービンジェット推進装置 | |
| US4264274A (en) | Apparatus maintaining rotor and stator clearance | |
| US2762559A (en) | Axial flow compressor with axially adjustable rotor | |
| US6067791A (en) | Turbine engine with a thermal valve | |
| GB2057573A (en) | Turbine rotor assembly | |
| US4310286A (en) | Rotor assembly having a multistage disk | |
| CN111322119B (zh) | 带有浮动护罩的涡轮发动机 |