SA515360329B1 - التحكم في درجة الحرارة في تجويف خاص بمحرك تربين - Google Patents
التحكم في درجة الحرارة في تجويف خاص بمحرك تربينInfo
- Publication number
- SA515360329B1 SA515360329B1 SA515360329A SA515360329A SA515360329B1 SA 515360329 B1 SA515360329 B1 SA 515360329B1 SA 515360329 A SA515360329 A SA 515360329A SA 515360329 A SA515360329 A SA 515360329A SA 515360329 B1 SA515360329 B1 SA 515360329B1
- Authority
- SA
- Saudi Arabia
- Prior art keywords
- flow
- medium
- space
- cavity
- temperature control
- Prior art date
Links
- 239000000543 intermediate Substances 0.000 abstract 4
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
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/601—Fluid transfer using an ejector or a jet pump
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
Abstract
يتعلق الاختراع الحالي بمحرك تربين turbine engine يتضمن حيز متوسط interme¬diate space محدد بين أجزاء خارجية وداخلية من محرك التربين. يتم توفير مزود طاقة تدفق flow energizer بما في ذلك جسم تدفق flow body موضوع في الحيز المتوسط ويتضمن منفذ دخول inlet port، منفذ خروج outlet port وممر تدفق flow passage يمتد في جسم التدفق بين منافذ الدخول والخروج inlet and outlet ports. يستقبل منفذ الدخول تدفق وسط أول موضوع في الحيز المتوسط ويقوم جسم التدفق بحقن تدفق مزود بالطاقة خاص بالوسط الثاني في جزء من الوسط الأول في جسم التدفق لخلق تدفق مزود بالطاقة لوسط مخلوط mixed medium من منفذ الخروج، ويقوم التدفق المزود بالطاقة energized flow الخاص بالوسط المخلوط بخلق تدفق الوسط الأول بجوار جسم التدفق في الحيز المتوسط. شكل 2
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/663,737 US9091171B2 (en) | 2012-10-30 | 2012-10-30 | Temperature control within a cavity of a turbine engine |
PCT/US2013/064903 WO2014070436A2 (en) | 2012-10-30 | 2013-10-15 | Temperature control within a cavity of a turbine engine |
Publications (1)
Publication Number | Publication Date |
---|---|
SA515360329B1 true SA515360329B1 (ar) | 2016-05-25 |
Family
ID=49950020
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SA515360329A SA515360329B1 (ar) | 2012-10-30 | 2015-04-23 | التحكم في درجة الحرارة في تجويف خاص بمحرك تربين |
Country Status (7)
Country | Link |
---|---|
US (1) | US9091171B2 (ar) |
EP (1) | EP2914815A2 (ar) |
JP (1) | JP2015533994A (ar) |
CN (1) | CN104769225A (ar) |
IN (1) | IN2015DN02803A (ar) |
SA (1) | SA515360329B1 (ar) |
WO (1) | WO2014070436A2 (ar) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2014175969A2 (en) * | 2013-03-13 | 2014-10-30 | United Technologies Corporation | Engine mid-turbine frame transfer tube for low pressure turbine case cooling |
US20140321981A1 (en) * | 2013-04-26 | 2014-10-30 | Jose L. Rodriguez | Turbine engine shutdown temperature control system |
JP6324548B2 (ja) * | 2014-06-10 | 2018-05-16 | シーメンス エナジー インコーポレイテッド | 排気ディフューザ内にロータセンタリング冷却システムを備えるガスタービンエンジン |
DE102014011042A1 (de) * | 2014-07-26 | 2016-01-28 | Man Diesel & Turbo Se | Strömungsmaschine |
JP6399894B2 (ja) * | 2014-10-29 | 2018-10-03 | 三菱日立パワーシステムズ株式会社 | 排気装置及びガスタービン |
GB201420966D0 (en) * | 2014-11-26 | 2015-01-07 | Rolls Royce Plc | Compressor cooling |
US9790860B2 (en) * | 2015-01-16 | 2017-10-17 | United Technologies Corporation | Cooling passages for a mid-turbine frame |
FR3039207B1 (fr) * | 2015-07-21 | 2019-07-26 | Safran Aircraft Engines | Carter d'echappement d'une turbomachine a duree de vie augmentee |
US10443449B2 (en) | 2015-07-24 | 2019-10-15 | Pratt & Whitney Canada Corp. | Spoke mounting arrangement |
US10920612B2 (en) * | 2015-07-24 | 2021-02-16 | Pratt & Whitney Canada Corp. | Mid-turbine frame spoke cooling system and method |
US20170306846A1 (en) * | 2016-04-22 | 2017-10-26 | General Electric Company | Ventilation system for turbomachine using bladeless airflow amplifier |
US20170306845A1 (en) * | 2016-04-22 | 2017-10-26 | General Electric Company | Ventilation system for turbomachine using bladeless airflow amplifier |
US10583933B2 (en) * | 2016-10-03 | 2020-03-10 | General Electric Company | Method and apparatus for undercowl flow diversion cooling |
CN107559091A (zh) * | 2017-08-28 | 2018-01-09 | 陈佳伟 | 一种燃气轮机 |
US11346249B2 (en) * | 2019-03-05 | 2022-05-31 | Pratt & Whitney Canada Corp. | Gas turbine engine with feed pipe for bearing housing |
US11326519B2 (en) * | 2020-02-25 | 2022-05-10 | General Electric Company | Frame for a heat engine |
US11047306B1 (en) | 2020-02-25 | 2021-06-29 | General Electric Company | Gas turbine engine reverse bleed for coking abatement |
US11525400B2 (en) | 2020-07-08 | 2022-12-13 | General Electric Company | System for rotor assembly thermal gradient reduction |
US12031484B2 (en) | 2021-01-28 | 2024-07-09 | General Electric Company | Gas turbine engine cooling system control |
US11473439B1 (en) * | 2021-09-23 | 2022-10-18 | General Electric Company | Gas turbine engine with hollow rotor in fluid communication with a balance piston cavity |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3631672A (en) * | 1969-08-04 | 1972-01-04 | Gen Electric | Eductor cooled gas turbine casing |
US4351150A (en) * | 1980-02-25 | 1982-09-28 | General Electric Company | Auxiliary air system for gas turbine engine |
US4765373A (en) | 1987-07-07 | 1988-08-23 | Coppus Engineering Corporation | Gas flow amplifier |
FR2766231B1 (fr) | 1997-07-18 | 1999-08-20 | Snecma | Dispositif d'echauffement ou de refroidissement d'un carter circulaire |
JP2002523661A (ja) * | 1998-08-18 | 2002-07-30 | シーメンス アクチエンゲゼルシヤフト | タービン車室 |
US6379108B1 (en) | 2000-08-08 | 2002-04-30 | General Electric Company | Controlling a rabbet load and air/oil seal temperatures in a turbine |
DE10233113A1 (de) | 2001-10-30 | 2003-05-15 | Alstom Switzerland Ltd | Turbomaschine |
WO2004090291A1 (de) | 2003-04-07 | 2004-10-21 | Alstom Technology Ltd | Turbomaschine |
US7124590B2 (en) * | 2003-10-03 | 2006-10-24 | United Technologies Corporation | Ejector for cooling air supply pressure optimization |
DE10352089A1 (de) | 2003-11-07 | 2005-06-09 | Alstom Technology Ltd | Verfahren zum Betreiben einer Turbomaschine, und Turbomaschine |
JP2006037855A (ja) * | 2004-07-28 | 2006-02-09 | Mitsubishi Heavy Ind Ltd | 車室ケーシング及びガスタービン |
FR2891300A1 (fr) * | 2005-09-23 | 2007-03-30 | Snecma Sa | Dispositif de controle de jeu dans une turbine a gaz |
JP5118496B2 (ja) * | 2008-01-10 | 2013-01-16 | 三菱重工業株式会社 | ガスタービンの排気部の構造およびガスタービン |
JP4969500B2 (ja) * | 2008-03-28 | 2012-07-04 | 三菱重工業株式会社 | ガスタービン |
IT1395820B1 (it) * | 2009-09-25 | 2012-10-26 | Nuovo Pignone Spa | Sistema di raffreddamento per una turbina a gas e relativo metodo di funzionamento |
JP4958967B2 (ja) * | 2009-12-15 | 2012-06-20 | 川崎重工業株式会社 | 換気構造を改良したガスタービンエンジン |
-
2012
- 2012-10-30 US US13/663,737 patent/US9091171B2/en not_active Expired - Fee Related
-
2013
- 2013-10-15 IN IN2803DEN2015 patent/IN2015DN02803A/en unknown
- 2013-10-15 CN CN201380056386.1A patent/CN104769225A/zh active Pending
- 2013-10-15 EP EP13819105.1A patent/EP2914815A2/en not_active Withdrawn
- 2013-10-15 WO PCT/US2013/064903 patent/WO2014070436A2/en active Application Filing
- 2013-10-15 JP JP2015539652A patent/JP2015533994A/ja active Pending
-
2015
- 2015-04-23 SA SA515360329A patent/SA515360329B1/ar unknown
Also Published As
Publication number | Publication date |
---|---|
JP2015533994A (ja) | 2015-11-26 |
EP2914815A2 (en) | 2015-09-09 |
US20140119880A1 (en) | 2014-05-01 |
WO2014070436A3 (en) | 2014-07-24 |
WO2014070436A2 (en) | 2014-05-08 |
CN104769225A (zh) | 2015-07-08 |
US9091171B2 (en) | 2015-07-28 |
IN2015DN02803A (ar) | 2015-09-04 |
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