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SA515360329B1 - التحكم في درجة الحرارة في تجويف خاص بمحرك تربين - Google Patents

التحكم في درجة الحرارة في تجويف خاص بمحرك تربين

Info

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
Application number
SA515360329A
Other languages
English (en)
Inventor
جوس ال. رودريجوز،
جيبينج زهانج،
عبداللطيف ام. شهاب،
ديفيد ايه. ليتل،
Original Assignee
سيمينس اكتنجسلشافت
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 سيمينس اكتنجسلشافت filed Critical سيمينس اكتنجسلشافت
Publication of SA515360329B1 publication Critical patent/SA515360329B1/ar

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/06Fluid supply conduits to nozzles or the like
    • F01D9/065Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/60Fluid transfer
    • F05D2260/601Fluid 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
SA515360329A 2012-10-30 2015-04-23 التحكم في درجة الحرارة في تجويف خاص بمحرك تربين SA515360329B1 (ar)

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)

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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

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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
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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
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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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