CN103711531B - 燃气涡轮机的废气扩散器 - Google Patents

燃气涡轮机的废气扩散器 Download PDF

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Publication number
CN103711531B
CN103711531B CN201310456329.4A CN201310456329A CN103711531B CN 103711531 B CN103711531 B CN 103711531B CN 201310456329 A CN201310456329 A CN 201310456329A CN 103711531 B CN103711531 B CN 103711531B
Authority
CN
China
Prior art keywords
strut
leading edge
turbulator
exhaust gas
width
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 - Fee Related
Application number
CN201310456329.4A
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English (en)
Chinese (zh)
Other versions
CN103711531A (zh
Inventor
M.B.陈加帕
M.苏布拉马尼彦
V.拉哈克里什南
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of CN103711531A publication Critical patent/CN103711531A/zh
Application granted granted Critical
Publication of CN103711531B publication Critical patent/CN103711531B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F01D25/30—Exhaust heads, chambers, or the like
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/127—Vortex generators, turbulators, or the like, for mixing

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CN201310456329.4A 2012-10-05 2013-09-29 燃气涡轮机的废气扩散器 Expired - Fee Related CN103711531B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/646003 2012-10-05
US13/646,003 US9359900B2 (en) 2012-10-05 2012-10-05 Exhaust diffuser

Publications (2)

Publication Number Publication Date
CN103711531A CN103711531A (zh) 2014-04-09
CN103711531B true CN103711531B (zh) 2017-06-09

Family

ID=49322240

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201310456329.4A Expired - Fee Related CN103711531B (zh) 2012-10-05 2013-09-29 燃气涡轮机的废气扩散器

Country Status (4)

Country Link
US (1) US9359900B2 (enExample)
EP (1) EP2716865A1 (enExample)
JP (1) JP2014077441A (enExample)
CN (1) CN103711531B (enExample)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130170969A1 (en) * 2012-01-04 2013-07-04 General Electric Company Turbine Diffuser
US10255406B2 (en) * 2015-02-24 2019-04-09 Siemens Corporation Designing the geometry of a gas turbine exhaust diffuser on the basis of fluid dynamics information
US10151325B2 (en) * 2015-04-08 2018-12-11 General Electric Company Gas turbine diffuser strut including a trailing edge flap and methods of assembling the same
MX392790B (es) 2015-04-08 2025-03-24 Horton Inc Caracteristicas de superficie de aspa de ventilador.
JP6546481B2 (ja) 2015-08-31 2019-07-17 川崎重工業株式会社 排気ディフューザ
US10767508B2 (en) * 2016-02-09 2020-09-08 Mitsubishi Heavy Industries Compressor Corporation Gas expander
US10563543B2 (en) 2016-05-31 2020-02-18 General Electric Company Exhaust diffuser
US10982544B2 (en) * 2016-12-26 2021-04-20 Mitsubishi Heavy Industries, Ltd. Turbine and gas turbine
KR101902240B1 (ko) * 2017-04-18 2018-09-28 두산중공업 주식회사 가변형 가이드 베인을 포함하는 배기 디퓨저 및 이를 포함하는 가스터빈
KR102403823B1 (ko) * 2019-12-13 2022-05-30 두산에너빌리티 주식회사 스트립이 형성된 배기 디퓨져의 스트롯 구조 및 가스터빈
DE102020203547A1 (de) * 2020-03-19 2021-09-23 Siemens Aktiengesellschaft Verfahren zum Anpassen einer Turbinenanordnung, Verkleidung, Satz mit mehreren Verkleidungen, Verwendung und Diffusor
IT202100002240A1 (it) * 2021-02-02 2022-08-02 Gen Electric Motore a turbine con palette a flusso trasversale ridotto
EP4374046B1 (fr) * 2021-07-21 2025-04-30 Safran Aero Boosters Turbomachine pour aeronef avec echangeur de chaleur
BE1029617B1 (fr) * 2021-07-21 2023-02-20 Safran Aero Boosters Turbomachine pour aeronef avec echangeur de chaleur

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3012709A (en) * 1955-05-18 1961-12-12 Daimler Benz Ag Blade for axial compressors
BE638547A (enExample) 1962-10-29 1900-01-01
US4128363A (en) * 1975-04-30 1978-12-05 Kabushiki Kaisha Toyota Chuo Kenkyusho Axial flow fan
DE3609541A1 (de) 1986-03-21 1987-09-24 Deutsche Forsch Luft Raumfahrt Verminderten stroemungswiderstand durch herabgesetzte wandschubspannung aufweisende oberflaeche eines turbolent ueberstroemten koerpers
US5851105A (en) 1995-06-28 1998-12-22 General Electric Company Tapered strut frame
DE19834647C2 (de) 1998-07-31 2000-06-29 Deutsch Zentr Luft & Raumfahrt Schaufelanordnung für eine Strömungsmaschine
US6792758B2 (en) 2002-11-07 2004-09-21 Siemens Westinghouse Power Corporation Variable exhaust struts shields
US20040109756A1 (en) 2002-12-09 2004-06-10 Mitsubishi Heavy Industries Ltd. Gas turbine
US6866479B2 (en) 2003-05-16 2005-03-15 Mitsubishi Heavy Industries, Ltd. Exhaust diffuser for axial-flow turbine
GB2402717B (en) 2003-06-10 2006-05-10 Rolls Royce Plc A vane assembly for a gas turbine engine
WO2005100752A1 (en) 2004-04-09 2005-10-27 Norris Thomas R Externally mounted vortex generators for flow duct passage
US20100186415A1 (en) * 2009-01-23 2010-07-29 General Electric Company Turbulated aft-end liner assembly and related cooling method
US20110232291A1 (en) 2010-03-26 2011-09-29 General Electric Company System and method for an exhaust diffuser
US8578696B2 (en) * 2010-08-03 2013-11-12 General Electric Company Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine

Also Published As

Publication number Publication date
JP2014077441A (ja) 2014-05-01
CN103711531A (zh) 2014-04-09
US9359900B2 (en) 2016-06-07
EP2716865A1 (en) 2014-04-09
US20140096500A1 (en) 2014-04-10

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Granted publication date: 20170609

Termination date: 20180929