CN102373972B - 尖部流道轮廓 - Google Patents

尖部流道轮廓 Download PDF

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Publication number
CN102373972B
CN102373972B CN201110280191.8A CN201110280191A CN102373972B CN 102373972 B CN102373972 B CN 102373972B CN 201110280191 A CN201110280191 A CN 201110280191A CN 102373972 B CN102373972 B CN 102373972B
Authority
CN
China
Prior art keywords
turbine
trailing edge
diffuser
tip
movable vane
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.)
Active
Application number
CN201110280191.8A
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English (en)
Chinese (zh)
Other versions
CN102373972A (zh
Inventor
G·L·塞登
C·A·比勒
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 Company PLC
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=45592968&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=CN102373972(B) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by General Electric Co filed Critical General Electric Co
Publication of CN102373972A publication Critical patent/CN102373972A/zh
Application granted granted Critical
Publication of CN102373972B publication Critical patent/CN102373972B/zh
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Classifications

    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • 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
    • 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
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F01D5/143—Contour of the outer or inner working fluid flow path wall, i.e. shroud or hub contour
    • 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
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CN201110280191.8A 2010-08-20 2011-08-19 尖部流道轮廓 Active CN102373972B (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/859970 2010-08-20
US12/859,970 US8628297B2 (en) 2010-08-20 2010-08-20 Tip flowpath contour

Publications (2)

Publication Number Publication Date
CN102373972A CN102373972A (zh) 2012-03-14
CN102373972B true CN102373972B (zh) 2015-11-25

Family

ID=45592968

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110280191.8A Active CN102373972B (zh) 2010-08-20 2011-08-19 尖部流道轮廓

Country Status (5)

Country Link
US (1) US8628297B2 (enExample)
JP (1) JP6018368B2 (enExample)
CN (1) CN102373972B (enExample)
CH (1) CH703654B1 (enExample)
DE (1) DE102011052672A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8628297B2 (en) * 2010-08-20 2014-01-14 General Electric Company Tip flowpath contour
JP6033154B2 (ja) * 2013-03-29 2016-11-30 三菱重工業株式会社 軸流回転機械、及びディフューザ
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
WO2016001002A1 (de) * 2014-07-03 2016-01-07 Abb Turbo Systems Ag Abströmbereich einer turbine eines abgasturboladers
US10329945B2 (en) * 2015-04-21 2019-06-25 Siemens Energy, Inc. High performance robust gas turbine exhaust with variable (adaptive) exhaust diffuser geometry
CN109284533B (zh) * 2018-08-09 2023-05-23 中国航发沈阳发动机研究所 航改燃气轮机流道计算方法
JP7692988B2 (ja) * 2021-03-24 2025-06-16 三菱重工業株式会社 ガスタービン

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1123879A (zh) * 1994-08-23 1996-06-05 株式会社日立制作所 联合循环发电站
CN1987066A (zh) * 2005-12-21 2007-06-27 通用电气公司 紧凑型增压排气涡轮风扇发动机
CN101010489A (zh) * 2004-07-02 2007-08-01 西门子公司 废气扩散器壁部轮廓
CN102373972A (zh) * 2010-08-20 2012-03-14 通用电气公司 尖部流道轮廓

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2806645A (en) 1951-03-02 1957-09-17 Edward A Stalker Radial diffusion compressors
CH484358A (de) 1968-02-15 1970-01-15 Escher Wyss Ag Abströmgehäuse einer axialen Turbomaschine
US3746469A (en) * 1971-03-03 1973-07-17 Gen Motors Corp Turbomachine rotor
US5203674A (en) 1982-11-23 1993-04-20 Nuovo Pignone S.P.A. Compact diffuser, particularly suitable for high-power gas turbines
CH672004A5 (enExample) * 1986-09-26 1989-10-13 Bbc Brown Boveri & Cie
DE3736836A1 (de) 1987-10-30 1989-05-11 Bbc Brown Boveri & Cie Axial durchstroemte gasturbine
DE59204947D1 (de) * 1992-08-03 1996-02-15 Asea Brown Boveri Mehrzoniger Diffusor für Turbomaschine
DE4422700A1 (de) 1994-06-29 1996-01-04 Abb Management Ag Diffusor für Turbomaschine
US5632142A (en) * 1995-02-15 1997-05-27 Surette; Robert G. Stationary gas turbine power system and related method
JPH08260905A (ja) * 1995-03-28 1996-10-08 Mitsubishi Heavy Ind Ltd 軸流タービン用排気ディフューザ
GB9823840D0 (en) * 1998-10-30 1998-12-23 Rolls Royce Plc Bladed ducting for turbomachinery
DE19905994A1 (de) * 1999-02-15 2000-08-24 Peter Kraus Vorrichtung und Verfahren zur Aufhebung von Stoß-Grenzschicht-Oszillationen bei kreisringförmigen Diffusoren (axial-radial) an Dampfturbinen
US6488470B1 (en) 1999-08-03 2002-12-03 Jerzy A. Owczarek Annular flow diffusers for gas turbines
JP3912989B2 (ja) 2001-01-25 2007-05-09 三菱重工業株式会社 ガスタービン
JP3564420B2 (ja) * 2001-04-27 2004-09-08 三菱重工業株式会社 ガスタービン
GB2384276A (en) * 2002-01-18 2003-07-23 Alstom Gas turbine low pressure stage
US20040109756A1 (en) 2002-12-09 2004-06-10 Mitsubishi Heavy Industries Ltd. Gas turbine
US7272930B2 (en) * 2003-09-25 2007-09-25 Siemens Power Generation Exhaust diffuser assembly with tunable velocity profile
JP2006291975A (ja) * 2006-08-03 2006-10-26 Mitsubishi Heavy Ind Ltd ガスタービン

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1123879A (zh) * 1994-08-23 1996-06-05 株式会社日立制作所 联合循环发电站
CN101010489A (zh) * 2004-07-02 2007-08-01 西门子公司 废气扩散器壁部轮廓
CN1987066A (zh) * 2005-12-21 2007-06-27 通用电气公司 紧凑型增压排气涡轮风扇发动机
CN102373972A (zh) * 2010-08-20 2012-03-14 通用电气公司 尖部流道轮廓

Also Published As

Publication number Publication date
US8628297B2 (en) 2014-01-14
US20120042654A1 (en) 2012-02-23
CH703654B1 (de) 2015-06-15
JP2012041925A (ja) 2012-03-01
CN102373972A (zh) 2012-03-14
DE102011052672A1 (de) 2012-03-29
JP6018368B2 (ja) 2016-11-02
CH703654A2 (de) 2012-02-29

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SE01 Entry into force of request for substantive examination
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Effective date of registration: 20240114

Address after: Swiss Baden

Patentee after: GENERAL ELECTRIC CO. LTD.

Address before: New York, United States

Patentee before: General Electric Co.

TR01 Transfer of patent right