RU2575956C2 - Компрессор и соответствующая газовая турбина - Google Patents

Компрессор и соответствующая газовая турбина Download PDF

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Publication number
RU2575956C2
RU2575956C2 RU2013105342/06A RU2013105342A RU2575956C2 RU 2575956 C2 RU2575956 C2 RU 2575956C2 RU 2013105342/06 A RU2013105342/06 A RU 2013105342/06A RU 2013105342 A RU2013105342 A RU 2013105342A RU 2575956 C2 RU2575956 C2 RU 2575956C2
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RU
Russia
Prior art keywords
compressor
ring
inner ring
guide vanes
paragraphs
Prior art date
Application number
RU2013105342/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2013105342A (ru
Inventor
Томас БРАНДЕНБУРГ
Даниэль ЭКЕ
Маркус ХОФМАНН
Торстен МАТТИАС
Бернвард МЕРТЕНС
Франк МИЛЬДНЕР
Маркус ПАУС
Ахим ШИРРМАХЕР
Вадим ШЕВЧЕНКО
Уве ЗИБЕР
Хубертус Михаэль ВИГГЕР
Original Assignee
Сименс Акциенгезелльшафт
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.)
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Publication date
Application filed by Сименс Акциенгезелльшафт filed Critical Сименс Акциенгезелльшафт
Publication of RU2013105342A publication Critical patent/RU2013105342A/ru
Application granted granted Critical
Publication of RU2575956C2 publication Critical patent/RU2575956C2/ru

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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
    • 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
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Rotary Pumps (AREA)
RU2013105342/06A 2010-07-08 2011-07-07 Компрессор и соответствующая газовая турбина RU2575956C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP10007062.2 2010-07-08
EP10007062A EP2405104A1 (fr) 2010-07-08 2010-07-08 Compresseur et moteur à turbine à gaz associé
PCT/EP2011/061486 WO2012004336A2 (fr) 2010-07-08 2011-07-07 Compresseur

Publications (2)

Publication Number Publication Date
RU2013105342A RU2013105342A (ru) 2014-08-20
RU2575956C2 true RU2575956C2 (ru) 2016-02-27

Family

ID=43221935

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2013105342/06A RU2575956C2 (ru) 2010-07-08 2011-07-07 Компрессор и соответствующая газовая турбина

Country Status (6)

Country Link
US (1) US20130216359A1 (fr)
EP (2) EP2405104A1 (fr)
JP (1) JP5638696B2 (fr)
CN (1) CN102985640B (fr)
RU (1) RU2575956C2 (fr)
WO (1) WO2012004336A2 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9951639B2 (en) * 2012-02-10 2018-04-24 Pratt & Whitney Canada Corp. Vane assemblies for gas turbine engines
US9341194B2 (en) 2012-11-01 2016-05-17 Solar Turbines Incorporated Gas turbine engine compressor with a biased inner ring
DE102016207212A1 (de) 2016-04-28 2017-11-02 MTU Aero Engines AG Leitschaufelkranz für eine Strömungsmaschine
JP7349274B2 (ja) * 2019-06-27 2023-09-22 三菱重工業株式会社 静翼支持リング及びタービン
CN112065777B (zh) * 2020-11-10 2021-01-19 中国航发上海商用航空发动机制造有限责任公司 压气机进口导流叶片的调节精度保持结构
JP7439315B1 (ja) 2023-03-16 2024-02-27 株式会社神鋼環境ソリューション 筒状構造体

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2671634A (en) * 1949-07-01 1954-03-09 Rolls Royce Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors
DE10225679A1 (de) * 2002-06-10 2003-12-18 Rolls Royce Deutschland Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine
RU2224895C2 (ru) * 1999-05-31 2004-02-27 Нуово Пиньоне Холдинг С.П.А. Средство для установки сопел ступени статора и для охлаждения дисков ротора в газовой турбине
EP1586744A2 (fr) * 2004-04-14 2005-10-19 General Electric Company Aubes de guidage variables pour turbine à gaz

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4792277A (en) * 1987-07-08 1988-12-20 United Technologies Corporation Split shroud compressor
FR2685033B1 (fr) * 1991-12-11 1994-02-11 Snecma Stator dirigeant l'entree de l'air a l'interieur d'une turbomachine et procede de montage d'une aube de ce stator.
US5395124A (en) * 1993-01-04 1995-03-07 Imo Industries, Inc. Retractible segmented packing ring for fluid turbines having gravity springs to neutralize packing segment weight forces
FR2723614B1 (fr) * 1994-08-10 1996-09-13 Snecma Dispositif d'assemblage d'un etage circulaire d'aubes pivotantes.
FR2775731B1 (fr) * 1998-03-05 2000-04-07 Snecma Etage circulaire d'aubes aux extremites interieures unies par un anneau de liaison
EP1205639A1 (fr) * 2000-11-09 2002-05-15 General Electric Company Système de fixation des aubes statoriques variables dans une virole interieure de turbines
US6682299B2 (en) * 2001-11-15 2004-01-27 General Electric Company Variable stator vane support arrangement
US6651986B2 (en) * 2002-01-29 2003-11-25 General Electric Company Retractable packing ring lower half segment retaining key and method for retaining retractable packing ring lower half segment
US7651319B2 (en) * 2002-02-22 2010-01-26 Drs Power Technology Inc. Compressor stator vane
US7101150B2 (en) * 2004-05-11 2006-09-05 Power Systems Mfg, Llc Fastened vane assembly
DE102005040574A1 (de) * 2005-08-26 2007-03-15 Rolls-Royce Deutschland Ltd & Co Kg Spaltkontrollvorrichtung für eine Gasturbine
FR2896012B1 (fr) * 2006-01-06 2008-04-04 Snecma Sa Dispositif anti-usure pour pivot de guidage d'aube a angle de calage variable de compresseur de turbomachine
FR2902843A1 (fr) * 2006-06-23 2007-12-28 Snecma Sa Secteur de redresseur de compresseur ou secteur de distributeur de turbomachine
US7572098B1 (en) * 2006-10-10 2009-08-11 Johnson Gabriel L Vane ring with a damper
US7824152B2 (en) * 2007-05-09 2010-11-02 Siemens Energy, Inc. Multivane segment mounting arrangement for a gas turbine
US8632300B2 (en) * 2010-07-22 2014-01-21 Siemens Energy, Inc. Energy absorbing apparatus in a gas turbine engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2671634A (en) * 1949-07-01 1954-03-09 Rolls Royce Adjustable stator blade and shroud ring arrangement for axial flow turbines and compressors
RU2224895C2 (ru) * 1999-05-31 2004-02-27 Нуово Пиньоне Холдинг С.П.А. Средство для установки сопел ступени статора и для охлаждения дисков ротора в газовой турбине
DE10225679A1 (de) * 2002-06-10 2003-12-18 Rolls Royce Deutschland Lagerring zur Lagerung von Schaufelfüßen von verstellbaren Statorschaufeln im Hochdruckverdichter einer Gasturbine
EP1586744A2 (fr) * 2004-04-14 2005-10-19 General Electric Company Aubes de guidage variables pour turbine à gaz

Also Published As

Publication number Publication date
EP2405104A1 (fr) 2012-01-11
WO2012004336A2 (fr) 2012-01-12
JP2013529755A (ja) 2013-07-22
EP2591213A2 (fr) 2013-05-15
US20130216359A1 (en) 2013-08-22
CN102985640B (zh) 2015-10-21
EP2591213B1 (fr) 2014-04-02
RU2013105342A (ru) 2014-08-20
JP5638696B2 (ja) 2014-12-10
WO2012004336A3 (fr) 2012-06-07
CN102985640A (zh) 2013-03-20

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20170708