CA2775423A1 - Axial compressor with arrangement for bleeding air from variable stator vane stages - Google Patents

Axial compressor with arrangement for bleeding air from variable stator vane stages Download PDF

Info

Publication number
CA2775423A1
CA2775423A1 CA2775423A CA2775423A CA2775423A1 CA 2775423 A1 CA2775423 A1 CA 2775423A1 CA 2775423 A CA2775423 A CA 2775423A CA 2775423 A CA2775423 A CA 2775423A CA 2775423 A1 CA2775423 A1 CA 2775423A1
Authority
CA
Canada
Prior art keywords
casing
axially
compressor
rows
stator
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.)
Abandoned
Application number
CA2775423A
Other languages
English (en)
French (fr)
Inventor
Thomas Ory Moniz
Thomas Viars
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 CA2775423A1 publication Critical patent/CA2775423A1/en
Abandoned legal-status Critical Current

Links

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F01D17/105—Final actuators by passing part of the fluid
    • 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
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0246—Surge control by varying geometry within the pumps, e.g. by adjusting vanes
    • 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
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/545—Ducts
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/023—Details or means for fluid extraction

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)
  • Geometry (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA2775423A 2011-04-27 2012-04-19 Axial compressor with arrangement for bleeding air from variable stator vane stages Abandoned CA2775423A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/094,934 2011-04-27
US13/094,934 US8734091B2 (en) 2011-04-27 2011-04-27 Axial compressor with arrangement for bleeding air from variable stator vane stages

Publications (1)

Publication Number Publication Date
CA2775423A1 true CA2775423A1 (en) 2012-10-27

Family

ID=46084830

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2775423A Abandoned CA2775423A1 (en) 2011-04-27 2012-04-19 Axial compressor with arrangement for bleeding air from variable stator vane stages

Country Status (4)

Country Link
US (1) US8734091B2 (https=)
EP (1) EP2518273A3 (https=)
JP (1) JP6105208B2 (https=)
CA (1) CA2775423A1 (https=)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9988915B2 (en) * 2013-03-13 2018-06-05 United Technologies Corporation Stator segment
JP6185781B2 (ja) * 2013-07-23 2017-08-23 三菱日立パワーシステムズ株式会社 軸流圧縮機
US9657647B2 (en) 2013-10-15 2017-05-23 The Boeing Company Methods and apparatus to adjust bleed ports on an aircraft engine
EP2881548B1 (de) * 2013-12-09 2018-08-15 MTU Aero Engines GmbH Gasturbinenverdichter
WO2015094509A1 (en) * 2013-12-16 2015-06-25 United Technologies Corporation Shortened support for compressor variable vane
EP2960437B1 (de) * 2014-06-26 2018-08-08 MTU Aero Engines GmbH Leitschaufelvorrichtung für eine gasturbine sowie gasturbine mit einer solchen leitschaufelvorrichtung
US10612416B2 (en) 2014-09-05 2020-04-07 United Technologies Corporation Offtakes for gas turbine engine secondary gas flows
RU2686769C1 (ru) 2015-03-31 2019-04-30 Хэллибертон Энерджи Сервисиз, Инк. Регулирующий проходное сечение статор, управляемый приводом, для разделения потока в забойных инструментах
US10215047B2 (en) 2015-12-28 2019-02-26 General Electric Company Actuation system utilizing MEMS technology
US10302019B2 (en) 2016-03-03 2019-05-28 General Electric Company High pressure compressor augmented bleed with autonomously actuated valve
US10731663B2 (en) * 2016-06-21 2020-08-04 Rolls-Royce North American Technologies Inc. Axial compressor with radially outer annulus
CN106194846A (zh) * 2016-07-12 2016-12-07 中国航空工业集团公司沈阳发动机设计研究所 一种双层机匣结构压气机及具有其的航空发动机
US11073160B2 (en) 2016-09-08 2021-07-27 The United States Of America As Represented By The Secretary Of The Army Adaptable articulating axial-flow compressor/turbine rotor blade
US10539153B2 (en) 2017-03-14 2020-01-21 General Electric Company Clipped heat shield assembly
US20180313364A1 (en) * 2017-04-27 2018-11-01 General Electric Company Compressor apparatus with bleed slot including turning vanes
US10934943B2 (en) 2017-04-27 2021-03-02 General Electric Company Compressor apparatus with bleed slot and supplemental flange
US10626879B2 (en) * 2017-11-13 2020-04-21 United Technologies Corporation Gas turbine engine with mid-compressor bleed
US10794272B2 (en) * 2018-02-19 2020-10-06 General Electric Company Axial and centrifugal compressor
DE102018113997A1 (de) * 2018-06-12 2019-12-12 Rolls-Royce Deutschland Ltd & Co Kg Gehäuseanordnung für einen Axialverdichter eines Gasturbinentriebwerks
JP7720681B2 (ja) * 2019-08-29 2025-08-08 三菱重工業株式会社 圧縮機、ガスタービン
US11866182B2 (en) 2020-05-01 2024-01-09 General Electric Company Fuel delivery system having a fuel oxygen reduction unit
US11512611B2 (en) * 2021-02-09 2022-11-29 General Electric Company Stator apparatus for a gas turbine engine
US11781504B2 (en) * 2021-10-19 2023-10-10 Honeywell International Inc. Bleed plenum for compressor section
CN115234518B (zh) * 2022-08-05 2025-05-30 中国航发贵阳发动机设计研究所 一种带集气腔结构的复合功能压气机机匣
US12110810B2 (en) * 2022-11-16 2024-10-08 General Electric Company Gas turbine engine bleed air flow control
US12196141B2 (en) 2023-04-19 2025-01-14 Honeywell International Inc. Systems and methods with distributed bleed for gas turbine engine compressor stabilization
US12247580B2 (en) * 2023-05-03 2025-03-11 General Electric Company Forward load reduction structures for aft-most stages of high pressure compressors

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3996964A (en) * 1972-09-15 1976-12-14 The Bendix Corporation Control apparatus particularly for a plurality of compressor bleed valves of a gas turbine engine
US3945759A (en) 1974-10-29 1976-03-23 General Electric Company Bleed air manifold
DE2740904A1 (de) * 1977-09-10 1979-03-22 Motoren Turbinen Union Vorrichtung zur betaetigung von absperrorganen in gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken
US4791783A (en) * 1981-11-27 1988-12-20 General Electric Company Convertible aircraft engine
FR2601074B1 (fr) * 1986-07-03 1990-05-25 Snecma Turbomachine munie d'un dispositif de commande du debit d'air de ventilation preleve en vue du controle des jeux entre rotor et stator.
DE3940248A1 (de) * 1989-04-17 1990-10-18 Gen Electric Verfahren und einrichtung zum regeln eines gasturbinentriebwerkes
US5155993A (en) 1990-04-09 1992-10-20 General Electric Company Apparatus for compressor air extraction
US5209633A (en) 1990-11-19 1993-05-11 General Electric Company High pressure compressor flowpath bleed valve extraction slot
US6109868A (en) 1998-12-07 2000-08-29 General Electric Company Reduced-length high flow interstage air extraction
US6325595B1 (en) 2000-03-24 2001-12-04 General Electric Company High recovery multi-use bleed
US6413043B1 (en) * 2000-11-09 2002-07-02 General Electric Company Inlet guide vane and shroud support contact
US6438941B1 (en) * 2001-04-26 2002-08-27 General Electric Company Bifurcated splitter for variable bleed flow
US6550254B2 (en) 2001-08-17 2003-04-22 General Electric Company Gas turbine engine bleed scoops
US6783324B2 (en) * 2002-08-15 2004-08-31 General Electric Company Compressor bleed case
FR2858027B1 (fr) * 2003-07-21 2005-09-23 Snecma Moteurs Compresseur haute pression a cycle hybride et turbomachine comprenant un tel compresseur
US7624581B2 (en) 2005-12-21 2009-12-01 General Electric Company Compact booster bleed turbofan
FR2916815B1 (fr) * 2007-05-30 2017-02-24 Snecma Compresseur a reinjection d'air
US8388308B2 (en) * 2007-10-30 2013-03-05 General Electric Company Asymmetric flow extraction system
EP2058524A1 (en) * 2007-11-12 2009-05-13 Siemens Aktiengesellschaft Air bleed compressor with variable guide vanes

Also Published As

Publication number Publication date
JP2012233476A (ja) 2012-11-29
JP6105208B2 (ja) 2017-03-29
EP2518273A3 (en) 2017-04-19
US8734091B2 (en) 2014-05-27
US20120275912A1 (en) 2012-11-01
EP2518273A2 (en) 2012-10-31

Similar Documents

Publication Publication Date Title
US8734091B2 (en) Axial compressor with arrangement for bleeding air from variable stator vane stages
US11448235B2 (en) Axi-centrifugal compressor with variable outlet guide vanes
CN107013335B (zh) 燃气涡轮发动机及用于其的冷却回路
CN1987066B (zh) 紧凑型增压排气涡轮风扇发动机
US20180328187A1 (en) Turbine engine with an airfoil and insert
US10030587B2 (en) Annular airflow actuation system for variable cycle gas turbine engines
US7631484B2 (en) High pressure ratio aft fan
US20180363676A1 (en) Inlet pre-swirl gas turbine engine
JP6043370B2 (ja) ガスタービンエンジンサンプ加圧システム
US10794272B2 (en) Axial and centrifugal compressor
CN106948968A (zh) 可变桨距风扇促动器
CN107023391A (zh) 用于压缩机扩散槽口的系统及方法
US10060286B2 (en) Geared annular airflow actuation system for variable cycle gas turbine engines
US20250264057A1 (en) Cooling air delivery system and methods thereof
US10393024B2 (en) Multi-air stream cooling system
CN112443364B (zh) 用于同心可变定子静叶的促动组件
CN108019238A (zh) 具有冷却回路的翼型件组件
US11401835B2 (en) Turbine center frame
CN115585056A (zh) 具有罩门的非管道式风扇涡轮发动机
US12092027B1 (en) Manifold assembly and anti-ice system for gas turbine engine
CN120426132A (zh) 用于具有多级排气提取的燃气涡轮发动机的压缩机组件
US12398671B2 (en) Compressor assembly for a gas turbine engine having multi-stage bleed extraction

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20170216

FZDE Discontinued

Effective date: 20190423