JP6105208B2 - 可変ステータベーン段から空気を抽気するための装置を備えた軸流圧縮機 - Google Patents
可変ステータベーン段から空気を抽気するための装置を備えた軸流圧縮機 Download PDFInfo
- Publication number
- JP6105208B2 JP6105208B2 JP2012098293A JP2012098293A JP6105208B2 JP 6105208 B2 JP6105208 B2 JP 6105208B2 JP 2012098293 A JP2012098293 A JP 2012098293A JP 2012098293 A JP2012098293 A JP 2012098293A JP 6105208 B2 JP6105208 B2 JP 6105208B2
- Authority
- JP
- Japan
- Prior art keywords
- casing
- compressor
- rows
- stator
- liner assembly
- 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
Links
- 238000000605 extraction Methods 0.000 claims description 20
- 230000000149 penetrating effect Effects 0.000 claims 1
- 230000000694 effects Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Images
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)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/094,934 US8734091B2 (en) | 2011-04-27 | 2011-04-27 | Axial compressor with arrangement for bleeding air from variable stator vane stages |
| US13/094,934 | 2011-04-27 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2012233476A JP2012233476A (ja) | 2012-11-29 |
| JP2012233476A5 JP2012233476A5 (OSRAM) | 2015-05-21 |
| JP6105208B2 true JP6105208B2 (ja) | 2017-03-29 |
Family
ID=46084830
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2012098293A Expired - Fee Related JP6105208B2 (ja) | 2011-04-27 | 2012-04-24 | 可変ステータベーン段から空気を抽気するための装置を備えた軸流圧縮機 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US8734091B2 (OSRAM) |
| EP (1) | EP2518273A3 (OSRAM) |
| JP (1) | JP6105208B2 (OSRAM) |
| CA (1) | CA2775423A1 (OSRAM) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014197042A2 (en) * | 2013-03-13 | 2014-12-11 | 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 |
| EP3084142B1 (en) * | 2013-12-16 | 2019-01-02 | 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 |
| EP2993313B1 (en) * | 2014-09-05 | 2019-10-30 | United Technologies Corporation | Offtakes for gas turbine engine secondary gas flows |
| AU2015390072B2 (en) | 2015-03-31 | 2018-05-10 | Halliburton Energy Services, Inc. | Actuator controlled variable flow area stator for flow splitting in down-hole tools |
| 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)
| 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 |
-
2011
- 2011-04-27 US US13/094,934 patent/US8734091B2/en active Active
-
2012
- 2012-04-19 CA CA2775423A patent/CA2775423A1/en not_active Abandoned
- 2012-04-24 JP JP2012098293A patent/JP6105208B2/ja not_active Expired - Fee Related
- 2012-04-26 EP EP12165786.0A patent/EP2518273A3/en not_active Withdrawn
Also Published As
| Publication number | Publication date |
|---|---|
| US8734091B2 (en) | 2014-05-27 |
| US20120275912A1 (en) | 2012-11-01 |
| EP2518273A3 (en) | 2017-04-19 |
| EP2518273A2 (en) | 2012-10-31 |
| JP2012233476A (ja) | 2012-11-29 |
| CA2775423A1 (en) | 2012-10-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6105208B2 (ja) | 可変ステータベーン段から空気を抽気するための装置を備えた軸流圧縮機 | |
| US11981419B2 (en) | Method and system for integrated pitch control mechanism actuator hydraulic fluid transfer | |
| JP6043370B2 (ja) | ガスタービンエンジンサンプ加圧システム | |
| US7077623B2 (en) | Fluid flow machine with integrated fluid circulation system | |
| CN118434961A (zh) | 配备有可变桨距轮叶和环形界面护罩的涡轮机模块 | |
| US10704563B2 (en) | Axi-centrifugal compressor with variable outlet guide vanes | |
| US8955304B2 (en) | Gas turbine engine with modular cores and propulsion unit | |
| US8789354B2 (en) | Gas turbine engine with separate core and propulsion unit | |
| US20180328187A1 (en) | Turbine engine with an airfoil and insert | |
| JP2017096269A (ja) | ガスタービンエンジンファン | |
| JP2017072136A (ja) | 可変ピッチ出口ガイドベーンを有するエンジン | |
| JP2017110640A (ja) | ベンチュリ効果を有する端壁処置部 | |
| JP2017078410A (ja) | 変調式タービン冷却のための方法およびシステム | |
| JP2016109124A (ja) | 漏洩流を制御するための軸流圧縮機端壁処理部 | |
| US10760426B2 (en) | Turbine engine with variable effective throat | |
| CN106468216A (zh) | 混合流涡轮核心 | |
| US11933193B2 (en) | Turbine engine with an airfoil having a set of dimples | |
| US10030587B2 (en) | Annular airflow actuation system for variable cycle gas turbine engines | |
| JP2017096268A (ja) | 可変ピッチファンアクチュエータ | |
| US9822792B2 (en) | Assembly for a fluid flow machine | |
| US20250264057A1 (en) | Cooling air delivery system and methods thereof | |
| CN1755080B (zh) | 用于涡轮机的鼻锥 | |
| CN112443364B (zh) | 用于同心可变定子静叶的促动组件 | |
| WO2015006009A1 (en) | Angled core engine | |
| US12123308B2 (en) | Clearance control system for a gas turbine engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20150406 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20150406 |
|
| A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20160128 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20160202 |
|
| A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20160425 |
|
| A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20160630 |
|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20160801 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20170207 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20170302 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 6105208 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| LAPS | Cancellation because of no payment of annual fees |