JP2008025578A - 遠心圧縮機のインペラの下流側空洞の換気システム - Google Patents
遠心圧縮機のインペラの下流側空洞の換気システム Download PDFInfo
- Publication number
- JP2008025578A JP2008025578A JP2007186669A JP2007186669A JP2008025578A JP 2008025578 A JP2008025578 A JP 2008025578A JP 2007186669 A JP2007186669 A JP 2007186669A JP 2007186669 A JP2007186669 A JP 2007186669A JP 2008025578 A JP2008025578 A JP 2008025578A
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- annular
- impeller
- downstream
- air
- metal plate
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- 238000009423 ventilation Methods 0.000 claims abstract description 36
- 239000002184 metal Substances 0.000 claims description 83
- 238000011144 upstream manufacturing Methods 0.000 claims description 33
- 238000002347 injection Methods 0.000 claims description 32
- 239000007924 injection Substances 0.000 claims description 32
- 238000000605 extraction Methods 0.000 claims description 4
- 239000000284 extract Substances 0.000 claims 1
- 238000000034 method Methods 0.000 abstract 1
- 238000002485 combustion reaction Methods 0.000 description 14
- 238000013459 approach Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000000630 rising effect Effects 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000013022 venting Methods 0.000 description 1
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Classifications
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- 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
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
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- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
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- 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
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/584—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps cooling or heating the machine
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
【解決手段】ターボ機械の遠心圧縮機のインペラの下流側空洞の換気システムであって、このシステムは、圧縮機10の出口から取り出される換気空気を分岐させて、換気空気をインペラの下流側面34に沿って径方向内側から外側に流れさせるようにさせるために、インペラ36の下流側空洞38に固定して取り付けられる、流れの分岐手段70、84を含む。
【選択図】図2
Description
12 ディフューザ
20 圧縮機の出口
22 ディフューザの入口
28 環状末端片
30、124、46 フランジ
32 噴射回路
34 下流側面
36 インペラ
38 下流側空洞
48 環状管路
70 第1の環状金属板
74 環状通路
84、120 第2の環状金属板
86、122 環状通路
92 第1の環状要素
92’ 第2の環状要素
104 穴
126 空気の通過穴
134、142 径方向の環状スペース
150 噴射手段
Claims (11)
- ターボ機械の遠心圧縮機のインペラの下流側空洞の換気システムであって、下流側空洞が、インペラの下流側面と遠心圧縮機の出口に配置された環状ディフューザの下流側末端片とにより画定され、かつ遠心圧縮機の出口から空気を取り出して換気され、前記換気システムが、インペラの下流側空洞に固定して取り付けられた分岐手段を備え、該分岐手段は、圧縮機の出口から取り出された空気を、インペラの下流側空洞内の入口へディフューザの環状末端片に沿って分岐させるとともに、下流側空洞の下流側部分からの換気空気を分岐させて、換気空気をインペラの下流側面に沿って径方向内側から外側に流れさせる、システム。
- 分岐手段が、インペラの下流側空洞内で、ディフューザの環状末端片の下流側端の固定手段に固定して取り付けられた環状金属板を含んでおり、該環状金属板が、前記固定手段からインペラの下流側面に沿って上流側に延びて、圧縮機の出口から空気を取り出す空気取り出し手段の近傍で終端する、請求項1に記載のシステム。
- 分岐手段が、ディフューザの環状末端片の下流側端の固定手段に固定して取り付けられた第2の環状金属板を含み、該第2の環状金属板が、前記固定手段からディフューザの環状末端片にほぼ平行に上流側に延びて、圧縮機の出口から空気を取り出す空気取り出し手段の近傍で終端する、請求項1または2に記載のシステム。
- 第2の環状金属板の上流側端が、第1の環状金属板の上流側端の径方向外側に配置される、請求項2および3に記載のシステム。
- インペラの下流側面が、2個の環状金属板の上流側端の間で下流側空洞内に突出部として延びる、流れを分岐させる環状要素を支持する、請求項4に記載のシステム。
- 第1の環状金属板が、インペラの下流側面と共に換気空気の環状通路を形成し、該換気空気の環状通路が、第2の環状金属板とディフューザの末端片との間に形成される換気空気の環状通路と下流側端で連通する、請求項3から5のいずれか一項に記載のシステム。
- 第2の環状金属板が、下流側空洞の内部にあり、第2の環状金属板がディフューザの環状末端片と共に形成する環状通路が、圧縮機の出口から取り出される空気を供給される、請求項6に記載のシステム。
- 第2の環状金属板が、下流側空洞の外側にあり、第2の環状金属板がディフューザの環状末端片と共に形成する環状通路が、ディフューザから出る空気を供給される、請求項6に記載のシステム。
- 環状金属板が、換気空気の噴射回路から取り出される空気を下流側端で供給される環状通路を、インペラの下流側面と共に画定する、請求項2に記載のシステム。
- インペラの下流側面に換気空気の噴射手段を含み、該噴射手段を出る空気の流れが、インペラの回転方向に向けられ、噴射手段が、第2の環状金属板および/またはディフューザの環状末端片により支持される、請求項3から9のいずれか一項に記載のシステム。
- 請求項1から10のいずれか一項に記載の換気システムを含む、ターボ機械。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0606541A FR2904036B1 (fr) | 2006-07-19 | 2006-07-19 | Systeme de ventilation d'une cavite aval de rouet de compresseur centrifuge |
FR0606541 | 2006-07-19 |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2008025578A true JP2008025578A (ja) | 2008-02-07 |
JP2008025578A5 JP2008025578A5 (ja) | 2010-08-12 |
JP4956809B2 JP4956809B2 (ja) | 2012-06-20 |
Family
ID=37770941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007186669A Active JP4956809B2 (ja) | 2006-07-19 | 2007-07-18 | 遠心圧縮機のインペラの下流側空洞の換気システム |
Country Status (6)
Country | Link |
---|---|
US (1) | US7942630B2 (ja) |
EP (1) | EP1882826B1 (ja) |
JP (1) | JP4956809B2 (ja) |
CA (1) | CA2594008C (ja) |
FR (1) | FR2904036B1 (ja) |
RU (1) | RU2433310C2 (ja) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8075247B2 (en) * | 2007-12-21 | 2011-12-13 | Pratt & Whitney Canada Corp. | Centrifugal impeller with internal heating |
US8087249B2 (en) * | 2008-12-23 | 2012-01-03 | General Electric Company | Turbine cooling air from a centrifugal compressor |
US8147178B2 (en) * | 2008-12-23 | 2012-04-03 | General Electric Company | Centrifugal compressor forward thrust and turbine cooling apparatus |
US9228497B2 (en) | 2010-12-30 | 2016-01-05 | Rolls-Royce Corporation | Gas turbine engine with secondary air flow circuit |
GB2510004B (en) * | 2013-08-19 | 2015-10-14 | Rolls Royce Plc | Axial flow machine cooling system |
FR3025260B1 (fr) * | 2014-08-29 | 2019-08-30 | Safran Aircraft Engines | Compresseur centrifuge a resistance amelioree |
US10208668B2 (en) * | 2015-09-30 | 2019-02-19 | Rolls-Royce Corporation | Turbine engine advanced cooling system |
US10830144B2 (en) | 2016-09-08 | 2020-11-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine compressor impeller cooling air sinks |
JP6750998B2 (ja) * | 2016-10-07 | 2020-09-02 | パナソニックi−PROセンシングソリューションズ株式会社 | 監視システム及び監視方法 |
FR3062682B1 (fr) * | 2017-02-07 | 2019-04-19 | Safran Aircraft Engines | Partie de turbomachine comprenant une paroi de separation de deux cavites pourvue de bossages |
CN107725479B (zh) * | 2017-09-26 | 2019-09-24 | 中国科学院工程热物理研究所 | 一种旋转盘腔内部的转子罩壳结构及包含该结构的发动机 |
US11525393B2 (en) | 2020-03-19 | 2022-12-13 | Rolls-Royce Corporation | Turbine engine with centrifugal compressor having impeller backplate offtake |
FR3137409A1 (fr) * | 2022-07-04 | 2024-01-05 | Safran Helicopter Engines | Compresseur pour aéronef |
US11773773B1 (en) | 2022-07-26 | 2023-10-03 | Rolls-Royce North American Technologies Inc. | Gas turbine engine centrifugal compressor with impeller load and cooling control |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4462204A (en) * | 1982-07-23 | 1984-07-31 | General Electric Company | Gas turbine engine cooling airflow modulator |
JPS62143098A (ja) * | 1985-12-18 | 1987-06-26 | 松下電器産業株式会社 | 明瞭度評価用単音節の合成方法 |
JPH08159085A (ja) * | 1994-05-31 | 1996-06-18 | Ingersoll Dresser Pump Co | 遠心ポンプ |
US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
JPH1089291A (ja) * | 1996-09-11 | 1998-04-07 | Tochigi Fuji Ind Co Ltd | 遠心式コンプレッサ |
US5996331A (en) * | 1997-09-15 | 1999-12-07 | Alliedsignal Inc. | Passive turbine coolant regulator responsive to engine load |
JP2000054996A (ja) * | 1998-05-25 | 2000-02-22 | Asea Brown Boveri Ag | ラジアル圧縮機とその運転法 |
US6035627A (en) * | 1998-04-21 | 2000-03-14 | Pratt & Whitney Canada Inc. | Turbine engine with cooled P3 air to impeller rear cavity |
JP2001123997A (ja) * | 1999-10-21 | 2001-05-08 | Hitachi Ltd | 磁気軸受搭載遠心圧縮機 |
US6276896B1 (en) * | 2000-07-25 | 2001-08-21 | Joseph C. Burge | Apparatus and method for cooling Axi-Centrifugal impeller |
JP2004301098A (ja) * | 2003-03-31 | 2004-10-28 | Yamada Seisakusho Co Ltd | ウォーターポンプ |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE968742C (de) * | 1944-09-22 | 1958-03-27 | Daimler Benz Ag | Mehrstufiges Radialgeblaese, vorzugsweise Ladegeblaese fuer Flugmotoren |
GB1047014A (en) * | 1962-07-03 | 1966-11-02 | English Electric Co Ltd | Improvements in or relating to hydraulic pumps, turbines or reversible pump turbines |
DE4225625A1 (de) * | 1992-08-03 | 1994-02-10 | Asea Brown Boveri | Abgasturbolader |
JP4375883B2 (ja) * | 2000-06-02 | 2009-12-02 | 本田技研工業株式会社 | ガスタービンエンジンの軸受へのシールエア供給装置 |
DE10325980A1 (de) * | 2003-06-07 | 2004-12-23 | Daimlerchrysler Ag | Abgasturbolader |
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2006
- 2006-07-19 FR FR0606541A patent/FR2904036B1/fr active Active
-
2007
- 2007-06-29 EP EP07290824A patent/EP1882826B1/fr active Active
- 2007-07-16 CA CA2594008A patent/CA2594008C/fr active Active
- 2007-07-17 US US11/779,016 patent/US7942630B2/en active Active
- 2007-07-18 JP JP2007186669A patent/JP4956809B2/ja active Active
- 2007-07-18 RU RU2007127561/06A patent/RU2433310C2/ru active
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4462204A (en) * | 1982-07-23 | 1984-07-31 | General Electric Company | Gas turbine engine cooling airflow modulator |
JPS62143098A (ja) * | 1985-12-18 | 1987-06-26 | 松下電器産業株式会社 | 明瞭度評価用単音節の合成方法 |
JPH08159085A (ja) * | 1994-05-31 | 1996-06-18 | Ingersoll Dresser Pump Co | 遠心ポンプ |
US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
JPH1089291A (ja) * | 1996-09-11 | 1998-04-07 | Tochigi Fuji Ind Co Ltd | 遠心式コンプレッサ |
US5996331A (en) * | 1997-09-15 | 1999-12-07 | Alliedsignal Inc. | Passive turbine coolant regulator responsive to engine load |
US6035627A (en) * | 1998-04-21 | 2000-03-14 | Pratt & Whitney Canada Inc. | Turbine engine with cooled P3 air to impeller rear cavity |
JP2000054996A (ja) * | 1998-05-25 | 2000-02-22 | Asea Brown Boveri Ag | ラジアル圧縮機とその運転法 |
JP2001123997A (ja) * | 1999-10-21 | 2001-05-08 | Hitachi Ltd | 磁気軸受搭載遠心圧縮機 |
US6276896B1 (en) * | 2000-07-25 | 2001-08-21 | Joseph C. Burge | Apparatus and method for cooling Axi-Centrifugal impeller |
JP2004301098A (ja) * | 2003-03-31 | 2004-10-28 | Yamada Seisakusho Co Ltd | ウォーターポンプ |
Also Published As
Publication number | Publication date |
---|---|
US7942630B2 (en) | 2011-05-17 |
RU2433310C2 (ru) | 2011-11-10 |
EP1882826A1 (fr) | 2008-01-30 |
EP1882826B1 (fr) | 2012-08-01 |
CA2594008C (fr) | 2014-11-04 |
FR2904036A1 (fr) | 2008-01-25 |
RU2007127561A (ru) | 2009-01-27 |
FR2904036B1 (fr) | 2008-08-29 |
JP4956809B2 (ja) | 2012-06-20 |
CA2594008A1 (fr) | 2008-01-19 |
US20100028137A1 (en) | 2010-02-04 |
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R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |