JP4012507B2 - 複流圧縮機 - Google Patents
複流圧縮機 Download PDFInfo
- Publication number
- JP4012507B2 JP4012507B2 JP2003523796A JP2003523796A JP4012507B2 JP 4012507 B2 JP4012507 B2 JP 4012507B2 JP 2003523796 A JP2003523796 A JP 2003523796A JP 2003523796 A JP2003523796 A JP 2003523796A JP 4012507 B2 JP4012507 B2 JP 4012507B2
- Authority
- JP
- Japan
- Prior art keywords
- rotor
- turbine engine
- gas turbine
- shroud
- annular
- 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
- 238000001816 cooling Methods 0.000 claims description 37
- 238000011144 upstream manufacturing Methods 0.000 claims description 11
- 239000012530 fluid Substances 0.000 claims description 5
- 230000007423 decrease Effects 0.000 claims description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000010248 power generation Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000001629 suppression Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 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
- 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
-
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/04—Blade-carrying members, e.g. rotors for radial-flow machines or engines
- F01D5/043—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
- F01D5/045—Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type the wheel comprising two adjacent bladed wheel portions, e.g. with interengaging blades for damping vibrations
-
- 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
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
-
- 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
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/50—Application for auxiliary power units (APU's)
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Claims (14)
- ハブ(17)と、該ハブ(17)から半径方向に延びたロータブレード(16;116)と、を備え、かつ、中心軸回りに回転するように構成された、ロータ(12;112)と、
上記中心軸と同軸上に位置し、かつ、外部壁(26;126)を定義する、環状圧縮機ケーシングと、
上記圧縮機ケーシング内にあり、かつ、上記中心軸と同軸上に位置するとともに、上記ロータ(12;112)から下流に向かって延びた、環状シュラウド(33;133)と、
上記環状シュラウド(33;133)内に区画された、第1の環状ダクト(36;136)と、
上記ロータの下流に、半径方向流出インペラ(27)と、
を備え、かつ、
上記ロータブレード(16;116)は、少なくとも部分的に上記外部壁(26;126)に極めて近接するチップ(25;125)と、該チップ(25;125)の近くに位置する端部と、を備え、
上記外部壁(26;126)は、上記ロータ(12;112)の上流に向かって延び、外部空気供給源と該ロータ(12;112)との間において、実質的に妨げられないように流体の連通を可能とし、
上記環状シュラウド(33;133)と上記外部壁(26;126)とは、第2の環状ダクト(34;134)を区画し、
上記第1のダクト(36;136)は、上記ロータ(12;112)と圧縮機出口との間において、コア流体の連通を可能とし、
上記第2のダクト(34;134)は、補助の用途のために、少なくとも上記ブレード(16;116)の上記端部から、空気を供給するように構成されており、
ステータ(11)が、上記インペラ(27)と上記ロータ(12;112)との間に配置されている、
ことを特徴とするガスタービンエンジン圧縮機(10;110)。 - 上記ロータブレード(16)の各々が、前縁と後縁とを備えるとともに、上記端部内に切り欠き部(24)を含み、かつ、上記環状シュラウド(33)が、該ロータブレード(16)の該切り欠き部(24)内の上流に向かって延びる、ことを特徴とする請求項1に記載のガスタービンエンジン圧縮機。
- 上記ロータブレード(16)の各々が、上記シュラウド上流に位置する上記チップに向かって延びた、残りの端部を備えることを特徴とする請求項2に記載のガスタービンエンジン圧縮機。
- 上記切り欠き部(24)を区画する上記端部の、軸方向のエッジ(24a)が、上記環状シュラウド(33)に極めて近接した位置を通過することを特徴とする請求項3に記載のガスタービンエンジン圧縮機。
- 上記ロータブレード(116)は、上記中心軸と同軸上に位置し、かつ、上記環状シュラウド(133)に整列した、翼幅分割シュラウド(30)を構成するように、各ブレードの両側から延在する、少なくとも1つのフランジを備えることを特徴とする請求項1に記載のガスタービンエンジン圧縮機。
- 上記翼幅分割シュラウド(30)が、シュラウドなしのブレードより薄型のブレードエーロフォイルの形状を可能とすることを特徴とする請求項5に記載のガスタービンエンジン圧縮機。
- 上記翼幅分割シュラウド(30)が、上記ロータブレード(116)の前縁から下流に向かって延びて、代替される前に上記ロータから下流に向かって延びていた上記環状シュラウドの上流端部であった上記環状シュラウド(133)の一部を代替することを特徴とする請求項5または6に記載のガスタービンエンジン圧縮機。
- 上記ガスタービンエンジン(10;110)が、補助動力装置であることを特徴とする請求項1〜7のいずれかに記載のガスタービンエンジン圧縮機。
- 補助の用途には、上記補助動力装置のパッシブオイル冷却システム用の冷却空気を供給すること、が含まれることを特徴とする請求項8に記載のガスタービンエンジン圧縮機。
- 補助の用途には、室内加圧用の冷却空気を供給すること、が含まれることを特徴とする請求項8に記載のガスタービンエンジン圧縮機。
- 上記第1のダクト(36;136)の断面積が、流れ方向に減少することを特徴とする請求項1〜10のいずれかに記載のガスタービンエンジン圧縮機。
- 上記圧縮機が、複数のロータと複数のステータとを備えることを特徴とする、請求項1〜11のいずれかに記載のガスタービンエンジン圧縮機。
- 上記インペラ(27;127)が、上記中心軸と同軸上に位置し、かつ、第1の環状ダクト(36;136)と第2の環状ダクト(34;134)とに分割する上記環状シュラウド(33;133)に整列する、翼幅分割シュラウドを、構成するように、各ブレードの両側から延びた少なくとも1つのフランジをそれぞれ含んだ、複数のブレード(29)を備えることを特徴とする、請求項1〜12のいずれかに記載のガスタービンエンジン圧縮機。
- 上記インペラ(29;129)は、上記第1の環状ダクト(36;136)から空気の供給を受けることを特徴とする請求項1〜13のいずれかに記載のガスタービンエンジン圧縮機。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/942,546 US6578351B1 (en) | 2001-08-29 | 2001-08-29 | APU core compressor providing cooler air supply |
PCT/CA2002/001303 WO2003018960A1 (en) | 2001-08-29 | 2002-08-26 | Double flow compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2005500459A JP2005500459A (ja) | 2005-01-06 |
JP4012507B2 true JP4012507B2 (ja) | 2007-11-21 |
Family
ID=25478247
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2003523796A Expired - Fee Related JP4012507B2 (ja) | 2001-08-29 | 2002-08-26 | 複流圧縮機 |
Country Status (6)
Country | Link |
---|---|
US (1) | US6578351B1 (ja) |
EP (1) | EP1421257B1 (ja) |
JP (1) | JP4012507B2 (ja) |
CA (2) | CA2729130C (ja) |
DE (1) | DE60221403T2 (ja) |
WO (1) | WO2003018960A1 (ja) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0206880D0 (en) * | 2002-03-23 | 2002-05-01 | Rolls Royce Plc | A vane for a rotor arrangement for a gas turbine engine |
US7055306B2 (en) * | 2003-04-30 | 2006-06-06 | Hamilton Sundstrand Corporation | Combined stage single shaft turbofan engine |
US7231767B2 (en) * | 2004-04-16 | 2007-06-19 | Pratt & Whitney Canada Corp. | Forced air cooling system |
DE102005019938A1 (de) * | 2005-04-29 | 2006-11-09 | Daimlerchrysler Ag | Abgasturbolader für eine Brennkraftmaschine |
US7698896B2 (en) * | 2005-07-27 | 2010-04-20 | Honeywell International Inc. | Compact, light weight eductor oil cooler plenum and surge flow plenum design |
US8221083B2 (en) * | 2008-04-15 | 2012-07-17 | United Technologies Corporation | Asymmetrical rotor blade fir-tree attachment |
FR2944060B1 (fr) * | 2009-04-06 | 2013-07-19 | Turbomeca | Systeme d'air secondaire pour compresseur centrifuge ou mixte |
FR2945330B1 (fr) * | 2009-05-11 | 2011-07-15 | Snecma | Pompe centrifuge a double echappement. |
US9091172B2 (en) | 2010-12-28 | 2015-07-28 | Rolls-Royce Corporation | Rotor with cooling passage |
CN102322430A (zh) * | 2011-10-24 | 2012-01-18 | 永济新时速电机电器有限责任公司 | 双风道内风扇 |
US8864067B2 (en) | 2012-05-31 | 2014-10-21 | Hamilton Sundstrand Corporation | Auxiliary fire resistant mount system for an auxiliary power unit |
US20140338360A1 (en) * | 2012-09-21 | 2014-11-20 | United Technologies Corporation | Bleed port ribs for turbomachine case |
US9677472B2 (en) | 2012-10-08 | 2017-06-13 | United Technologies Corporation | Bleed air slot |
US9915199B2 (en) | 2012-10-08 | 2018-03-13 | United Technologies Corporation | Bi-directional compression fan rotor for a gas turbine engine |
US9938855B2 (en) | 2014-01-31 | 2018-04-10 | Pratt & Whitney Canada Corp. | Cooling system and method for supplying a cooling gas flow |
EP3037674A1 (en) * | 2014-12-22 | 2016-06-29 | Alstom Technology Ltd | Engine and method for operating said engine |
US11174786B2 (en) | 2016-11-15 | 2021-11-16 | General Electric Company | Monolithic superstructure for load path optimization |
US10544986B2 (en) | 2017-03-29 | 2020-01-28 | Air Products And Chemicals, Inc. | Parallel compression in LNG plants using a double flow compressor |
WO2018222192A1 (en) * | 2017-06-01 | 2018-12-06 | Florida Turbine Technologies, Inc. | High pressure ratio twin spool industrial gas turbine engine with dual flow high spool compressor |
US11155357B2 (en) | 2019-01-03 | 2021-10-26 | Ge Aviation Systems Llc | Generator with jet pump having motive fluid for fluidly coupling to a cooling circuit |
US11300051B2 (en) | 2019-02-01 | 2022-04-12 | Honeywell International Inc. | Engine systems with load compressor that provides cooling air |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
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DE722424C (de) | 1940-04-16 | 1942-07-09 | Friedrich Schicht | Gleichdruck-Geblaese oder Gleichdruck-Pumpe |
FR1006128A (fr) | 1947-11-19 | 1952-04-21 | Dispositif d'alimentation et de combustion pour turbines à gaz et turbo-réacteurs | |
FR1059635A (fr) | 1952-07-10 | 1954-03-26 | Perfectionnements aux turbines à gaz | |
US2696074A (en) | 1953-01-02 | 1954-12-07 | Gen Motors Corp | Combined torque converter and engine air-cooling system |
FR2063491A6 (ja) | 1969-10-17 | 1971-07-09 | Cit Alcatel | |
GB1342590A (en) | 1970-07-17 | 1974-01-03 | Secr Defence | Suppression of noise in gas turbine engines |
DE2344023C2 (de) | 1973-08-31 | 1983-12-08 | Wallace Murray Corp., 10171 New York, N.Y. | Ladeluftkühlung einer abgasturbogeladenen Brennkraftmaschine |
US4052845A (en) | 1974-06-20 | 1977-10-11 | United Technologies Corporation | Variable ratio bypass gas turbine engine with flow diverter valve |
US3979903A (en) | 1974-08-01 | 1976-09-14 | General Electric Company | Gas turbine engine with booster stage |
FR2309712A1 (fr) | 1975-04-28 | 1976-11-26 | Garrett Corp | Turbomachine a courants fluidiques multiples |
US4372113A (en) | 1981-01-15 | 1983-02-08 | Ramer James L | Pipeline energy recapture device |
DE3512714A1 (de) | 1985-04-09 | 1986-10-09 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Gasturbinentriebwerk |
US5105616A (en) * | 1989-12-07 | 1992-04-21 | Sundstrand Corporation | Gas turbine with split flow radial compressor |
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FR2738283B1 (fr) * | 1995-08-30 | 1997-09-26 | Snecma | Agencement de turbomachine comprenant une grille d'aubes et un carter intermediaire |
US5673559A (en) | 1995-11-24 | 1997-10-07 | Benson; Steven R. | Turbine housing system |
-
2001
- 2001-08-29 US US09/942,546 patent/US6578351B1/en not_active Expired - Lifetime
-
2002
- 2002-08-26 WO PCT/CA2002/001303 patent/WO2003018960A1/en active IP Right Grant
- 2002-08-26 CA CA2729130A patent/CA2729130C/en not_active Expired - Lifetime
- 2002-08-26 JP JP2003523796A patent/JP4012507B2/ja not_active Expired - Fee Related
- 2002-08-26 EP EP02757999A patent/EP1421257B1/en not_active Expired - Fee Related
- 2002-08-26 CA CA2458550A patent/CA2458550C/en not_active Expired - Lifetime
- 2002-08-26 DE DE60221403T patent/DE60221403T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP2005500459A (ja) | 2005-01-06 |
CA2729130C (en) | 2013-11-12 |
DE60221403D1 (de) | 2007-09-06 |
CA2729130A1 (en) | 2003-03-06 |
DE60221403T2 (de) | 2008-04-03 |
CA2458550A1 (en) | 2003-03-06 |
EP1421257A1 (en) | 2004-05-26 |
CA2458550C (en) | 2011-04-05 |
WO2003018960A1 (en) | 2003-03-06 |
EP1421257B1 (en) | 2007-07-25 |
US6578351B1 (en) | 2003-06-17 |
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