DE602007001921D1 - Strömungsmaschine mit einem Kühlsystem für die Rückseite eines Zentrifugalverdichterrads - Google Patents
Strömungsmaschine mit einem Kühlsystem für die Rückseite eines ZentrifugalverdichterradsInfo
- Publication number
- DE602007001921D1 DE602007001921D1 DE602007001921T DE602007001921T DE602007001921D1 DE 602007001921 D1 DE602007001921 D1 DE 602007001921D1 DE 602007001921 T DE602007001921 T DE 602007001921T DE 602007001921 T DE602007001921 T DE 602007001921T DE 602007001921 D1 DE602007001921 D1 DE 602007001921D1
- Authority
- DE
- Germany
- Prior art keywords
- turbomachine
- cooling system
- centrifugal compressor
- compressor wheel
- wheel
- 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.)
- Active
Links
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
- 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
- F01D5/046—Heating, heat insulation or cooling means
-
- 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
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- 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
-
- 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
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/205—Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes
-
- 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)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0606544A FR2904038A1 (fr) | 2006-07-19 | 2006-07-19 | Systeme de refroidissement de la face aval d'un rouet de compresseur centrifuge |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602007001921D1 true DE602007001921D1 (de) | 2009-09-24 |
Family
ID=37771107
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602007001921T Active DE602007001921D1 (de) | 2006-07-19 | 2007-06-20 | Strömungsmaschine mit einem Kühlsystem für die Rückseite eines Zentrifugalverdichterrads |
Country Status (8)
Country | Link |
---|---|
US (1) | US7841187B2 (de) |
EP (1) | EP1882815B1 (de) |
JP (1) | JP4998920B2 (de) |
CA (1) | CA2594005C (de) |
DE (1) | DE602007001921D1 (de) |
FR (1) | FR2904038A1 (de) |
RU (1) | RU2437000C2 (de) |
UA (1) | UA93364C2 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2927951B1 (fr) * | 2008-02-27 | 2011-08-19 | Snecma | Ensemble diffuseur-redresseur pour une turbomachine |
CN101965443B (zh) * | 2008-02-27 | 2014-04-23 | 三菱重工业株式会社 | 燃气轮机及燃气轮机的机室开放方法 |
US8087249B2 (en) * | 2008-12-23 | 2012-01-03 | General Electric Company | Turbine cooling air from a centrifugal compressor |
FR2946687B1 (fr) * | 2009-06-10 | 2011-07-01 | Snecma | Turbomachine comprenant des moyens ameliores de reglage du debit d'un flux d'air de refroidissement preleve en sortie de compresseur haute pression |
FR2950656B1 (fr) * | 2009-09-25 | 2011-09-23 | Snecma | Ventilation d'une roue de turbine dans une turbomachine |
US9228497B2 (en) * | 2010-12-30 | 2016-01-05 | Rolls-Royce Corporation | Gas turbine engine with secondary air flow circuit |
EP2961931B1 (de) | 2013-03-01 | 2019-10-30 | Rolls-Royce North American Technologies, Inc. | Wärmeregulierung eines hochdruckverdichters sowie verfahren zum zusammenbau und zur kühlung |
EP2961991B1 (de) * | 2013-03-01 | 2020-07-22 | Rolls-Royce North American Technologies, Inc. | Gasturbinenmotorlaufradsystem für einen zwischendruckverdichter |
EP2964960B1 (de) | 2013-03-08 | 2019-06-12 | Rolls-Royce North American Technologies, Inc. | Turbostrahltriebwerk-radialverdichter mit dichtung zwischen zwei diffusorteilen |
GB2510004B (en) | 2013-08-19 | 2015-10-14 | Rolls Royce Plc | Axial flow machine cooling system |
US9945248B2 (en) * | 2014-04-01 | 2018-04-17 | United Technologies Corporation | Vented tangential on-board injector for a gas turbine engine |
KR101765583B1 (ko) * | 2014-07-29 | 2017-08-07 | 현대자동차 주식회사 | 공기 압축기의 냉각유닛 |
GB201420966D0 (en) * | 2014-11-26 | 2015-01-07 | Rolls Royce Plc | Compressor cooling |
US10208668B2 (en) * | 2015-09-30 | 2019-02-19 | Rolls-Royce Corporation | Turbine engine advanced cooling system |
US10415599B2 (en) * | 2015-10-30 | 2019-09-17 | Ford Global Technologies, Llc | Axial thrust loading mitigation in a turbocharger |
US10830144B2 (en) | 2016-09-08 | 2020-11-10 | Rolls-Royce North American Technologies Inc. | Gas turbine engine compressor impeller cooling air sinks |
CN111295521B (zh) | 2017-11-01 | 2021-11-16 | 株式会社Ihi | 离心压缩机 |
DE112018005198T5 (de) | 2017-11-01 | 2020-06-10 | Ihi Corporation | Zentrifugalverdichter |
DE112018005188T5 (de) | 2017-11-01 | 2020-06-25 | Ihi Corporation | Zentrifugalverdichter |
CN110318874B (zh) * | 2019-06-24 | 2020-09-25 | 中国科学院工程热物理研究所 | 一种燃气轮机中离心压气机背腔的控涡流路系统 |
US11668324B2 (en) * | 2019-08-02 | 2023-06-06 | Hamilton Sundstrand Corporation | Motor and bearing cooling paths and a transfer tube for another cooling channel |
US11525393B2 (en) | 2020-03-19 | 2022-12-13 | Rolls-Royce Corporation | Turbine engine with centrifugal compressor having impeller backplate offtake |
CN113357189B (zh) * | 2021-06-23 | 2022-11-18 | 中国航发湖南动力机械研究所 | 径向外流叶轮背腔引气结构和燃气涡轮发动机 |
CN113847147B (zh) * | 2021-09-24 | 2023-01-17 | 中国航发沈阳发动机研究所 | 一种航空发动机内部冷却空气的引气除尘结构 |
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 |
Family Cites Families (14)
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 |
DE3514352A1 (de) * | 1985-04-20 | 1986-10-23 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Gasturbinentriebwerk mit einrichtungen zur abzweigung von verdichterluft zur kuehlung von heissteilen |
DE3627306A1 (de) * | 1986-02-28 | 1987-09-03 | Mtu Muenchen Gmbh | Einrichtung zur belueftung von rotorbauteilen fuer verdichter von gasturbinentriebwerken |
DE3820062A1 (de) * | 1988-06-13 | 1989-12-21 | Klein Schanzlin & Becker Ag | Stroemungsmaschine |
CA2015777C (en) * | 1990-04-30 | 1993-10-12 | Lynn P. Tessier | Centrifugal pump |
US5555721A (en) * | 1994-09-28 | 1996-09-17 | General Electric Company | Gas turbine engine cooling supply circuit |
US5862666A (en) * | 1996-12-23 | 1999-01-26 | Pratt & Whitney Canada Inc. | Turbine engine having improved thrust bearing load control |
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 |
EP0961033B1 (de) * | 1998-05-25 | 2003-10-08 | ABB Turbo Systems AG | Radialverdichter |
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 |
US6276896B1 (en) * | 2000-07-25 | 2001-08-21 | Joseph C. Burge | Apparatus and method for cooling Axi-Centrifugal impeller |
JP4091874B2 (ja) * | 2003-05-21 | 2008-05-28 | 本田技研工業株式会社 | ガスタービンエンジンの二次エア供給装置 |
US7252474B2 (en) * | 2003-09-12 | 2007-08-07 | Mes International, Inc. | Sealing arrangement in a compressor |
-
2006
- 2006-07-19 FR FR0606544A patent/FR2904038A1/fr not_active Withdrawn
-
2007
- 2007-06-20 EP EP07290765A patent/EP1882815B1/de active Active
- 2007-06-20 DE DE602007001921T patent/DE602007001921D1/de active Active
- 2007-07-16 CA CA2594005A patent/CA2594005C/fr active Active
- 2007-07-18 JP JP2007186668A patent/JP4998920B2/ja active Active
- 2007-07-18 RU RU2007127559/06A patent/RU2437000C2/ru active
- 2007-07-18 UA UAA200708218A patent/UA93364C2/uk unknown
- 2007-07-19 US US11/780,252 patent/US7841187B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP1882815A1 (de) | 2008-01-30 |
RU2007127559A (ru) | 2009-01-27 |
FR2904038A1 (fr) | 2008-01-25 |
US7841187B2 (en) | 2010-11-30 |
UA93364C2 (uk) | 2011-02-10 |
US20080141679A1 (en) | 2008-06-19 |
EP1882815B1 (de) | 2009-08-12 |
JP4998920B2 (ja) | 2012-08-15 |
RU2437000C2 (ru) | 2011-12-20 |
JP2008025577A (ja) | 2008-02-07 |
CA2594005C (fr) | 2014-04-08 |
CA2594005A1 (fr) | 2008-01-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |