JPH08232603A5 - - Google Patents

Info

Publication number
JPH08232603A5
JPH08232603A5 JP1995341388A JP34138895A JPH08232603A5 JP H08232603 A5 JPH08232603 A5 JP H08232603A5 JP 1995341388 A JP1995341388 A JP 1995341388A JP 34138895 A JP34138895 A JP 34138895A JP H08232603 A5 JPH08232603 A5 JP H08232603A5
Authority
JP
Japan
Prior art keywords
supersonic
hub
distributor according
supersonic distributor
blade elements
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.)
Granted
Application number
JP1995341388A
Other languages
English (en)
Japanese (ja)
Other versions
JP3779360B2 (ja
JPH08232603A (ja
Filing date
Publication date
Priority claimed from FR9415693A external-priority patent/FR2728618B1/fr
Application filed filed Critical
Publication of JPH08232603A publication Critical patent/JPH08232603A/ja
Publication of JPH08232603A5 publication Critical patent/JPH08232603A5/ja
Application granted granted Critical
Publication of JP3779360B2 publication Critical patent/JP3779360B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

JP34138895A 1994-12-27 1995-12-27 ターボ機械の入口段用の超音速分配器 Expired - Lifetime JP3779360B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9415693A FR2728618B1 (fr) 1994-12-27 1994-12-27 Distributeur supersonique d'etage d'entree de turbomachine
FR9415693 1994-12-27

Publications (3)

Publication Number Publication Date
JPH08232603A JPH08232603A (ja) 1996-09-10
JPH08232603A5 true JPH08232603A5 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) 2004-11-18
JP3779360B2 JP3779360B2 (ja) 2006-05-24

Family

ID=9470273

Family Applications (1)

Application Number Title Priority Date Filing Date
JP34138895A Expired - Lifetime JP3779360B2 (ja) 1994-12-27 1995-12-27 ターボ機械の入口段用の超音速分配器

Country Status (6)

Country Link
US (1) US5676522A (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
EP (1) EP0719906B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
JP (1) JP3779360B2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
CA (1) CA2165863A1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
DE (1) DE69509056T2 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
FR (1) FR2728618B1 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6508631B1 (en) 1999-11-18 2003-01-21 Mks Instruments, Inc. Radial flow turbomolecular vacuum pump
US6358012B1 (en) 2000-05-01 2002-03-19 United Technologies Corporation High efficiency turbomachinery blade
WO2002004788A1 (en) * 2000-07-06 2002-01-17 Drysdale Kenneth William Patte Turbine, power generation system therefor and method of power generation
RU2202696C2 (ru) * 2001-02-22 2003-04-20 Масютин Владимир Ильич Газотурбинный двигатель
US7334990B2 (en) * 2002-01-29 2008-02-26 Ramgen Power Systems, Inc. Supersonic compressor
US20030210980A1 (en) * 2002-01-29 2003-11-13 Ramgen Power Systems, Inc. Supersonic compressor
US7293955B2 (en) * 2002-09-26 2007-11-13 Ramgen Power Systrms, Inc. Supersonic gas compressor
US7434400B2 (en) * 2002-09-26 2008-10-14 Lawlor Shawn P Gas turbine power plant with supersonic shock compression ramps
GB0323909D0 (en) * 2003-10-11 2003-11-12 Rolls Royce Plc Turbine blades
FR2868467B1 (fr) * 2004-04-05 2006-06-02 Snecma Moteurs Sa Carter de turbine a crochets refractaires obtenu par procede mdp
DE102009013399A1 (de) * 2009-03-16 2010-09-23 Mtu Aero Engines Gmbh Tandemschaufelkonstruktion
WO2011116231A2 (en) * 2010-03-19 2011-09-22 Sp Tech Propeller blade
US8683791B2 (en) 2010-08-20 2014-04-01 Toyota Motor Engineering & Manufacturing North America, Inc. Method and system for homogenizing exhaust from an engine
JP6030853B2 (ja) * 2011-06-29 2016-11-24 三菱日立パワーシステムズ株式会社 タービン動翼及び軸流タービン
CN104937236B (zh) * 2013-02-21 2018-10-30 三菱重工业株式会社 涡轮机动叶片
CN104420888B (zh) * 2013-08-19 2016-04-20 中国科学院工程热物理研究所 渐缩流道跨音速涡轮叶片及应用其的涡轮
CN105822432A (zh) * 2016-04-22 2016-08-03 山东元动力科技有限公司 一种微型涡喷发动机
US10677077B2 (en) 2017-03-01 2020-06-09 Panasonic Corporation Turbine nozzle and radial turbine including the same
CN107023395B (zh) * 2017-06-07 2019-02-26 中国空气动力研究与发展中心计算空气动力研究所 一种可调喉道面积的超声速飞行器进气道及调节方法
US10710705B2 (en) 2017-06-28 2020-07-14 General Electric Company Open rotor and airfoil therefor
CN107489462A (zh) * 2017-09-18 2017-12-19 中国船舶重工集团公司第七0四研究所 涡轮机用沿流线周向扩张的扇形截面超音速喷嘴
WO2019167319A1 (ja) 2018-02-27 2019-09-06 株式会社Ihi ロケットエンジン用ターボポンプ
EP3569817B1 (en) * 2018-05-14 2020-10-14 ArianeGroup GmbH Guide vane arrangement for use in a turbine
CN111425259A (zh) * 2020-02-27 2020-07-17 合肥通用机械研究院有限公司 一种磁悬浮超音速透平膨胀机
US11840939B1 (en) * 2022-06-08 2023-12-12 General Electric Company Gas turbine engine with an airfoil
WO2024096946A2 (en) 2022-08-11 2024-05-10 Next Gen Compression Llc Variable geometry supersonic compressor

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL4075C (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) * 1913-10-31
US1801427A (en) * 1927-03-12 1931-04-21 Holzwarth Gas Turbine Co Gas-turbine blade
US3156407A (en) * 1958-07-07 1964-11-10 Commissariat Energie Atomique Supersonic compressors
CH427851A (de) * 1965-04-01 1967-01-15 Bbc Brown Boveri & Cie Laufschaufelkranz für transsonische Strömung
US3333817A (en) * 1965-04-01 1967-08-01 Bbc Brown Boveri & Cie Blading structure for axial flow turbo-machines
US3565548A (en) * 1969-01-24 1971-02-23 Gen Electric Transonic buckets for axial flow turbines
US4408957A (en) * 1972-02-22 1983-10-11 General Motors Corporation Supersonic blading
GB1420318A (en) * 1972-11-04 1976-01-07 Rolls Royce Method and apparatus for manufaccturing an article from a particulate material
US4639189A (en) * 1984-02-27 1987-01-27 Rockwell International Corporation Hollow, thermally-conditioned, turbine stator nozzle
US4968216A (en) * 1984-10-12 1990-11-06 The Boeing Company Two-stage fluid driven turbine
US5277549A (en) * 1992-03-16 1994-01-11 Westinghouse Electric Corp. Controlled reaction L-2R steam turbine blade

Similar Documents

Publication Publication Date Title
JPH08232603A5 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html)
US3861826A (en) Cascade diffuser having thin, straight vanes
JP3779360B2 (ja) ターボ機械の入口段用の超音速分配器
EP1507977B1 (en) Discrete passage diffuser
US8100643B2 (en) Centrifugal compressor vane diffuser wall contouring
EP0439267B1 (en) Compressor impeller with displaced splitter blades
US4349314A (en) Compressor diffuser and method
JPH06280503A (ja) 半径流タービンノズル羽根
US8721273B2 (en) Ring diffuser for an axial turbomachine
US8038392B2 (en) Axial diffuser for a centrifugal compressor
JPS5990797A (ja) 遠心圧縮機及び圧縮方法
JPS5936119B2 (ja) 遠心コンプレツサ用デイフユ−ザ
EP2434094A2 (en) Steam turbine stator vane and steam turbine
US11859543B2 (en) Diffuser pipe with exit flare
JP2012031864A (ja) 低圧蒸気タービン及び低圧蒸気タービンを運転する方法
US7273352B2 (en) Inlet partial blades for structural integrity and performance
US3968935A (en) Contoured supersonic nozzle
US10823195B2 (en) Diffuser pipe with non-axisymmetric end wall
US6017187A (en) Device for reducing noise in centrifugal pumps
US20160369654A1 (en) Axial Turbine
US4966523A (en) Two-row pipe diffusers with boundary layer control
US5447413A (en) Stator endwall for an elastic-fluid turbine
JP2009036112A (ja) 回転機械の翼
USRE30720E (en) Contoured supersonic nozzle
JPH07332007A (ja) タービン静翼