MX338204B - Rotor de compresor supersonico y metodo para comprimir un fluido. - Google Patents
Rotor de compresor supersonico y metodo para comprimir un fluido.Info
- Publication number
- MX338204B MX338204B MX2013013944A MX2013013944A MX338204B MX 338204 B MX338204 B MX 338204B MX 2013013944 A MX2013013944 A MX 2013013944A MX 2013013944 A MX2013013944 A MX 2013013944A MX 338204 B MX338204 B MX 338204B
- Authority
- MX
- Mexico
- Prior art keywords
- compressor rotor
- flow channel
- supersonic compressor
- supersonic
- compressing
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage 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
- F04D19/00—Axial-flow pumps
- F04D19/02—Multi-stage pumps
- F04D19/024—Multi-stage pumps with contrarotating parts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D21/00—Pump involving supersonic speed of pumped fluids
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Abstract
Un rotor de compresor supersónico. El rotor del compresor supersónico incluye un cuerpo (56) de disco esencialmente cilíndrico que incluye una superficie (68) corriente arriba, una superficie (70) corriente abajo y una superficie (66) radialmente externa que se extiende generalmente en forma axial entre la superficie (68) corriente arriba y la superficie corriente abajo. El cuerpo de disco define un eje (62) de línea central. Una pluralidad de aletas (54) está acoplada con la superficie radialmente externa. Las aletas adyacentes forman un par y están orientadas de tal forma que se define un canal (88) de flujo entre cada par de aletas adyacentes. El canal de flujo se extiende generalmente en forma axial entre la abertura (90) de entrada y la abertura (92) de salida. Por lo menos una rampa (112) de compresión supersónica está colocada dentro del canal de flujo. La rampa de compresión supersónica se puede colocar, en forma selectiva, en una primera posición (156), en una segunda posición (158) y en cualquier posición entre ellas.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/117,878 US8770929B2 (en) | 2011-05-27 | 2011-05-27 | Supersonic compressor rotor and method of compressing a fluid |
PCT/US2012/039492 WO2012166564A1 (en) | 2011-05-27 | 2012-05-25 | Supersonic compressor rotor and method of compressing a fluid |
Publications (2)
Publication Number | Publication Date |
---|---|
MX2013013944A MX2013013944A (es) | 2014-01-23 |
MX338204B true MX338204B (es) | 2016-04-07 |
Family
ID=46178863
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2013013944A MX338204B (es) | 2011-05-27 | 2012-05-25 | Rotor de compresor supersonico y metodo para comprimir un fluido. |
Country Status (10)
Country | Link |
---|---|
US (1) | US8770929B2 (es) |
EP (1) | EP2715143B1 (es) |
JP (1) | JP6078053B2 (es) |
KR (1) | KR20140024911A (es) |
CN (1) | CN103597213B (es) |
AU (1) | AU2012262564A1 (es) |
BR (1) | BR112013029742A2 (es) |
CA (1) | CA2836303A1 (es) |
MX (1) | MX338204B (es) |
WO (1) | WO2012166564A1 (es) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN202991533U (zh) * | 2011-07-09 | 2013-06-12 | 拉姆金动力系统有限责任公司 | 超音速压缩机 |
US9909597B2 (en) | 2013-10-15 | 2018-03-06 | Dresser-Rand Company | Supersonic compressor with separator |
US20160281727A1 (en) * | 2015-03-27 | 2016-09-29 | Dresser-Rand Company | Apparatus, system, and method for compressing a process fluid |
CN110360130B (zh) * | 2018-04-09 | 2022-12-27 | 开利公司 | 可变扩压器驱动系统 |
WO2024096946A2 (en) | 2022-08-11 | 2024-05-10 | Next Gen Compression Llc | Variable geometry supersonic compressor |
Family Cites Families (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2853227A (en) * | 1948-05-29 | 1958-09-23 | Melville W Beardsley | Supersonic compressor |
US2925952A (en) | 1953-07-01 | 1960-02-23 | Maschf Augsburg Nuernberg Ag | Radial-flow-compressor |
GB885661A (en) | 1959-06-19 | 1961-12-28 | Power Jets Res & Dev Ltd | Intakes for supersonic flow |
US2971330A (en) * | 1959-07-20 | 1961-02-14 | United Aircraft Corp | Air-inlet shock controller |
US4199296A (en) | 1974-09-03 | 1980-04-22 | Chair Rory S De | Gas turbine engines |
US4012166A (en) | 1974-12-04 | 1977-03-15 | Deere & Company | Supersonic shock wave compressor diffuser with circular arc channels |
US4463772A (en) | 1981-09-29 | 1984-08-07 | The Boeing Company | Flush inlet for supersonic aircraft |
US4704861A (en) | 1984-05-15 | 1987-11-10 | A/S Kongsberg Vapenfabrikk | Apparatus for mounting, and for maintaining running clearance in, a double entry radial compressor |
US4620679A (en) | 1984-08-02 | 1986-11-04 | United Technologies Corporation | Variable-geometry inlet |
JP2873581B2 (ja) * | 1988-12-05 | 1999-03-24 | 一男 黒岩 | 遠心圧縮機 |
US5424824A (en) * | 1993-05-12 | 1995-06-13 | The Boeing Company | Method and apparatus for normal shock sensing within the focal region of a laser beam |
US5525038A (en) | 1994-11-04 | 1996-06-11 | United Technologies Corporation | Rotor airfoils to control tip leakage flows |
CN1187232A (zh) * | 1995-06-07 | 1998-07-08 | 肖恩·P·劳勒 | 用于产生动力的改进方法和装置 |
US5881758A (en) | 1996-03-28 | 1999-03-16 | The Boeing Company | Internal compression supersonic engine inlet |
GEP20002218B (en) | 1996-12-16 | 2000-08-25 | Ramgen Power Systems Inc | Device and Method for Power Generation |
WO1999051866A2 (en) | 1998-02-26 | 1999-10-14 | Allison Advanced Development Company | Compressor endwall bleed system |
DE19812624A1 (de) | 1998-03-23 | 1999-09-30 | Bmw Rolls Royce Gmbh | Rotor-Schaufelblatt einer Axialströmungsmaschine |
US6338609B1 (en) | 2000-02-18 | 2002-01-15 | General Electric Company | Convex compressor casing |
US6488469B1 (en) | 2000-10-06 | 2002-12-03 | Pratt & Whitney Canada Corp. | Mixed flow and centrifugal compressor for gas turbine engine |
US7334990B2 (en) | 2002-01-29 | 2008-02-26 | Ramgen Power Systems, Inc. | Supersonic compressor |
CA2382382A1 (fr) | 2002-04-16 | 2003-10-16 | Universite De Sherbrooke | Moteur rotatif continu a combustion induite par onde de choc |
US7434400B2 (en) | 2002-09-26 | 2008-10-14 | Lawlor Shawn P | Gas turbine power plant with supersonic shock compression ramps |
US7293955B2 (en) | 2002-09-26 | 2007-11-13 | Ramgen Power Systrms, Inc. | Supersonic gas compressor |
US6948306B1 (en) | 2002-12-24 | 2005-09-27 | The United States Of America As Represented By The Secretary Of The Navy | Apparatus and method of using supersonic combustion heater for hypersonic materials and propulsion testing |
US7070388B2 (en) | 2004-02-26 | 2006-07-04 | United Technologies Corporation | Inducer with shrouded rotor for high speed applications |
US7866937B2 (en) * | 2007-03-30 | 2011-01-11 | Innovative Energy, Inc. | Method of pumping gaseous matter via a supersonic centrifugal pump |
US8960596B2 (en) | 2007-08-20 | 2015-02-24 | Kevin Kremeyer | Energy-deposition systems, equipment and method for modifying and controlling shock waves and supersonic flow |
US8393158B2 (en) | 2007-10-24 | 2013-03-12 | Gulfstream Aerospace Corporation | Low shock strength inlet |
WO2009092046A1 (en) | 2008-01-18 | 2009-07-23 | Ramgen Power Systems, Llc | Method and apparatus for starting supersonic compressors |
US8016901B2 (en) | 2008-07-14 | 2011-09-13 | Tenoroc Llc | Aerodynamic separation nozzle |
US8137054B2 (en) | 2008-12-23 | 2012-03-20 | General Electric Company | Supersonic compressor |
US9097258B2 (en) * | 2009-06-25 | 2015-08-04 | General Electric Company | Supersonic compressor comprising radial flow path |
US9103345B2 (en) * | 2009-12-16 | 2015-08-11 | General Electric Company | Supersonic compressor rotor |
-
2011
- 2011-05-27 US US13/117,878 patent/US8770929B2/en active Active
-
2012
- 2012-05-25 CA CA2836303A patent/CA2836303A1/en not_active Abandoned
- 2012-05-25 KR KR1020137031233A patent/KR20140024911A/ko not_active Application Discontinuation
- 2012-05-25 MX MX2013013944A patent/MX338204B/es active IP Right Grant
- 2012-05-25 BR BR112013029742A patent/BR112013029742A2/pt not_active IP Right Cessation
- 2012-05-25 EP EP12724522.3A patent/EP2715143B1/en active Active
- 2012-05-25 WO PCT/US2012/039492 patent/WO2012166564A1/en active Application Filing
- 2012-05-25 CN CN201280025973.XA patent/CN103597213B/zh active Active
- 2012-05-25 JP JP2014512129A patent/JP6078053B2/ja active Active
- 2012-05-25 AU AU2012262564A patent/AU2012262564A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP2715143B1 (en) | 2021-03-10 |
KR20140024911A (ko) | 2014-03-03 |
US20120301271A1 (en) | 2012-11-29 |
AU2012262564A1 (en) | 2013-12-12 |
CN103597213A (zh) | 2014-02-19 |
WO2012166564A1 (en) | 2012-12-06 |
CN103597213B (zh) | 2016-02-17 |
CA2836303A1 (en) | 2012-12-06 |
BR112013029742A2 (pt) | 2018-04-24 |
EP2715143A1 (en) | 2014-04-09 |
JP6078053B2 (ja) | 2017-02-08 |
US8770929B2 (en) | 2014-07-08 |
JP2014515455A (ja) | 2014-06-30 |
MX2013013944A (es) | 2014-01-23 |
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Legal Events
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FG | Grant or registration |