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
Application number
MX2013013944A
Other languages
English (en)
Spanish (es)
Other versions
MX2013013944A (es
Inventor
Douglas Carl Hofer
Dhananjayarao Gottapu
Original Assignee
Gen Electric
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of MX2013013944A publication Critical patent/MX2013013944A/es
Publication of MX338204B publication Critical patent/MX338204B/es

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)
MX2013013944A 2011-05-27 2012-05-25 Rotor de compresor supersonico y metodo para comprimir un fluido. MX338204B (es)

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 (enExample)
EP (1) EP2715143B1 (enExample)
JP (1) JP6078053B2 (enExample)
KR (1) KR20140024911A (enExample)
CN (1) CN103597213B (enExample)
AU (1) AU2012262564A1 (enExample)
BR (1) BR112013029742A2 (enExample)
CA (1) CA2836303A1 (enExample)
MX (1) MX338204B (enExample)
WO (1) WO2012166564A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013009642A2 (en) * 2011-07-09 2013-01-17 Ramgen Power Systems, Llc Stator for supersonic compressor
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
WO2024035894A1 (en) 2022-08-11 2024-02-15 Next Gen Compression Llc Method for efficient part load compressor operation
US12066027B2 (en) 2022-08-11 2024-08-20 Next Gen Compression Llc Variable geometry supersonic compressor

Family Cites Families (33)

* Cited by examiner, † Cited by third party
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
HUP9904124A3 (en) 1996-12-16 2001-04-28 Ramgen Power Systems Inc Belle Ramjet engine for power generation
JP2003517525A (ja) 1998-02-26 2003-05-27 アリソン・アドバンスト・ディベロップメント・カンパニー 圧縮機端壁ブリードシステム
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
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
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
WO2009025803A1 (en) 2007-08-20 2009-02-26 Kevin Kremeyer Energy-deposition systems, equipment and methods for modifying and controlling shock waves and supersonic flow
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
ATE530771T1 (de) 2008-01-18 2011-11-15 Ramgen Power Systems Llc Verfahren und vorrichtung zum starten von überschallverdichtern
EP2310109A4 (en) 2008-07-14 2012-03-28 Tenoroc Llc AERODYNAMIC TRUNK 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

Also Published As

Publication number Publication date
CN103597213A (zh) 2014-02-19
EP2715143B1 (en) 2021-03-10
BR112013029742A2 (pt) 2018-04-24
EP2715143A1 (en) 2014-04-09
US20120301271A1 (en) 2012-11-29
WO2012166564A1 (en) 2012-12-06
AU2012262564A1 (en) 2013-12-12
KR20140024911A (ko) 2014-03-03
MX2013013944A (es) 2014-01-23
US8770929B2 (en) 2014-07-08
JP6078053B2 (ja) 2017-02-08
CN103597213B (zh) 2016-02-17
JP2014515455A (ja) 2014-06-30
CA2836303A1 (en) 2012-12-06

Similar Documents

Publication Publication Date Title
MX338204B (es) Rotor de compresor supersonico y metodo para comprimir un fluido.
EP2423511A3 (en) A supersonic compressor rotor and method of assembling same
EP2762682A3 (en) Axial turbine with meridionally divided turbine housing
MX2013009899A (es) Mezcladora dinamica.
WO2014114653A3 (en) Gas turbine outer case active ambient cooling including air exhaust into sub-ambient cavity
EP2584142A3 (en) Gas turbine engine cooling systems having hub-bleed impellers and methods for the production thereof
GB201102987D0 (en) A propfan engine
WO2013165510A3 (en) Multi-lobed cooling hole and method of manufacture
EP4364787A3 (en) Blood pump
WO2013165517A3 (en) Gas turbine engine component with diffusive cooling hole
EP2518272A3 (en) High area ratio turbine vane
WO2013090144A3 (en) Gas turbine engine exhaust diffuser including circumferential vane
WO2014113808A3 (en) Duct fitiing with reduced flow pressure loss
EP3018349A3 (en) Rotary screw compressor
EP3150917A3 (en) Combustion system and method having annular flow path architecture
MX2014001013A (es) Propulsor centrifugo y turbomaquina.
WO2009144415A3 (fr) Collecteur d'air dans une turbomachine
MX2018004804A (es) Triturador de medios de chorro.
EP2385219A3 (en) Diffuser for gas turbine system between compressor exit and combustor inlet
EP2530331A3 (en) Axial fan assembly for a vehicle cooling system
WO2014123654A8 (en) Suction-based active clearance control system
EP2466146A3 (en) Supersonic compressor and method of assembling same
GB2547846A (en) Compressor and turbocharger
MX2019000433A (es) Metodo para mejorar el rendimiento del compresor de turbina.
WO2010097384A3 (de) Multi-inlet-vakuumpumpe

Legal Events

Date Code Title Description
FG Grant or registration