MX338178B - Rotor de compresor supersonica. - Google Patents

Rotor de compresor supersonica.

Info

Publication number
MX338178B
MX338178B MX2012007050A MX2012007050A MX338178B MX 338178 B MX338178 B MX 338178B MX 2012007050 A MX2012007050 A MX 2012007050A MX 2012007050 A MX2012007050 A MX 2012007050A MX 338178 B MX338178 B MX 338178B
Authority
MX
Mexico
Prior art keywords
rotor
rotor disk
supersonic compressor
flow channel
disks
Prior art date
Application number
MX2012007050A
Other languages
English (en)
Other versions
MX2012007050A (es
Inventor
Douglas Carl Hofer
Zachary William Nagel
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 MX2012007050A publication Critical patent/MX2012007050A/es
Publication of MX338178B publication Critical patent/MX338178B/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
    • F04D21/00—Pump involving supersonic speed of pumped fluids
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/10—Centrifugal pumps for compressing or evacuating
    • F04D17/12—Multi-stage pumps
    • F04D17/127—Multi-stage pumps with radially spaced stages, e.g. for contrarotating type
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

La presente invención proporciona un compresor supersónico que comprende un rotor de compresor supersónico (100) comprendiendo un disco de rotor acoplable que permite la restricción o abertura de porciones de un canal de flujo de fluido del rotor con el fin de mejorar el funcionamiento del rotor durante diferentes etapas operacionales, por ejemplo, encendido del rotor o estado estacionario. El rotor de compresor supersónico (100) comprende un primer disco de rotor (101), un segundo disco de rotor (102), y un tercer disco de rotor (103), los cuales comparten un eje común de rotación. Los primero y segundo discos de rotor (101, 102) están giratoriamente acoplados, y el tercer disco de rotor (103) está dispuesto entre ellos. El tercer disco de rotor (103) es independientemente giratorio con relación a dichos primero y segundo discos (101, 102), y comprende una estructura de superficie erguida (110) para restringir o abrir una porción del canal de flujo definido por los discos de rotor (101, 102, 103) y por lo menos dos paletas (150). El canal de flujo comprende una rampa de compresión supersónica (120) y abarca la estructura de superficie erguida (110).
MX2012007050A 2009-12-16 2010-10-08 Rotor de compresor supersonica. MX338178B (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/639,036 US9103345B2 (en) 2009-12-16 2009-12-16 Supersonic compressor rotor
PCT/US2010/051887 WO2011075204A1 (en) 2009-12-16 2010-10-08 Supersonic compressor rotor

Publications (2)

Publication Number Publication Date
MX2012007050A MX2012007050A (es) 2012-08-23
MX338178B true MX338178B (es) 2016-04-06

Family

ID=43402097

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2012007050A MX338178B (es) 2009-12-16 2010-10-08 Rotor de compresor supersonica.

Country Status (9)

Country Link
US (1) US9103345B2 (es)
EP (1) EP2513485B1 (es)
JP (1) JP5728022B2 (es)
CN (1) CN102753832B (es)
AU (1) AU2010332262B2 (es)
BR (1) BR112012014659A2 (es)
CA (1) CA2784370A1 (es)
MX (1) MX338178B (es)
WO (1) WO2011075204A1 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9022730B2 (en) 2010-10-08 2015-05-05 General Electric Company Supersonic compressor startup support system
EP2668455B1 (en) * 2011-01-26 2019-11-20 Carrier Corporation System to perform a vapor compression refrigeration cycle using water as the refrigerant
US8827640B2 (en) * 2011-03-01 2014-09-09 General Electric Company System and methods of assembling a supersonic compressor rotor including a radial flow channel
US8550770B2 (en) * 2011-05-27 2013-10-08 General Electric Company Supersonic compressor startup support system
US8770929B2 (en) * 2011-05-27 2014-07-08 General Electric Company Supersonic compressor rotor and method of compressing a fluid
US9909597B2 (en) 2013-10-15 2018-03-06 Dresser-Rand Company Supersonic compressor with separator
CN104912821B (zh) * 2015-06-16 2018-02-23 常州协发机械制造有限公司 一种激波压缩机
WO2019160550A1 (en) * 2018-02-15 2019-08-22 Dresser-Rand Company Centrifugal compressor achieving high pressure ratio
CN110173443B (zh) * 2019-04-18 2024-05-28 西安热工研究院有限公司 微小体积流量超临界工质半开式离心压缩装置及方法

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Publication number Priority date Publication date Assignee Title
US2579049A (en) * 1949-02-04 1951-12-18 Nathan C Price Rotating combustion products generator and turbine of the continuous combustion type
US2947139A (en) * 1957-08-29 1960-08-02 United Aircraft Corp By-pass turbojet
FR1246160A (fr) * 1957-12-19 1960-11-18 American Mach & Foundry Procédé de compression de fluides au moyen de compresseurs centripètes
US3187816A (en) * 1962-12-28 1965-06-08 Herman G A Winter Fluid power screw
US3797239A (en) * 1965-10-24 1974-03-19 United Aircraft Corp Supersonic combustion engine
US3879941A (en) * 1973-05-21 1975-04-29 Gen Electric Variable cycle gas turbine engine
US4199296A (en) * 1974-09-03 1980-04-22 Chair Rory S De Gas turbine engines
FR2506840A1 (fr) 1981-05-29 1982-12-03 Onera (Off Nat Aerospatiale) Turboreacteur a roues contra-rotatives
FR2513697A1 (fr) * 1981-09-25 1983-04-01 Snecma Moteur de propulsion, notamment pour avion supersonique
CN1087405A (zh) 1992-11-25 1994-06-01 发动机制造设计局 叶片式压缩机的转子
KR100389990B1 (ko) 1995-04-06 2003-11-17 가부시끼가이샤 히다치 세이사꾸쇼 가스터빈
US7334990B2 (en) * 2002-01-29 2008-02-26 Ramgen Power Systems, Inc. Supersonic compressor
WO2004029432A2 (en) * 2002-09-26 2004-04-08 Ramgen Power Systems, Inc. Gas turbine power plant with supersonic gas 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
US6901739B2 (en) * 2003-10-07 2005-06-07 General Electric Company Gas turbine engine with variable pressure ratio fan system
US7076952B1 (en) * 2005-01-02 2006-07-18 Jan Vetrovec Supercharged internal combustion engine
ATE530771T1 (de) * 2008-01-18 2011-11-15 Ramgen Power Systems Llc Verfahren und vorrichtung zum starten von überschallverdichtern
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

Also Published As

Publication number Publication date
EP2513485B1 (en) 2017-12-13
JP5728022B2 (ja) 2015-06-03
CN102753832B (zh) 2016-03-30
JP2013514491A (ja) 2013-04-25
EP2513485A1 (en) 2012-10-24
US9103345B2 (en) 2015-08-11
AU2010332262A1 (en) 2012-07-05
WO2011075204A1 (en) 2011-06-23
MX2012007050A (es) 2012-08-23
AU2010332262B2 (en) 2016-02-11
BR112012014659A2 (pt) 2016-04-05
CN102753832A (zh) 2012-10-24
US20110142592A1 (en) 2011-06-16
CA2784370A1 (en) 2011-06-23

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