WO2004029451A3 - Supersonic gas compressor - Google Patents

Supersonic gas compressor Download PDF

Info

Publication number
WO2004029451A3
WO2004029451A3 PCT/US2003/030608 US0330608W WO2004029451A3 WO 2004029451 A3 WO2004029451 A3 WO 2004029451A3 US 0330608 W US0330608 W US 0330608W WO 2004029451 A3 WO2004029451 A3 WO 2004029451A3
Authority
WO
WIPO (PCT)
Prior art keywords
inlet
compressor
gas
supersonic
swirl
Prior art date
Application number
PCT/US2003/030608
Other languages
French (fr)
Other versions
WO2004029451A2 (en
Inventor
Shawn P Lawlor
Mark A Novaresi
Charles C Cornelius
Original Assignee
Ramgen Power Systems Inc
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 Ramgen Power Systems Inc filed Critical Ramgen Power Systems Inc
Priority to AU2003279036A priority Critical patent/AU2003279036A1/en
Publication of WO2004029451A2 publication Critical patent/WO2004029451A2/en
Publication of WO2004029451A3 publication Critical patent/WO2004029451A3/en

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/16Combinations of two or more pumps ; Producing two or more separate gas flows
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D21/00Pump involving supersonic speed of pumped fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • F04D29/682Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps by fluid extraction

Landscapes

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

Abstract

A gas compressor (20) based on the use of a driven rotor (30, 32) having a compression ramp (R) traveling at a local supersonic inlet velocity (based on the combination of inlet gas velocity and tangential speed of the ramp) which compresses inlet gas against a stationary sidewall (42, 44). In using this method to compress inlet gas, the supersonic compressor efficiently achieves high compression ratios while utilizing a compact, stabilized gasdynamic flow path. Operated at supersonic speeds, the inlet stabilizes an oblique/normal shock system in the gasdyanamic flow path formed between the rim of the rotor (30, 32), the strakes (S), and a stationary external housing (22). Part load efficiency is enhanced by the use of a pre-swirl compressor (104, 106), and using a bypass stream to bleed a portion of the intermediate pressure gas after passing through the pre-swirl compressor back to the inlet of the pre-swirl compressor.
PCT/US2003/030608 2002-09-26 2003-09-25 Supersonic gas compressor WO2004029451A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU2003279036A AU2003279036A1 (en) 2002-09-26 2003-09-25 Supersonic gas compressor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US41479302P 2002-09-26 2002-09-26
US60/414,793 2002-09-26

Publications (2)

Publication Number Publication Date
WO2004029451A2 WO2004029451A2 (en) 2004-04-08
WO2004029451A3 true WO2004029451A3 (en) 2005-03-17

Family

ID=32043409

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2003/030608 WO2004029451A2 (en) 2002-09-26 2003-09-25 Supersonic gas compressor

Country Status (3)

Country Link
US (1) US20040151579A1 (en)
AU (1) AU2003279036A1 (en)
WO (1) WO2004029451A2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2009205934B2 (en) * 2008-01-18 2013-12-12 Ramgen Power Systems, Llc Method and apparatus for starting supersonic compressors
US8668446B2 (en) * 2010-08-31 2014-03-11 General Electric Company Supersonic compressor rotor and method of assembling same
US9493903B2 (en) * 2014-10-27 2016-11-15 Haier Us Appliance Solutions, Inc. Impeller assembly for an appliance
EP3557078A1 (en) * 2018-04-20 2019-10-23 Belenos Clean Power Holding AG Fluid compressor
CN116379002B (en) * 2023-06-05 2023-08-11 中国空气动力研究与发展中心空天技术研究所 Design method of equal-rotation-speed reversing diffuser structure and diffuser structure

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5562405A (en) * 1994-03-10 1996-10-08 Weir Pumps Limited Multistage axial flow pumps and compressors

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU721469B2 (en) * 1996-12-16 2000-07-06 Ramgen Power Systems, Llc Ramjet engine for power generation

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5562405A (en) * 1994-03-10 1996-10-08 Weir Pumps Limited Multistage axial flow pumps and compressors

Also Published As

Publication number Publication date
AU2003279036A8 (en) 2004-04-19
WO2004029451A2 (en) 2004-04-08
US20040151579A1 (en) 2004-08-05
AU2003279036A1 (en) 2004-04-19

Similar Documents

Publication Publication Date Title
EP1148927B1 (en) Gas separation with split stream centrifugal turbomachinery
CA2337790A1 (en) Low speed high pressure ratio turbocharger
WO2006026133A3 (en) Multi-stage turbocharging system with efficient bypass
CA2486013A1 (en) Device for utilizing the waste heat of compressors
CA2325048A1 (en) Small turbo compressor
EP1273859A3 (en) Ejector cycle system
US7382061B2 (en) Supercharger coupled to a motor/generator unit
ATE510130T1 (en) TWO-STAGE ROTARY PISTON COMPRESSOR
US20020056374A1 (en) Gas separation with split stream centrifugal turbomachinery
WO2002044562A3 (en) Hermetic compressor
JP2966575B2 (en) Oil-free scroll compressor
WO2004099588A3 (en) Supersonic compressor
WO2004029451A3 (en) Supersonic gas compressor
WO2004029432A3 (en) Gas turbine power plant with supersonic gas compressor
EP0743458A3 (en) Variable speed centrifugal compressors for adsorption systems
EP1418341A3 (en) Axial thrust balancing system for a centrifugal compressor, having improved safety characteristics
US9377025B2 (en) Compressor housing and two-stage turbocharger thereof
CA2383429A1 (en) Method and device for increasing the pressure of a gas
CA2154238A1 (en) Noise Control in a Centrifugal Chiller
US6672856B1 (en) Diffuser guide vanes for high-speed screw compressor
RU2064067C1 (en) Double-flow turbojet engine
WO2003100333A8 (en) Low pressure impact separator for separation, classification and collection of ultra­fine particles
JP3438356B2 (en) Multi-stage centrifugal compressor
RU2143574C1 (en) Cooled multistage turbine of turbojet engine
US20030206809A1 (en) Method for creating an air pressure

Legal Events

Date Code Title Description
AK Designated states

Kind code of ref document: A2

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NO NZ OM PH PL PT RO RU SC SD SE SG SK SL TJ TM TN TR TT TZ UA UG UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A2

Designated state(s): GH GM KE LS MW MZ SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
DFPE Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed before 20040101)
122 Ep: pct application non-entry in european phase
NENP Non-entry into the national phase

Ref country code: JP

WWW Wipo information: withdrawn in national office

Country of ref document: JP