ATE530771T1 - Verfahren und vorrichtung zum starten von überschallverdichtern - Google Patents

Verfahren und vorrichtung zum starten von überschallverdichtern

Info

Publication number
ATE530771T1
ATE530771T1 AT09701600T AT09701600T ATE530771T1 AT E530771 T1 ATE530771 T1 AT E530771T1 AT 09701600 T AT09701600 T AT 09701600T AT 09701600 T AT09701600 T AT 09701600T AT E530771 T1 ATE530771 T1 AT E530771T1
Authority
AT
Austria
Prior art keywords
gas
compressor
bleed
supersonic
bypass
Prior art date
Application number
AT09701600T
Other languages
English (en)
Inventor
Shawn P Lawlor
Original Assignee
Ramgen Power Systems Llc
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 Llc filed Critical Ramgen Power Systems Llc
Application granted granted Critical
Publication of ATE530771T1 publication Critical patent/ATE530771T1/de

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
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Reciprocating Pumps (AREA)
AT09701600T 2008-01-18 2009-01-16 Verfahren und vorrichtung zum starten von überschallverdichtern ATE530771T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US1152808P 2008-01-18 2008-01-18
PCT/US2009/031340 WO2009092046A1 (en) 2008-01-18 2009-01-16 Method and apparatus for starting supersonic compressors

Publications (1)

Publication Number Publication Date
ATE530771T1 true ATE530771T1 (de) 2011-11-15

Family

ID=40626609

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09701600T ATE530771T1 (de) 2008-01-18 2009-01-16 Verfahren und vorrichtung zum starten von überschallverdichtern

Country Status (9)

Country Link
US (2) US8152439B2 (de)
EP (1) EP2242929B9 (de)
CN (1) CN101918719B (de)
AT (1) ATE530771T1 (de)
AU (1) AU2009205934B2 (de)
BR (1) BRPI0906792A2 (de)
CA (1) CA2712343A1 (de)
MX (1) MX2010007686A (de)
WO (1) WO2009092046A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009092046A1 (en) * 2008-01-18 2009-07-23 Ramgen Power Systems, Llc Method and apparatus for starting supersonic compressors
US9103345B2 (en) 2009-12-16 2015-08-11 General Electric Company Supersonic compressor rotor
US8978380B2 (en) * 2010-08-10 2015-03-17 Dresser-Rand Company Adiabatic compressed air energy storage process
US8668446B2 (en) 2010-08-31 2014-03-11 General Electric Company Supersonic compressor rotor and method of assembling same
US9022730B2 (en) 2010-10-08 2015-05-05 General Electric Company Supersonic compressor startup support system
US8864454B2 (en) 2010-10-28 2014-10-21 General Electric Company System and method of assembling a supersonic compressor system including a supersonic compressor rotor and a compressor assembly
US20120156015A1 (en) 2010-12-17 2012-06-21 Ravindra Gopaldas Devi Supersonic compressor and method of assembling same
US8657571B2 (en) 2010-12-21 2014-02-25 General Electric Company Supersonic compressor rotor and methods for assembling same
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
WO2013009636A2 (en) 2011-07-09 2013-01-17 Ramgen Power Systems, Llc Gas turbine engine with supersonic compressor
CN103047154A (zh) 2011-07-09 2013-04-17 拉姆金动力系统有限责任公司 超音速压缩机
CN102507203B (zh) * 2011-11-03 2014-01-15 中国科学院力学研究所 基于激波风洞的高超声速进气道自起动测试装置
US9909597B2 (en) 2013-10-15 2018-03-06 Dresser-Rand Company Supersonic compressor with separator
EP3715320A1 (de) * 2019-03-27 2020-09-30 Siemens Aktiengesellschaft Verfahren zur erzeugung eines gasprodukts
CN110500299B (zh) * 2019-08-23 2021-04-27 何备荒 超音速超高压二氧化碳压缩机机组
US12066027B2 (en) 2022-08-11 2024-08-20 Next Gen Compression Llc Variable geometry supersonic compressor
WO2024035894A1 (en) 2022-08-11 2024-02-15 Next Gen Compression Llc Method for efficient part load compressor operation

Family Cites Families (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2628768A (en) * 1946-03-27 1953-02-17 Kantrowitz Arthur Axial-flow compressor
US2721693A (en) * 1949-05-24 1955-10-25 Onera (Off Nat Aerospatiale) Supersonic compressor
US2853852A (en) * 1956-12-10 1958-09-30 Jr Albert G Bodine Boundary layer control for aerodynamic ducts
US2971329A (en) * 1959-07-20 1961-02-14 United Aircraft Corp Air-inlet controller
US2971330A (en) * 1959-07-20 1961-02-14 United Aircraft Corp Air-inlet shock controller
US3777487A (en) * 1961-02-09 1973-12-11 Garrett Corp Method and apparatus for reaction propulsion
US3783616A (en) * 1961-03-02 1974-01-08 Garrett Corp Control method for detonation combustion engines
GB1166733A (en) * 1967-02-14 1969-10-08 Minster Of Technology London Aircraft Engine Intake Ducts
US3643676A (en) * 1970-06-15 1972-02-22 Us Federal Aviation Admin Supersonic air inlet control system
FR2248732A5 (de) * 1973-10-23 1975-05-16 Onera (Off Nat Aerospatiale)
US3846039A (en) * 1973-10-23 1974-11-05 Stalker Corp Axial flow compressor
US4199296A (en) * 1974-09-03 1980-04-22 Chair Rory S De Gas turbine engines
US4000869A (en) * 1975-10-21 1977-01-04 Northrop Corporation Strong shock boundary layer interaction control system
US4123196A (en) * 1976-11-01 1978-10-31 General Electric Company Supersonic compressor with off-design performance improvement
FR2487018A1 (fr) * 1980-07-16 1982-01-22 Onera (Off Nat Aerospatiale) Perfectionnements aux compresseurs supersoniques
US4477039A (en) * 1982-06-30 1984-10-16 Mcdonnell Douglas Corporation Vented cowl variable geometry inlet for aircraft
US4741497A (en) * 1984-11-23 1988-05-03 Fox Brothers Limited Partnership Graduated aircraft design and construction method
US4607657A (en) * 1985-10-28 1986-08-26 General Electric Company Aircraft engine inlet
US4879895A (en) * 1988-08-29 1989-11-14 Mcdonnell Douglas Corporation Normal shock locator
US4872807A (en) * 1988-12-05 1989-10-10 United Technologies Corporation Static pressure system for gas turbine engines
US5074118A (en) * 1989-01-09 1991-12-24 United Technologies Corporation Air turbo-ramjet engine
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
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
CN1092289C (zh) * 1996-12-16 2002-10-09 拉姆金动力系统公司 产生动力用的冲压喷射发动机
US5904470A (en) * 1997-01-13 1999-05-18 Massachusetts Institute Of Technology Counter-rotating compressors with control of boundary layers by fluid removal
US6009406A (en) * 1997-12-05 1999-12-28 Square D Company Methodology and computer-based tools for re-engineering a custom-engineered product line
US6358012B1 (en) * 2000-05-01 2002-03-19 United Technologies Corporation High efficiency turbomachinery blade
US6488469B1 (en) * 2000-10-06 2002-12-03 Pratt & Whitney Canada Corp. Mixed flow and centrifugal compressor for gas turbine engine
US6920890B2 (en) * 2001-07-30 2005-07-26 Techland Research, Inc. Airflow controller
US20030210980A1 (en) * 2002-01-29 2003-11-13 Ramgen Power Systems, Inc. Supersonic compressor
US7334990B2 (en) * 2002-01-29 2008-02-26 Ramgen Power Systems, Inc. Supersonic compressor
US7434400B2 (en) * 2002-09-26 2008-10-14 Lawlor Shawn P Gas turbine power plant with supersonic shock compression ramps
WO2004029451A2 (en) * 2002-09-26 2004-04-08 Ramgen Power Systems, Inc. Supersonic gas compressor
US7293955B2 (en) * 2002-09-26 2007-11-13 Ramgen Power Systrms, Inc. Supersonic gas compressor
US7147426B2 (en) * 2004-05-07 2006-12-12 Pratt & Whitney Canada Corp. Shockwave-induced boundary layer bleed
US7252263B1 (en) * 2004-07-29 2007-08-07 Hawker Beechcraft Corporation Design methods and configurations for supersonic aircraft
WO2009092046A1 (en) * 2008-01-18 2009-07-23 Ramgen Power Systems, Llc Method and apparatus for starting supersonic compressors

Also Published As

Publication number Publication date
US8152439B2 (en) 2012-04-10
US20090196731A1 (en) 2009-08-06
EP2242929B9 (de) 2012-04-25
CN101918719B (zh) 2013-10-02
CN101918719A (zh) 2010-12-15
EP2242929B1 (de) 2011-10-26
AU2009205934B2 (en) 2013-12-12
WO2009092046A1 (en) 2009-07-23
US8500391B1 (en) 2013-08-06
AU2009205934A1 (en) 2009-07-23
EP2242929A1 (de) 2010-10-27
US20130223975A1 (en) 2013-08-29
MX2010007686A (es) 2010-10-04
CA2712343A1 (en) 2009-07-23
BRPI0906792A2 (pt) 2015-07-14

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