SG144099A1 - Method for shaping a magnetic field in a magnetic field-enhanced plasma reactor - Google Patents

Method for shaping a magnetic field in a magnetic field-enhanced plasma reactor

Info

Publication number
SG144099A1
SG144099A1 SG200718849-3A SG2007188493A SG144099A1 SG 144099 A1 SG144099 A1 SG 144099A1 SG 2007188493 A SG2007188493 A SG 2007188493A SG 144099 A1 SG144099 A1 SG 144099A1
Authority
SG
Singapore
Prior art keywords
magnetic field
shaping
plasma reactor
enhanced plasma
primary shape
Prior art date
Application number
SG200718849-3A
Other languages
English (en)
Inventor
Scott A Hogenson
Roger Alan Lindley
Daniel J Hoffman
Original Assignee
Applied Materials 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 Applied Materials Inc filed Critical Applied Materials Inc
Publication of SG144099A1 publication Critical patent/SG144099A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
  • Plasma Technology (AREA)
SG200718849-3A 2006-12-18 2007-12-18 Method for shaping a magnetic field in a magnetic field-enhanced plasma reactor SG144099A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/612,012 US7926290B2 (en) 2006-12-18 2006-12-18 Turbine engine with modulated flow fan and method of operation

Publications (1)

Publication Number Publication Date
SG144099A1 true SG144099A1 (en) 2008-07-29

Family

ID=39276756

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200718849-3A SG144099A1 (en) 2006-12-18 2007-12-18 Method for shaping a magnetic field in a magnetic field-enhanced plasma reactor

Country Status (4)

Country Link
US (1) US7926290B2 (ja)
EP (1) EP1939437B1 (ja)
JP (2) JP5306638B2 (ja)
SG (1) SG144099A1 (ja)

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US20110167791A1 (en) * 2009-09-25 2011-07-14 James Edward Johnson Convertible fan engine
US20110167792A1 (en) * 2009-09-25 2011-07-14 James Edward Johnson Adaptive engine
US8695324B2 (en) * 2009-11-20 2014-04-15 General Electric Co. Multistage tip fan
US20110120083A1 (en) * 2009-11-20 2011-05-26 Rollin George Giffin Gas turbine engine with outer fans
US9353684B2 (en) * 2009-12-11 2016-05-31 Northrop Grumman Systems Corporation Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching
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US9896968B2 (en) * 2012-07-30 2018-02-20 United Technologies Corporation Forward compartment baffle arrangement for a geared turbofan engine
US9488101B2 (en) 2013-03-14 2016-11-08 United Technologies Corporation Adaptive fan reverse core geared turbofan engine with separate cold turbine
US9850822B2 (en) 2013-03-15 2017-12-26 United Technologies Corporation Shroudless adaptive fan with free turbine
US10400710B2 (en) * 2013-05-07 2019-09-03 General Electric Company Secondary nozzle for jet engine
US9920710B2 (en) * 2013-05-07 2018-03-20 General Electric Company Multi-nozzle flow diverter for jet engine
JP6554282B2 (ja) 2014-12-24 2019-07-31 川崎重工業株式会社 航空機用エンジン装置
US10030558B2 (en) * 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US10215070B2 (en) * 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
EP3193003A1 (en) * 2016-01-15 2017-07-19 Goodrich Actuation Systems Ltd. Thrust reverser actuation system architecture
CN108518248A (zh) * 2017-04-15 2018-09-11 罗显平 一种螺管转子螺旋桨发动机
EP4015796A3 (en) * 2020-12-18 2022-08-17 The Boeing Company Systems and methods for expanding an operating speed range of a high speed flight vehicle
US11835064B1 (en) 2022-12-27 2023-12-05 Rolls-Royce North American Technologies Inc. Electric fan array for distortion tolerance of turbofan engines
US12025059B1 (en) 2022-12-27 2024-07-02 Rolls-Royce North American Technologies Inc. Distributed electric tip fans for distortion tolerance of turbofan engines

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Also Published As

Publication number Publication date
JP2008151135A (ja) 2008-07-03
EP1939437A3 (en) 2014-07-16
JP2013199936A (ja) 2013-10-03
EP1939437A2 (en) 2008-07-02
EP1939437B1 (en) 2016-11-02
US20080141676A1 (en) 2008-06-19
US7926290B2 (en) 2011-04-19
JP5306638B2 (ja) 2013-10-02
JP5514354B2 (ja) 2014-06-04

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