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MX2009004180A - Premezclador para gas y combustible para usarse en combinacion con un dispositivo de conversion/liberacion de energia. - Google Patents

Premezclador para gas y combustible para usarse en combinacion con un dispositivo de conversion/liberacion de energia.

Info

Publication number
MX2009004180A
MX2009004180A MX2009004180A MX2009004180A MX2009004180A MX 2009004180 A MX2009004180 A MX 2009004180A MX 2009004180 A MX2009004180 A MX 2009004180A MX 2009004180 A MX2009004180 A MX 2009004180A MX 2009004180 A MX2009004180 A MX 2009004180A
Authority
MX
Mexico
Prior art keywords
fuel
gas
combination
conversion device
premixer
Prior art date
Application number
MX2009004180A
Other languages
English (en)
Inventor
Anatoly M Rakhmailov
Original Assignee
Lean Flame 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 Lean Flame Inc filed Critical Lean Flame Inc
Publication of MX2009004180A publication Critical patent/MX2009004180A/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00015—Trapped vortex combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Of Fluid Fuel (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Preliminary Treatment Of Fibers (AREA)

Abstract

La invención se refiere al uso de un aparato pre-mezclador para gas y combustible en combinación con un dispositivo de conversión/liberación de energía de un tipo caracterizado que tiene una alta velocidad de consumo.
MX2009004180A 2006-10-18 2007-10-18 Premezclador para gas y combustible para usarse en combinacion con un dispositivo de conversion/liberacion de energia. MX2009004180A (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US82999306P 2006-10-18 2006-10-18
PCT/US2007/081803 WO2008049067A2 (en) 2006-10-18 2007-10-18 Premixer for gas and fuel for use in combination with energy release/conversion device

Publications (1)

Publication Number Publication Date
MX2009004180A true MX2009004180A (es) 2009-07-15

Family

ID=39301279

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2009004180A MX2009004180A (es) 2006-10-18 2007-10-18 Premezclador para gas y combustible para usarse en combinacion con un dispositivo de conversion/liberacion de energia.

Country Status (14)

Country Link
US (1) US20080092544A1 (es)
EP (1) EP2076714B1 (es)
JP (1) JP2010507067A (es)
KR (1) KR20090099051A (es)
CN (1) CN101573561B (es)
AU (1) AU2007310971A1 (es)
BR (1) BRPI0718271A2 (es)
CA (1) CA2667093A1 (es)
IL (1) IL198211A (es)
MX (1) MX2009004180A (es)
RU (1) RU2009118442A (es)
SA (1) SA07280547B1 (es)
WO (1) WO2008049067A2 (es)
ZA (1) ZA200902701B (es)

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US10823418B2 (en) 2017-03-02 2020-11-03 General Electric Company Gas turbine engine combustor comprising air inlet tubes arranged around the combustor

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Also Published As

Publication number Publication date
EP2076714B1 (en) 2016-08-31
IL198211A0 (en) 2009-12-24
BRPI0718271A2 (pt) 2013-11-12
CN101573561B (zh) 2012-03-28
HK1138348A1 (en) 2010-08-20
IL198211A (en) 2013-03-24
AU2007310971A1 (en) 2008-04-24
WO2008049067A2 (en) 2008-04-24
ZA200902701B (en) 2010-10-27
SA07280547B1 (ar) 2011-06-22
CA2667093A1 (en) 2008-04-24
JP2010507067A (ja) 2010-03-04
WO2008049067A3 (en) 2008-06-26
US20080092544A1 (en) 2008-04-24
RU2009118442A (ru) 2010-11-27
EP2076714A2 (en) 2009-07-08
KR20090099051A (ko) 2009-09-21
CN101573561A (zh) 2009-11-04

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