BRPI0513524A - compressed air generation system - Google Patents

compressed air generation system

Info

Publication number
BRPI0513524A
BRPI0513524A BRPI0513524-9A BRPI0513524A BRPI0513524A BR PI0513524 A BRPI0513524 A BR PI0513524A BR PI0513524 A BRPI0513524 A BR PI0513524A BR PI0513524 A BRPI0513524 A BR PI0513524A
Authority
BR
Brazil
Prior art keywords
compressed air
gas turbine
generation system
generation
fed
Prior art date
Application number
BRPI0513524-9A
Other languages
Portuguese (pt)
Inventor
Paul J J Rn
Original Assignee
Airbus Gmbh
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
Priority claimed from DE102004039019A external-priority patent/DE102004039019A1/en
Application filed by Airbus Gmbh filed Critical Airbus Gmbh
Publication of BRPI0513524A publication Critical patent/BRPI0513524A/en

Links

Landscapes

  • Control Of Turbines (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

SISTEMA DE GERAçãO DE AR COMPRIMIDO Um sistema compreende um gerador a vapor (2) para a geração de um vapor super-aquecido alimentado diretamente para uma turbina a gás (8) a fim de colocar a mesma em uma velocidade rotativa suficiente para resultar em uma razão de ar comprimido na turbina a gás que permita a operação da turbina a gás com um combustível, ou que o vapor super-aquecido seja alimentado para um gerador de ar comprimido (4) para a geração de ar comprimido, em que o ar comprimido gerado é alimentado para um sistema de ar comprimido (7), por exemplo, de uma aeronave, ou é usado para dar a partida a uma turbina a gás ou para outros sistemas de ar comprimido.COMPRESSED AIR GENERATION SYSTEM A system comprises a steam generator (2) for the generation of an overheated steam fed directly to a gas turbine (8) in order to place it at a rotational speed sufficient to result in a compressed air ratio in the gas turbine allowing operation of the gas turbine with a fuel, or overheated steam being fed to a compressed air generator (4) for the generation of compressed air, where compressed air The generated power is fed to a compressed air system (7), for example of an aircraft, or is used to start a gas turbine or other compressed air systems.

BRPI0513524-9A 2004-08-11 2005-08-10 compressed air generation system BRPI0513524A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US60050204P 2004-08-11 2004-08-11
DE102004039019A DE102004039019A1 (en) 2004-08-11 2004-08-11 Compressed air generating system for starting gas turbine e.g. aircraft engine has hydrogen/oxygen steam generator that produces steam that is fed into gas turbine for gas turbine to reach sufficiently high rotary speed
PCT/EP2005/008691 WO2006015857A1 (en) 2004-08-11 2005-08-10 Compressed-air generating system

Publications (1)

Publication Number Publication Date
BRPI0513524A true BRPI0513524A (en) 2008-05-06

Family

ID=39294137

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0513524-9A BRPI0513524A (en) 2004-08-11 2005-08-10 compressed air generation system

Country Status (4)

Country Link
AT (1) ATE423271T1 (en)
BR (1) BRPI0513524A (en)
DE (1) DE602005012837D1 (en)
RU (1) RU2423616C2 (en)

Also Published As

Publication number Publication date
RU2423616C2 (en) 2011-07-10
ATE423271T1 (en) 2009-03-15
DE602005012837D1 (en) 2009-04-02
RU2007102026A (en) 2008-09-20

Similar Documents

Publication Publication Date Title
BR112017018148A2 (en) A thrust generator and an airplane
BRPI0607421A2 (en) fuel cell emergency system
BR9905893A (en) Apparatus for adding nitrogen and moisture derived from low pressure steam from combustible gas used to drive a gas turbine and for adding low pressure steam and nitrogen to combustible gas used to drive a gas turbine system, and, process for increase the energy output of a gas turbine system.
BRPI0618012A8 (en) IMPROVED AIR FLOW DISTRIBUTION FOR A LOW COMBUSTION EMMITTER
US20130031912A1 (en) Gas turbine start architecture
EP2511487A3 (en) Combined cycle power plant
WO2008091502A3 (en) Power augmentation of combustion turbines by injection of cold air upstream of compressor
US9517843B2 (en) Generator for flight vehicle
BR112015009878A2 (en) aircraft propelled by a counter-rotating turboprop
PE20010079A1 (en) SYSTEM AND METHOD TO CONVERT LIGHT HYDROCARBONS INTO HEAVY HYDROCARBONS WITH MULTIPLE SYNTHESIS GAS SUBSYSTEMS
BR112013005250A2 (en) gas turbine engine comprising axial retaining means of a fan of said engine
FR2911916B1 (en) GAS TURBINE ENGINE INCORPORATING A STARTER MOUNTED ON THE GEARBOX
BR112015015613A2 (en) electrical power system for an aircraft and method for producing electrical power in an aircraft
EA200970199A1 (en) KNOT OF A WIND AIR ENGINE AND MECHANICAL VEHICLE WITH THIS KNOT
ITCO20100026A1 (en) TURBOESPANSORE FOR POWER GENERATION SYSTEMS
BRPI0805148A2 (en) internal combustion engine fitted with a combustion chamber and an exhaust gas system and method for operating an internal combustion engine
BR112012027246A2 (en) turbine equipped with sealing air valve system
Jansohn Overview of gas turbine types and applications
BRPI0507437A (en) method for generating power from a control station to a natural gas distribution system
BR112016005119A2 (en) system and emergency start method of an aircraft turbomachine
BRPI0513524A (en) compressed air generation system
EP2423461A3 (en) Systems Involving Hybrid Power Plants
BR0206743A (en) Arrangement and method for vehicle compressed air systems
BR9913938A (en) Process for the preparation of ethylene oxide
RU2000131795A (en) POWER INSTALLATION OF THE AIRCRAFT

Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS OPERATIONS GMBH (DE)

Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 9A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2266 DE 10/06/2014.