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CL2010000671A1 - Sistema para aumentar la potencia de un motor de turbina, que comprende un pasaje con una entrada de aire, una turbina, y un conjunto de boquillas para humidificar el aire aguas arriba de la turbina, dicho conjunto comprende una serie de etapas y subsecciones en un corte transversal del pasaje; y metodos para humidificar el aire. - Google Patents

Sistema para aumentar la potencia de un motor de turbina, que comprende un pasaje con una entrada de aire, una turbina, y un conjunto de boquillas para humidificar el aire aguas arriba de la turbina, dicho conjunto comprende una serie de etapas y subsecciones en un corte transversal del pasaje; y metodos para humidificar el aire.

Info

Publication number
CL2010000671A1
CL2010000671A1 CL2010000671A CL2010000671A CL2010000671A1 CL 2010000671 A1 CL2010000671 A1 CL 2010000671A1 CL 2010000671 A CL2010000671 A CL 2010000671A CL 2010000671 A CL2010000671 A CL 2010000671A CL 2010000671 A1 CL2010000671 A1 CL 2010000671A1
Authority
CL
Chile
Prior art keywords
turbine
passage
air
series
subsections
Prior art date
Application number
CL2010000671A
Other languages
English (en)
Inventor
Bland Robert
Original Assignee
Gas Turbine Efficiency Sweden
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 Gas Turbine Efficiency Sweden filed Critical Gas Turbine Efficiency Sweden
Publication of CL2010000671A1 publication Critical patent/CL2010000671A1/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/057—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Air Humidification (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Sistema para aumentar la potencia que comprende un pasaje con una entrada de aire, una turbina, y un conjunto de boquillas aguas abajo de la entrada de aire y aguas arriba de la turbina, dicho conjunto comprende una serie de etapas con una serie de subsecciones en un corte transversal del pasaje; y método de humidificación de aire.
CL2010000671A 2009-06-26 2010-06-22 Sistema para aumentar la potencia de un motor de turbina, que comprende un pasaje con una entrada de aire, una turbina, y un conjunto de boquillas para humidificar el aire aguas arriba de la turbina, dicho conjunto comprende una serie de etapas y subsecciones en un corte transversal del pasaje; y metodos para humidificar el aire. CL2010000671A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/492,666 US20100326083A1 (en) 2009-06-26 2009-06-26 Spray system, power augmentation system for engine containing spray system and method of humidifying air

Publications (1)

Publication Number Publication Date
CL2010000671A1 true CL2010000671A1 (es) 2011-04-08

Family

ID=42937065

Family Applications (1)

Application Number Title Priority Date Filing Date
CL2010000671A CL2010000671A1 (es) 2009-06-26 2010-06-22 Sistema para aumentar la potencia de un motor de turbina, que comprende un pasaje con una entrada de aire, una turbina, y un conjunto de boquillas para humidificar el aire aguas arriba de la turbina, dicho conjunto comprende una serie de etapas y subsecciones en un corte transversal del pasaje; y metodos para humidificar el aire.

Country Status (14)

Country Link
US (1) US20100326083A1 (es)
EP (1) EP2282030A3 (es)
JP (1) JP5281044B2 (es)
KR (1) KR101211879B1 (es)
CN (1) CN101936219B (es)
AR (1) AR076906A1 (es)
AU (1) AU2010202153C1 (es)
BR (1) BRPI1002352A2 (es)
CA (1) CA2707267C (es)
CL (1) CL2010000671A1 (es)
IL (1) IL206458A (es)
MX (1) MX2010007146A (es)
RU (1) RU2443480C1 (es)
TW (1) TWI411725B (es)

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US10557413B1 (en) * 2014-11-26 2020-02-11 Caldwell Tanks, Inc. Systems and methods for controlling liquid flow to a turbine fogging array
JP6492714B2 (ja) * 2015-02-05 2019-04-03 東京電力ホールディングス株式会社 吸気冷却装置、ガスタービンプラント、及び吸気冷却方法
EP3109441B1 (en) * 2015-06-24 2020-02-19 Aaf Ltd. System for reducing inlet air temperature of a device
FR3065993B1 (fr) * 2017-05-03 2019-05-10 Ge Energy Products France Snc Conduit d'admission pour turbine a gaz ou au fioul munie d'une structure de saturation d'eau
CN112173137B (zh) * 2020-09-25 2022-09-30 中国直升机设计研究所 一种直升机降温进气道
US12196140B1 (en) 2024-04-18 2025-01-14 Ge Infrastructure Technology Llc Inlet conditioning systems and methods for a turbomachine
CN119801733B (zh) * 2024-11-21 2025-09-16 中国航发沈阳发动机研究所 一种射流降温装置

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Also Published As

Publication number Publication date
CA2707267C (en) 2014-03-18
CA2707267A1 (en) 2010-12-26
AU2010202153B2 (en) 2011-07-07
MX2010007146A (es) 2011-01-05
AU2010202153C1 (en) 2012-09-20
US20100326083A1 (en) 2010-12-30
EP2282030A2 (en) 2011-02-09
CN101936219B (zh) 2014-02-19
RU2443480C1 (ru) 2012-02-27
KR101211879B1 (ko) 2012-12-13
BRPI1002352A2 (pt) 2012-03-13
TW201107585A (en) 2011-03-01
IL206458A (en) 2014-04-30
TWI411725B (zh) 2013-10-11
AU2010202153A1 (en) 2011-01-20
EP2282030A3 (en) 2015-03-18
IL206458A0 (en) 2010-12-30
RU2010126193A (ru) 2011-12-27
JP2011007190A (ja) 2011-01-13
AR076906A1 (es) 2011-07-20
KR20110000534A (ko) 2011-01-03
CN101936219A (zh) 2011-01-05
JP5281044B2 (ja) 2013-09-04

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