RU2425994C2 - Узел подачи текучей среды, система увеличения мощности и способ инжектирования текучей среды - Google Patents

Узел подачи текучей среды, система увеличения мощности и способ инжектирования текучей среды Download PDF

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Publication number
RU2425994C2
RU2425994C2 RU2009123447/06A RU2009123447A RU2425994C2 RU 2425994 C2 RU2425994 C2 RU 2425994C2 RU 2009123447/06 A RU2009123447/06 A RU 2009123447/06A RU 2009123447 A RU2009123447 A RU 2009123447A RU 2425994 C2 RU2425994 C2 RU 2425994C2
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RU
Russia
Prior art keywords
fluid
valve
stage
pump
stages
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RU2009123447/06A
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English (en)
Russian (ru)
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RU2009123447A (ru
Inventor
Роберт БЛЭНД (US)
Роберт БЛЭНД
Original Assignee
Гэз Тербайн Иффишенси Свиден Аб
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Application filed by Гэз Тербайн Иффишенси Свиден Аб filed Critical Гэз Тербайн Иффишенси Свиден Аб
Publication of RU2009123447A publication Critical patent/RU2009123447A/ru
Application granted granted Critical
Publication of RU2425994C2 publication Critical patent/RU2425994C2/ru

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    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • 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
    • 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
    • F02C3/305—Increasing the power, speed, torque or efficiency of a gas turbine or the thrust of a turbojet engine by injecting or adding water, steam or other fluids
    • 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
    • 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
    • F02C7/1435—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages by water injection
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Control Of Non-Positive-Displacement Pumps (AREA)
  • Regulating Braking Force (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Details Of Reciprocating Pumps (AREA)
  • Reciprocating Pumps (AREA)
  • Loading And Unloading Of Fuel Tanks Or Ships (AREA)
  • Flow Control (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
RU2009123447/06A 2008-06-20 2009-06-19 Узел подачи текучей среды, система увеличения мощности и способ инжектирования текучей среды RU2425994C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/143,254 2008-06-20
US12/143,254 US7647777B2 (en) 2008-06-20 2008-06-20 Skid architecture for a power augmentation system

Publications (2)

Publication Number Publication Date
RU2009123447A RU2009123447A (ru) 2010-12-27
RU2425994C2 true RU2425994C2 (ru) 2011-08-10

Family

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Family Applications (1)

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RU2009123447/06A RU2425994C2 (ru) 2008-06-20 2009-06-19 Узел подачи текучей среды, система увеличения мощности и способ инжектирования текучей среды

Country Status (16)

Country Link
US (1) US7647777B2 (enExample)
EP (1) EP2136051B1 (enExample)
JP (2) JP4922348B2 (enExample)
KR (1) KR101141824B1 (enExample)
CN (1) CN101608576B (enExample)
AR (1) AR072255A1 (enExample)
AU (1) AU2009201880B2 (enExample)
BR (1) BRPI0902078A2 (enExample)
CA (1) CA2665329C (enExample)
CL (1) CL2009001406A1 (enExample)
IL (1) IL199109A (enExample)
MX (1) MX2009006412A (enExample)
MY (1) MY147076A (enExample)
RU (1) RU2425994C2 (enExample)
SG (1) SG158009A1 (enExample)
TW (1) TWI367281B (enExample)

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RU2653640C2 (ru) * 2013-11-08 2018-05-11 Континенталь Отомотив Франс Способ определения факта нахождения инжектора в заблокированном состоянии

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JP5422456B2 (ja) * 2010-03-24 2014-02-19 三菱重工業株式会社 吸気システム、これを備えたガスタービンおよびこれを備えた発電プラント
JP5818510B2 (ja) * 2011-05-24 2015-11-18 株式会社東芝 ガスタービン吸気冷却装置及び方法
US9086019B2 (en) 2012-07-02 2015-07-21 United Technologies Corporation Turbomachine thermal energy exchange
WO2014072842A1 (en) * 2012-11-06 2014-05-15 Al Mahmood Fuad Reducing the load consumed by gas turbine compressor and maximizing turbine mass flow
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DE102013216083A1 (de) * 2013-08-14 2015-02-19 ES Vertrieb und Service GmbH Luftbefeuchtungsanordnung und Verfahren zum Befeuchten eines Luftstroms
US9850816B2 (en) * 2013-11-04 2017-12-26 General Electric Company Gas turbine inlet system and related method for cooling gas turbine inlet air
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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
US9527585B2 (en) * 2014-12-11 2016-12-27 Bell Helicopter Textron Inc. Aircraft ground steering system
US20170370286A1 (en) * 2016-06-22 2017-12-28 General Electric Company Systems and Methods for Variable Water Injection Flow Control
CN110091588B (zh) * 2018-12-13 2024-06-04 株洲三新包装技术有限公司 一种两端向内喷水清理的刮墨腔
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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2653640C2 (ru) * 2013-11-08 2018-05-11 Континенталь Отомотив Франс Способ определения факта нахождения инжектора в заблокированном состоянии

Also Published As

Publication number Publication date
SG158009A1 (en) 2010-01-29
MX2009006412A (es) 2010-01-15
EP2136051B1 (en) 2015-11-25
IL199109A0 (en) 2010-03-28
JP5400117B2 (ja) 2014-01-29
BRPI0902078A2 (pt) 2010-05-18
US20090314256A1 (en) 2009-12-24
EP2136051A3 (en) 2010-12-22
TWI367281B (en) 2012-07-01
TW201016952A (en) 2010-05-01
JP4922348B2 (ja) 2012-04-25
CL2009001406A1 (es) 2010-11-12
CN101608576A (zh) 2009-12-23
JP2010001893A (ja) 2010-01-07
AR072255A1 (es) 2010-08-18
RU2009123447A (ru) 2010-12-27
KR20090132549A (ko) 2009-12-30
CN101608576B (zh) 2013-06-05
IL199109A (en) 2012-06-28
CA2665329C (en) 2013-10-22
EP2136051A2 (en) 2009-12-23
JP2011256880A (ja) 2011-12-22
KR101141824B1 (ko) 2012-05-07
MY147076A (en) 2012-10-31
US7647777B2 (en) 2010-01-19
AU2009201880B2 (en) 2012-06-14
CA2665329A1 (en) 2009-12-20
AU2009201880A1 (en) 2010-01-14

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20170620