PL421253A1 - System wylotowy sprężarki - Google Patents

System wylotowy sprężarki

Info

Publication number
PL421253A1
PL421253A1 PL421253A PL42125317A PL421253A1 PL 421253 A1 PL421253 A1 PL 421253A1 PL 421253 A PL421253 A PL 421253A PL 42125317 A PL42125317 A PL 42125317A PL 421253 A1 PL421253 A1 PL 421253A1
Authority
PL
Poland
Prior art keywords
bleed
pressure area
compressor outlet
outlet system
low pressure
Prior art date
Application number
PL421253A
Other languages
English (en)
Inventor
Przemysław Sebastian Drezek
Michael Anthony Acosta
Victor Gerardo Cabal-Velarde
Richard Michael Watkins
David Garza-Maldonado
Original Assignee
General Electric Company
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 General Electric Company filed Critical General Electric Company
Priority to PL421253A priority Critical patent/PL421253A1/pl
Priority to US15/585,010 priority patent/US10641171B2/en
Priority to CN201820500167.8U priority patent/CN209067294U/zh
Publication of PL421253A1 publication Critical patent/PL421253A1/pl

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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid flow
    • F02C9/52—Control of fuel supply conjointly with another control of the plant with control of working fluid flow by bleeding or by-passing the working fluid
    • 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
    • F02C9/24—Control of the pressure level in closed cycles

Landscapes

  • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pipeline Systems (AREA)

Abstract

System obejmuje system upustowy (36), który kieruje przepływ upustowy z obszaru wysokiego ciśnienia (44) do obszaru niskiego ciśnienia. System upustowy zawiera przewód upustowy (40), który zawiera wlot połączony z obszarem wysokiego ciśnienia. System upustowy zawiera także wylot, który zapewnia przepływ upustowy do obszaru niskiego ciśnienia. Przewód upustowy jest połączony przesuwnie z obudową, która wyznacza obszar niskiego ciśnienia.
PL421253A 2017-04-10 2017-04-10 System wylotowy sprężarki PL421253A1 (pl)

Priority Applications (3)

Application Number Priority Date Filing Date Title
PL421253A PL421253A1 (pl) 2017-04-10 2017-04-10 System wylotowy sprężarki
US15/585,010 US10641171B2 (en) 2017-04-10 2017-05-02 Compressor discharge system
CN201820500167.8U CN209067294U (zh) 2017-04-10 2018-04-10 放气系统以及燃气涡轮发动机

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL421253A PL421253A1 (pl) 2017-04-10 2017-04-10 System wylotowy sprężarki

Publications (1)

Publication Number Publication Date
PL421253A1 true PL421253A1 (pl) 2018-10-22

Family

ID=63710789

Family Applications (1)

Application Number Title Priority Date Filing Date
PL421253A PL421253A1 (pl) 2017-04-10 2017-04-10 System wylotowy sprężarki

Country Status (3)

Country Link
US (1) US10641171B2 (pl)
CN (1) CN209067294U (pl)
PL (1) PL421253A1 (pl)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180142809A1 (en) * 2016-11-23 2018-05-24 General Electric Company Systems and methods for ensuring the correct orientation of tubing in a gas turbine engine
US11808215B2 (en) 2021-11-22 2023-11-07 General Electric Company System and method for reconfiguring a bleed system
US12044178B2 (en) * 2022-01-06 2024-07-23 Ge Infrastructure Technology Llc System and method for air cooling fuel purge flow

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6442941B1 (en) 2000-09-11 2002-09-03 General Electric Company Compressor discharge bleed air circuit in gas turbine plants and related method
US6912856B2 (en) 2003-06-23 2005-07-05 General Electric Company Method and system for controlling gas turbine by adjusting target exhaust temperature
US7607308B2 (en) 2005-12-08 2009-10-27 General Electric Company Shrouded turbofan bleed duct
EP2058524A1 (en) * 2007-11-12 2009-05-13 Siemens Aktiengesellschaft Air bleed compressor with variable guide vanes
US8522528B2 (en) * 2008-06-30 2013-09-03 Solar Turbines Inc. System for diffusing bleed air flow
US8430202B1 (en) 2011-12-28 2013-04-30 General Electric Company Compact high-pressure exhaust muffling devices
RU2490508C1 (ru) 2012-04-24 2013-08-20 Открытое акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель с дожиганием генераторного газа
PL225152B1 (pl) * 2012-12-28 2017-02-28 Gen Electric Układ upustowy sprężarki, zwłaszcza do silnika turbogazowego i silnik turbogazowy zawierający układ upustowy sprężarki
GB201416928D0 (en) * 2014-09-25 2014-11-12 Rolls Royce Plc A gas turbine and a method of washing a gas turbine engine

Also Published As

Publication number Publication date
US20180291806A1 (en) 2018-10-11
US10641171B2 (en) 2020-05-05
CN209067294U (zh) 2019-07-05

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