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SE9001450L - Saett och anordning foer att minska differentialtryckpaakaenning i foerstaerkt gasturbinmotor - Google Patents

Saett och anordning foer att minska differentialtryckpaakaenning i foerstaerkt gasturbinmotor

Info

Publication number
SE9001450L
SE9001450L SE9001450A SE9001450A SE9001450L SE 9001450 L SE9001450 L SE 9001450L SE 9001450 A SE9001450 A SE 9001450A SE 9001450 A SE9001450 A SE 9001450A SE 9001450 L SE9001450 L SE 9001450L
Authority
SE
Sweden
Prior art keywords
gas turbine
turbine engine
differential pressure
setting
liner
Prior art date
Application number
SE9001450A
Other languages
Unknown language ( )
English (en)
Other versions
SE469188B (sv
SE9001450D0 (sv
Inventor
J C Mayer
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SE9001450D0 publication Critical patent/SE9001450D0/sv
Publication of SE9001450L publication Critical patent/SE9001450L/sv
Publication of SE469188B publication Critical patent/SE469188B/sv

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Spray-Type Burners (AREA)
SE9001450A 1989-04-26 1990-04-23 Gasturbinmotor samt saett att i en foerstaerkare eller tillskottsdel till en saadan oeka motstaandet mot buckelbildning SE469188B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/343,226 US5070690A (en) 1989-04-26 1989-04-26 Means and method for reducing differential pressure loading in an augmented gas turbine engine

Publications (3)

Publication Number Publication Date
SE9001450D0 SE9001450D0 (sv) 1990-04-23
SE9001450L true SE9001450L (sv) 1990-10-27
SE469188B SE469188B (sv) 1993-05-24

Family

ID=23345221

Family Applications (1)

Application Number Title Priority Date Filing Date
SE9001450A SE469188B (sv) 1989-04-26 1990-04-23 Gasturbinmotor samt saett att i en foerstaerkare eller tillskottsdel till en saadan oeka motstaandet mot buckelbildning

Country Status (8)

Country Link
US (1) US5070690A (sv)
JP (1) JP2891743B2 (sv)
CN (1) CN1028663C (sv)
CA (1) CA2012228C (sv)
DE (1) DE4012756A1 (sv)
FR (1) FR2646474B1 (sv)
GB (1) GB2233714B (sv)
SE (1) SE469188B (sv)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6901739B2 (en) * 2003-10-07 2005-06-07 General Electric Company Gas turbine engine with variable pressure ratio fan system
US7216475B2 (en) * 2003-11-21 2007-05-15 General Electric Company Aft FLADE engine
US7334409B2 (en) * 2004-05-19 2008-02-26 Alltech, Inc. Retractable afterburner for jet engine
US7100358B2 (en) * 2004-07-16 2006-09-05 Pratt & Whitney Canada Corp. Turbine exhaust case and method of making
US7828546B2 (en) * 2005-06-30 2010-11-09 General Electric Company Naturally aspirated fluidic control for diverting strong pressure waves
EP1989486A1 (de) * 2006-02-28 2008-11-12 Siemens Aktiengesellschaft Gasturbinenbrenner und verfahren zum betreiben eines gasturbinenbrenners
US8726670B2 (en) * 2010-06-24 2014-05-20 General Electric Company Ejector purge of cavity adjacent exhaust flowpath
CN101975121A (zh) * 2010-10-19 2011-02-16 靳北彪 涵道套装涡轮喷气发动机
US20140208714A1 (en) * 2012-12-19 2014-07-31 United Technologies Corporation Thermal Management for Gas Turbine Engine
CN108131325B (zh) * 2017-12-19 2020-01-24 北京理工大学 轴向超音通流转叶激波静叶风扇级
CN111636976B (zh) * 2020-06-08 2021-10-19 清华大学 一种三涵道大推重比高效动力推进器
CN114060853B (zh) * 2021-12-02 2022-07-19 厦门大学 一种用于一体化加力燃烧室的多级梯齿型混合器

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3296800A (en) * 1967-01-10 Gas turbine power plant
US3374631A (en) * 1965-08-16 1968-03-26 Mcdonnell Aircraft Corp Combination subsonic and supersonic propulsion system and apparatus
US3491539A (en) * 1967-07-13 1970-01-27 Thiokol Chemical Corp Injector assembly for eliminating the smoke trail of a solid propellant rocket motor
FR1558584A (sv) * 1968-01-17 1969-02-28
US3712062A (en) * 1968-04-17 1973-01-23 Gen Electric Cooled augmentor liner
DE1923150A1 (de) * 1968-05-08 1970-01-15 Man Turbo Gmbh Zweistromturbinenstrahltriebwerk
FR1588974A (sv) * 1968-10-02 1970-03-16
US4335573A (en) * 1970-09-02 1982-06-22 General Electric Company Gas turbine engine mixer
US4085583A (en) * 1975-03-31 1978-04-25 The Boeing Company Method for selectively switching motive fluid supply to an aft turbine of a multicycle engine
US4064692A (en) * 1975-06-02 1977-12-27 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable cycle gas turbine engines
US4069661A (en) * 1975-06-02 1978-01-24 The United States Of America As Represented By The United States National Aeronautics And Space Administration Variable mixer propulsion cycle
JPS5946825B2 (ja) * 1978-01-30 1984-11-15 トヨタ自動車株式会社 ステアリングメインシヤフトの支持構造
US4285194A (en) * 1979-04-23 1981-08-25 General Electric Company Apparatus and method for controlling fan duct flow in a gas turbine engine
US4833881A (en) * 1984-12-17 1989-05-30 General Electric Company Gas turbine engine augmentor
US4813229A (en) * 1985-03-04 1989-03-21 General Electric Company Method for controlling augmentor liner coolant flow pressure in a mixed flow, variable cycle gas

Also Published As

Publication number Publication date
FR2646474A1 (fr) 1990-11-02
GB2233714A (en) 1991-01-16
JP2891743B2 (ja) 1999-05-17
SE469188B (sv) 1993-05-24
FR2646474B1 (fr) 1994-10-28
SE9001450D0 (sv) 1990-04-23
CN1028663C (zh) 1995-05-31
JPH0315651A (ja) 1991-01-24
GB2233714B (en) 1993-11-17
CA2012228A1 (en) 1990-10-26
DE4012756A1 (de) 1990-10-31
CN1046958A (zh) 1990-11-14
GB9009299D0 (en) 1990-06-20
CA2012228C (en) 1999-08-24
US5070690A (en) 1991-12-10

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