PL3259461T3 - Układ spalania przy stałej objętości do maszyny wirowej silnika statku powietrznego - Google Patents

Układ spalania przy stałej objętości do maszyny wirowej silnika statku powietrznego

Info

Publication number
PL3259461T3
PL3259461T3 PL16713954T PL16713954T PL3259461T3 PL 3259461 T3 PL3259461 T3 PL 3259461T3 PL 16713954 T PL16713954 T PL 16713954T PL 16713954 T PL16713954 T PL 16713954T PL 3259461 T3 PL3259461 T3 PL 3259461T3
Authority
PL
Poland
Prior art keywords
constant
engine
combustion system
volume combustion
turbine engine
Prior art date
Application number
PL16713954T
Other languages
English (en)
Inventor
Guillaume TALIERCIO
Christophe Nicolas Henri Viguier
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3259461T3 publication Critical patent/PL3259461T3/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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • 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
    • F23R7/00—Intermittent or explosive combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PL16713954T 2015-02-17 2016-02-15 Układ spalania przy stałej objętości do maszyny wirowej silnika statku powietrznego PL3259461T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1551301A FR3032781B1 (fr) 2015-02-17 2015-02-17 Systeme de combustion a volume constant pour turbomachine de moteur d'aeronef
PCT/FR2016/050337 WO2016132055A1 (fr) 2015-02-17 2016-02-15 Système de combustion à volume constant pour turbomachine de moteur d'aéronef
EP16713954.2A EP3259461B1 (fr) 2015-02-17 2016-02-15 Système de combustion à volume constant pour turbomachine de moteur d'aéronef

Publications (1)

Publication Number Publication Date
PL3259461T3 true PL3259461T3 (pl) 2020-08-24

Family

ID=53674030

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16713954T PL3259461T3 (pl) 2015-02-17 2016-02-15 Układ spalania przy stałej objętości do maszyny wirowej silnika statku powietrznego

Country Status (10)

Country Link
US (1) US20180038278A1 (pl)
EP (1) EP3259461B1 (pl)
JP (1) JP2018508694A (pl)
KR (1) KR20170117570A (pl)
CN (1) CN107250509B (pl)
CA (1) CA2976148A1 (pl)
FR (1) FR3032781B1 (pl)
PL (1) PL3259461T3 (pl)
RU (1) RU2717473C2 (pl)
WO (1) WO2016132055A1 (pl)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3068075B1 (fr) * 2017-06-23 2019-08-09 Safran Systeme de combustion a volume constant comprenant un element d'obturation tournant a lumieres segmentees
FR3083823B1 (fr) * 2018-07-12 2020-09-25 Safran Systeme d'injection de carburant d'un systeme de combustion a volume constant pour turbomachine
FR3091899B1 (fr) * 2019-01-22 2020-12-25 Safran Aircraft Engines Ensemble pour turbomachine
CN109869241B (zh) * 2019-03-07 2020-07-10 浙江理工大学 超重力燃气发动机装置及方法
USD885438S1 (en) 2019-10-05 2020-05-26 Mountain Aerospace Research Solutions, Inc. Engine
US11174817B2 (en) 2020-01-29 2021-11-16 Mountain Aerospace Research Solutions, Inc. Air-Breathing rocket engine
US11002225B1 (en) 2020-01-29 2021-05-11 Mountain Aerospace Research Solutions, Inc. Air-breathing rocket engine
US10961952B1 (en) 2020-01-29 2021-03-30 Mountain Aerospace Research Solutions, Inc. Air-breathing rocket engine
US11220979B1 (en) 2020-11-10 2022-01-11 Mountain Aerospace Research Solutions, Inc. Liquid-cooled air-breathing rocket engine

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675675A (en) * 1954-04-20 Muctlpefi combustion chamber jet
FR346883A (fr) * 1904-07-04 1905-02-13 Pierre Rambal Turbine à gaz à explosion
US861329A (en) * 1905-07-03 1907-07-30 Der Maschinenfabriken Von Escher Wyss & Co Ag Explosion gas-turbine.
DE387166C (de) * 1922-06-07 1923-12-21 Alfred Krone Drehschiebersteuerung fuer Explosionsturbinen
US1654119A (en) * 1925-12-05 1927-12-27 Enders Karl Internal-combustion turbine with rotary slide valve
US2010823A (en) * 1930-12-11 1935-08-13 Holzwarth Gas Turbine Company Method of and apparatus for supercharging explosion chambers
SU31718A1 (ru) * 1931-05-30 1933-08-31 Б.К. Штавеман Реактивна турбина внутреннего горени
FR772104A (fr) * 1933-04-24 1934-10-23 Procédé pour allumer des mélanges combustibles dans des chambres d'explosion, particulièrement de turbines à combustion
US2579321A (en) * 1948-04-09 1951-12-18 Nina K Guercken Apparatus for producing gas under pressure
DE2232025A1 (de) * 1972-06-30 1974-01-17 Motoren Turbinen Union Gasturbinenanlage, insbesondere triebwerk mit gleichraumverbrennung
US4177638A (en) * 1975-06-24 1979-12-11 Deere & Company Single shaft gas turbine engine with radial exhaust diffuser
GB2035459A (en) * 1978-11-27 1980-06-18 Semery J An intermittent combustion gas turbine plant
SU1149688A1 (ru) * 1983-07-18 1997-01-20 Н.К. Рязанцев Газотурбинный двигатель периодического сгорания
US4693075A (en) * 1984-10-31 1987-09-15 Andrew Sabatiuk Gas turbine engines employing fixed volume combustion
JPS63268938A (ja) * 1987-04-27 1988-11-07 Nec Corp ガスタ−ビンエンジン
US4993220A (en) * 1989-07-24 1991-02-19 Sundstrand Corporation Axial flow gas turbine engine combustor
US5237811A (en) * 1990-12-26 1993-08-24 Stockwell James K Rotary internal combustion engine apparatus
US5615548A (en) * 1995-07-26 1997-04-01 Lockheed Martin Corporation Dual rotor pulse detonation apparatus
JP3952202B2 (ja) * 2004-02-19 2007-08-01 独立行政法人 宇宙航空研究開発機構 パルスデトネーションエンジン
US6983604B1 (en) * 2004-07-30 2006-01-10 Samuel Barran Tafoya Thermodynamic pressure generator
US8065881B2 (en) * 2008-08-12 2011-11-29 Siemens Energy, Inc. Transition with a linear flow path with exhaust mouths for use in a gas turbine engine
FR2970304B1 (fr) * 2011-01-11 2013-02-08 Turbomeca Procede de demarrage d'une turbomachine
KR101774093B1 (ko) * 2011-08-22 2017-09-12 마제드 토칸 가스 터빈 엔진에서 사용되는 스테이지가 형성되고 접선방향으로 형성된 연료-공기 노즐을 가진 캔-애뉼러형 연소실
US9121302B2 (en) * 2012-07-12 2015-09-01 Hamilton Sundstrand Corporation Radial compressor blade clearance control system
CN203879631U (zh) * 2014-06-04 2014-10-15 华能国际电力股份有限公司 一种利用脉冲爆震燃烧的地面燃气轮机

Also Published As

Publication number Publication date
JP2018508694A (ja) 2018-03-29
KR20170117570A (ko) 2017-10-23
CA2976148A1 (fr) 2016-08-25
US20180038278A1 (en) 2018-02-08
CN107250509B (zh) 2020-07-28
EP3259461A1 (fr) 2017-12-27
RU2017132266A3 (pl) 2019-08-29
CN107250509A (zh) 2017-10-13
RU2017132266A (ru) 2019-03-18
RU2717473C2 (ru) 2020-03-23
EP3259461B1 (fr) 2020-05-06
FR3032781B1 (fr) 2018-07-06
WO2016132055A1 (fr) 2016-08-25
FR3032781A1 (fr) 2016-08-19

Similar Documents

Publication Publication Date Title
PL3259461T3 (pl) Układ spalania przy stałej objętości do maszyny wirowej silnika statku powietrznego
EP3088688B8 (en) Lubrication system for gas turbine engines
EP3150918A4 (en) Combustion device for gas turbine engine
GB201610878D0 (en) Gas turbine engine
GB201407743D0 (en) Gas turbine engine fuel system
GB201418685D0 (en) Gas turbine engine fuel system
GB2544735B (en) Vanes of a gas turbine engine
GB201511841D0 (en) Fuel spray nozel for a gas turbine engine
GB201610877D0 (en) Gas Turbine engine
GB201600180D0 (en) Gas turbine engine
GB201610879D0 (en) Gas turbine engine
GB2545538B (en) A gas turbine engine having sequential combustion
PL3321489T3 (pl) Konfiguracja pobierania powietrza gazowego silnika turbinowego
EP2949883B8 (en) Gas turbine engine lubrication system
GB2551260B (en) A vane for turbomachinery such as an aircraft turbojet or tubofan engine or an aircraft turboprop engine
GB201518345D0 (en) Combustor for a gas turbine engine
GB201616108D0 (en) Gas turbine engine
GB201619960D0 (en) Gas turbine engine
GB201603254D0 (en) Gas turbine engine
GB2522997B (en) Method and system for combustion mode transfer for a gas turbine engine
GB201614888D0 (en) Gas turbine engine
GB201612021D0 (en) A method of operating a gas turbine engine
EP3325343A4 (en) Internal combustion piston engine for aviation
GB201608413D0 (en) Gas turbine engine
GB201516292D0 (en) Method of operating a 5 N aftertreatment system of an internal combustion engine