ZA200801960B - A method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit - Google Patents
A method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit Download PDFInfo
- Publication number
- ZA200801960B ZA200801960B ZA200801960A ZA200801960A ZA200801960B ZA 200801960 B ZA200801960 B ZA 200801960B ZA 200801960 A ZA200801960 A ZA 200801960A ZA 200801960 A ZA200801960 A ZA 200801960A ZA 200801960 B ZA200801960 B ZA 200801960B
- Authority
- ZA
- South Africa
- Prior art keywords
- engine
- circuit
- fuel
- combustion chamber
- main
- Prior art date
Links
- 239000000446 fuel Substances 0.000 title claims description 40
- 238000000034 method Methods 0.000 title claims description 10
- 238000002485 combustion reaction Methods 0.000 claims description 24
- 239000007858 starting material Substances 0.000 claims description 24
- 235000015277 pork Nutrition 0.000 claims 1
- 238000010926 purge Methods 0.000 description 6
- 238000004939 coking Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
-
- 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
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0753613A FR2913250B1 (fr) | 2007-03-02 | 2007-03-02 | Procede pour le demarrage d'un moteur d'helicoptere a turbine a gaz, circuit d'alimentation en carburant d'un tel moteur, et moteur ayant un tel circuit. |
Publications (1)
Publication Number | Publication Date |
---|---|
ZA200801960B true ZA200801960B (en) | 2008-11-26 |
Family
ID=38596743
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ZA200801960A ZA200801960B (en) | 2007-03-02 | 2008-02-29 | A method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit |
Country Status (11)
Country | Link |
---|---|
US (1) | US20080209910A1 (zh) |
EP (1) | EP1965056B1 (zh) |
JP (1) | JP2008215350A (zh) |
CN (1) | CN101255821A (zh) |
AT (1) | ATE463664T1 (zh) |
BR (1) | BRPI0800386A (zh) |
CA (1) | CA2622113A1 (zh) |
DE (1) | DE602008000920D1 (zh) |
FR (1) | FR2913250B1 (zh) |
RU (1) | RU2008108047A (zh) |
ZA (1) | ZA200801960B (zh) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5185757B2 (ja) | 2008-10-01 | 2013-04-17 | 三菱重工業株式会社 | ガスタービンの燃料制御方法および燃料制御装置ならびにガスタービン |
CN101806251B (zh) * | 2010-03-25 | 2012-08-22 | 北京航空航天大学 | 一种微型燃气轮机的起动控制装置以及起动控制方法 |
FR2970304B1 (fr) * | 2011-01-11 | 2013-02-08 | Turbomeca | Procede de demarrage d'une turbomachine |
US8590310B2 (en) * | 2012-03-27 | 2013-11-26 | Hamilton Sundstrand Corporation | Passive equilization flow divider valve |
CN102996223A (zh) * | 2012-11-01 | 2013-03-27 | 大连理工大学 | 柴油机预混合燃烧系统 |
FR3001497B1 (fr) * | 2013-01-29 | 2016-05-13 | Turbomeca | Ensemble de combustion de turbomachine comprenant un circuit d alimentation de carburant ameliore |
FR3015567B1 (fr) * | 2013-12-19 | 2015-12-25 | Turbomeca | Dispositif de drainage de fluides pour un moteur d'aeronef |
CN105083566B (zh) * | 2014-05-07 | 2017-06-06 | 哈尔滨飞机工业集团有限责任公司 | 直升机发动机起动控制电路 |
CZ308533B6 (cs) * | 2016-05-19 | 2020-10-29 | První Brněnská Strojírna Velká Bíteš, A.S. | Malý turbínový motor se zapalovacím systémem |
CN107965390B (zh) * | 2017-12-18 | 2023-09-15 | 中科合肥微小型燃气轮机研究院有限责任公司 | 一种燃气轮机燃油分配装置及其控制方法 |
CN110674582B (zh) * | 2019-09-29 | 2023-08-25 | 中仿智能科技(上海)股份有限公司 | 一种模拟飞行器燃油系统的仿真模型及其方法 |
CN111709119B (zh) * | 2020-05-19 | 2021-07-06 | 中国电子产品可靠性与环境试验研究所((工业和信息化部电子第五研究所)(中国赛宝实验室)) | 压力脉动分析方法、装置、计算机设备和存储介质 |
CN112413645B (zh) * | 2020-11-19 | 2022-06-07 | 中国航发沈阳发动机研究所 | 一种航空发动机加力点火供油方法及系统 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB842354A (en) * | 1956-08-07 | 1960-07-27 | Dowty Fuel Syst Ltd | Improvements in variable liquid supply systems |
US2970440A (en) * | 1958-09-02 | 1961-02-07 | United Aircraft Corp | Starting system for engines |
US5809771A (en) * | 1996-01-19 | 1998-09-22 | Woodward Governor Company | Aircraft engine fuel system |
FR2867552B1 (fr) * | 2004-03-15 | 2008-07-11 | Gen Electric | Injecteur de carburant a pression regulee |
-
2007
- 2007-03-02 FR FR0753613A patent/FR2913250B1/fr not_active Expired - Fee Related
-
2008
- 2008-02-28 CA CA002622113A patent/CA2622113A1/fr not_active Abandoned
- 2008-02-28 EP EP08102136A patent/EP1965056B1/fr active Active
- 2008-02-28 DE DE602008000920T patent/DE602008000920D1/de active Active
- 2008-02-28 AT AT08102136T patent/ATE463664T1/de not_active IP Right Cessation
- 2008-02-29 BR BRPI0800386-6A patent/BRPI0800386A/pt not_active IP Right Cessation
- 2008-02-29 JP JP2008049225A patent/JP2008215350A/ja not_active Withdrawn
- 2008-02-29 ZA ZA200801960A patent/ZA200801960B/en unknown
- 2008-02-29 US US12/040,388 patent/US20080209910A1/en not_active Abandoned
- 2008-02-29 RU RU2008108047/06A patent/RU2008108047A/ru not_active Application Discontinuation
- 2008-03-03 CN CNA200810083125XA patent/CN101255821A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
CN101255821A (zh) | 2008-09-03 |
ATE463664T1 (de) | 2010-04-15 |
FR2913250B1 (fr) | 2009-05-29 |
RU2008108047A (ru) | 2009-09-10 |
CA2622113A1 (fr) | 2008-09-02 |
EP1965056B1 (fr) | 2010-04-07 |
DE602008000920D1 (de) | 2010-05-20 |
JP2008215350A (ja) | 2008-09-18 |
EP1965056A1 (fr) | 2008-09-03 |
BRPI0800386A (pt) | 2008-10-21 |
US20080209910A1 (en) | 2008-09-04 |
FR2913250A1 (fr) | 2008-09-05 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ZA200801960B (en) | A method of starting a gas turbine helicopter engine, a fuel feed circuit for such an engine, and an engine having such a circuit | |
EP1278014B1 (en) | Fuel delivery system | |
EP1865260B1 (en) | Stage one turbine nozzle | |
US7942003B2 (en) | Dual-injector fuel injector system | |
EP2065643A2 (en) | Combusting system, remodeling method for combusting system, and fuel injection method for combusting system | |
US10794296B2 (en) | Gas turbine combustor and method of operating the same | |
EP1605148B1 (fr) | Procédé et système de protection des injecteurs de carburant de turbine à gaz | |
US9631560B2 (en) | Fuel-air mixture distribution for gas turbine engine combustors | |
US5345757A (en) | Combustor apparatus for use in a gas turbine engine | |
US4062183A (en) | Fuel supply system for a gas turbine engine | |
EP2075507A3 (en) | Gas turbine engine combustor and method for delivering purge gas into a combustion chamber of the combustor | |
US11002196B2 (en) | Combustion chamber comprising two types of injectors in which the sealing members have a different opening threshold | |
US9028247B2 (en) | Combustion chamber and method for damping pulsations | |
WO2014076367A1 (en) | Gas feed system for reciprocating engine and installation method | |
US20100064661A1 (en) | Injector head of liquid rocket engine | |
US20140000566A1 (en) | Injector nozzle coking compensation strategy | |
EP0953759A3 (en) | Injector and ignition system for rocket engines | |
CA2394694A1 (en) | Pilot nozzle of gas turbine combustor | |
JP2019060340A (ja) | 二元燃料エンジンのための噴射ノズル及び二元燃料エンジン | |
KR101922143B1 (ko) | 기화기의 시동 중에 연료 공급을 전환하기 위한 시스템과 방법 | |
US20090272096A1 (en) | Single Manifold Dual Gas Turbine Fuel System | |
JP2008280922A (ja) | 副室式エンジン | |
JP2010236386A (ja) | ロケット用噴射器 | |
US8806872B2 (en) | Procedure for igniting a turbine engine combustion chamber | |
EP3004621B1 (en) | Fuel system and method for operating a piston engine |