JP2015520821A5 - - Google Patents
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- Publication number
- JP2015520821A5 JP2015520821A5 JP2015507577A JP2015507577A JP2015520821A5 JP 2015520821 A5 JP2015520821 A5 JP 2015520821A5 JP 2015507577 A JP2015507577 A JP 2015507577A JP 2015507577 A JP2015507577 A JP 2015507577A JP 2015520821 A5 JP2015520821 A5 JP 2015520821A5
- Authority
- JP
- Japan
- Prior art keywords
- motor
- gas
- shaft
- positive displacement
- emergency start
- Prior art date
- Legal status (The legal status 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 status listed.)
- Granted
Links
- 239000007789 gas Substances 0.000 claims description 46
- 238000006073 displacement reaction Methods 0.000 claims description 35
- 230000008878 coupling Effects 0.000 claims description 10
- 238000010168 coupling process Methods 0.000 claims description 10
- 238000005859 coupling reaction Methods 0.000 claims description 10
- 238000000034 method Methods 0.000 claims description 10
- 239000007858 starting material Substances 0.000 claims description 8
- 238000002485 combustion reaction Methods 0.000 claims description 7
- 238000009434 installation Methods 0.000 claims description 5
- 230000004913 activation Effects 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 4
- 238000007906 compression Methods 0.000 claims description 4
- 239000012530 fluid Substances 0.000 claims description 4
- 238000010248 power generation Methods 0.000 claims description 3
- 230000001141 propulsive effect Effects 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000004891 communication Methods 0.000 claims description 2
- 230000033001 locomotion Effects 0.000 claims 2
- 241000885593 Geisha Species 0.000 claims 1
- 238000002347 injection Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 239000002184 metal Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 239000000567 combustion gas Substances 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- WJYVXARRCUTRBW-HNNXBMFYSA-N (3s)-3-[[6-[[[3-(acetylsulfamoyl)phenyl]sulfonylamino]methyl]pyridine-3-carbonyl]amino]-4-oxobutanoic acid Chemical compound CC(=O)NS(=O)(=O)C1=CC=CC(S(=O)(=O)NCC=2N=CC(=CC=2)C(=O)N[C@@H](CC(O)=O)C=O)=C1 WJYVXARRCUTRBW-HNNXBMFYSA-N 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1253938A FR2990004B1 (fr) | 2012-04-27 | 2012-04-27 | Procede et systeme de demarrage d'urgence d'architecture generatrice d'energie |
| FR1253938 | 2012-04-27 | ||
| PCT/FR2013/050863 WO2013160590A1 (fr) | 2012-04-27 | 2013-04-18 | Procédé et système de démarrage d'urgence d'architecture génératrice d'énergie |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2015520821A JP2015520821A (ja) | 2015-07-23 |
| JP2015520821A5 true JP2015520821A5 (https=) | 2017-09-28 |
| JP6208216B2 JP6208216B2 (ja) | 2017-10-04 |
Family
ID=46826641
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2015507577A Expired - Fee Related JP6208216B2 (ja) | 2012-04-27 | 2013-04-18 | エネルギー発電設備の緊急起動の方法およびシステム |
Country Status (12)
| Country | Link |
|---|---|
| US (1) | US10072580B2 (https=) |
| EP (1) | EP2841742B1 (https=) |
| JP (1) | JP6208216B2 (https=) |
| KR (1) | KR102049130B1 (https=) |
| CN (1) | CN104246181B (https=) |
| CA (1) | CA2869361C (https=) |
| ES (1) | ES2572093T3 (https=) |
| FR (1) | FR2990004B1 (https=) |
| IN (1) | IN2014DN08865A (https=) |
| PL (1) | PL2841742T3 (https=) |
| RU (1) | RU2621190C2 (https=) |
| WO (1) | WO2013160590A1 (https=) |
Families Citing this family (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3017417B1 (fr) * | 2014-02-10 | 2018-10-26 | Safran Helicopter Engines | Dispositif pyrotechnique pour l'entrainement d'une machine tournante |
| FR3019524B1 (fr) * | 2014-04-03 | 2017-12-08 | Turbomeca | Chaine motrice pour helicoptere incorporant un module moteur pyrotechnique d'assistance et helicoptere la comportant |
| FR3019588B1 (fr) | 2014-04-08 | 2019-06-14 | Safran Helicopter Engines | Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif et procede correspondant |
| FR3027346B1 (fr) * | 2014-10-20 | 2019-08-09 | Safran Helicopter Engines | Pack amovible de reactivation d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel pack et helicoptere correspondant |
| US10054008B2 (en) * | 2015-02-09 | 2018-08-21 | United Technologies Corporation | Turbomachine accessory gearbox bracket |
| FR3033882B1 (fr) * | 2015-03-16 | 2017-04-07 | Herakles | Generateur de gaz |
| US10539079B2 (en) | 2016-02-12 | 2020-01-21 | United Technologies Corporation | Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters |
| US10443505B2 (en) | 2016-02-12 | 2019-10-15 | United Technologies Corporation | Bowed rotor start mitigation in a gas turbine engine |
| US10443507B2 (en) | 2016-02-12 | 2019-10-15 | United Technologies Corporation | Gas turbine engine bowed rotor avoidance system |
| US9664070B1 (en) | 2016-02-12 | 2017-05-30 | United Technologies Corporation | Bowed rotor prevention system |
| US10125636B2 (en) | 2016-02-12 | 2018-11-13 | United Technologies Corporation | Bowed rotor prevention system using waste heat |
| US10040577B2 (en) | 2016-02-12 | 2018-08-07 | United Technologies Corporation | Modified start sequence of a gas turbine engine |
| US10436064B2 (en) | 2016-02-12 | 2019-10-08 | United Technologies Corporation | Bowed rotor start response damping system |
| US10125691B2 (en) | 2016-02-12 | 2018-11-13 | United Technologies Corporation | Bowed rotor start using a variable position starter valve |
| US10508601B2 (en) | 2016-02-12 | 2019-12-17 | United Technologies Corporation | Auxiliary drive bowed rotor prevention system for a gas turbine engine |
| US10508567B2 (en) | 2016-02-12 | 2019-12-17 | United Technologies Corporation | Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory |
| US10174678B2 (en) | 2016-02-12 | 2019-01-08 | United Technologies Corporation | Bowed rotor start using direct temperature measurement |
| EP3211184B1 (en) | 2016-02-29 | 2021-05-05 | Raytheon Technologies Corporation | Bowed rotor prevention system and associated method of bowed rotor prevention |
| CN107404147A (zh) * | 2016-05-20 | 2017-11-28 | 北京汽车股份有限公司 | 汽车及其应急启动发电装置 |
| US10787933B2 (en) | 2016-06-20 | 2020-09-29 | Raytheon Technologies Corporation | Low-power bowed rotor prevention and monitoring system |
| US10358936B2 (en) | 2016-07-05 | 2019-07-23 | United Technologies Corporation | Bowed rotor sensor system |
| US10384791B2 (en) | 2016-07-21 | 2019-08-20 | United Technologies Corporation | Cross engine coordination during gas turbine engine motoring |
| US10618666B2 (en) | 2016-07-21 | 2020-04-14 | United Technologies Corporation | Pre-start motoring synchronization for multiple engines |
| US10221774B2 (en) | 2016-07-21 | 2019-03-05 | United Technologies Corporation | Speed control during motoring of a gas turbine engine |
| EP3273006B1 (en) | 2016-07-21 | 2019-07-03 | United Technologies Corporation | Alternating starter use during multi-engine motoring |
| EP3273016B1 (en) | 2016-07-21 | 2020-04-01 | United Technologies Corporation | Multi-engine coordination during gas turbine engine motoring |
| US10787968B2 (en) | 2016-09-30 | 2020-09-29 | Raytheon Technologies Corporation | Gas turbine engine motoring with starter air valve manual override |
| US10443543B2 (en) | 2016-11-04 | 2019-10-15 | United Technologies Corporation | High compressor build clearance reduction |
| US10823079B2 (en) | 2016-11-29 | 2020-11-03 | Raytheon Technologies Corporation | Metered orifice for motoring of a gas turbine engine |
| CN110291282B (zh) * | 2016-12-15 | 2021-12-31 | 通用电气航空系统有限责任公司 | 具有分离器的空气涡轮启动器 |
| US10823080B2 (en) | 2017-05-31 | 2020-11-03 | General Electric Company | Dual accessory gearbox |
| FR3082225B1 (fr) | 2018-06-07 | 2020-06-05 | Safran Helicopter Engines | Systeme propulsif asymetrique a recuperation de chaleur |
| US11512645B2 (en) * | 2020-03-06 | 2022-11-29 | Goodrich Corporation | Solid-propellant gas generator assemblies and methods |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1104252A (fr) * | 1954-05-06 | 1955-11-17 | Snecma | Démarreur amovible destiné notamment aux moteurs d'aviation |
| US2942415A (en) * | 1954-11-29 | 1960-06-28 | Bayard Gaston | System for feeding gases into a starting turbine |
| FR1126010A (fr) * | 1955-05-09 | 1956-11-13 | Air Equipement | Perfectionnements aux démarreurs à turbine |
| FR1303228A (fr) * | 1961-08-29 | 1962-09-07 | Sundstrand A G | Démarreur pour moteurs |
| FR1334270A (fr) * | 1962-09-25 | 1963-08-02 | Cessna Aircraft Co | Moteur actionné par un fluide sous pression |
| US3633360A (en) * | 1970-01-20 | 1972-01-11 | Talley Industries | Boost starter system |
| FR2475127A1 (fr) * | 1980-02-06 | 1981-08-07 | Snecma | Generateur de gaz a variation de volume |
| US6931856B2 (en) * | 2003-09-12 | 2005-08-23 | Mes International, Inc. | Multi-spool turbogenerator system and control method |
| RU2275957C1 (ru) * | 2004-09-13 | 2006-05-10 | Российская Федерация, от имени которой выступает Государственный заказчик - Федеральное агентство по атомной энергии | Устройство для генерирования газа |
| FR2897895A1 (fr) * | 2006-02-27 | 2007-08-31 | Hispano Suiza Sa | Integration d'un demarreur/generateur dans une boite de transmission d'une turbine a gaz |
| FR2914697B1 (fr) * | 2007-04-06 | 2012-11-30 | Turbomeca | Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration |
| US8148834B2 (en) * | 2009-05-19 | 2012-04-03 | General Electric Company | Aircraft engine starting/generating system and method of control |
-
2012
- 2012-04-27 FR FR1253938A patent/FR2990004B1/fr not_active Expired - Fee Related
-
2013
- 2013-04-18 PL PL13722505T patent/PL2841742T3/pl unknown
- 2013-04-18 IN IN8865DEN2014 patent/IN2014DN08865A/en unknown
- 2013-04-18 RU RU2014142446A patent/RU2621190C2/ru active
- 2013-04-18 KR KR1020147028294A patent/KR102049130B1/ko not_active Expired - Fee Related
- 2013-04-18 US US14/396,235 patent/US10072580B2/en active Active
- 2013-04-18 CA CA2869361A patent/CA2869361C/fr not_active Expired - Fee Related
- 2013-04-18 JP JP2015507577A patent/JP6208216B2/ja not_active Expired - Fee Related
- 2013-04-18 WO PCT/FR2013/050863 patent/WO2013160590A1/fr not_active Ceased
- 2013-04-18 CN CN201380021227.8A patent/CN104246181B/zh not_active Expired - Fee Related
- 2013-04-18 ES ES13722505T patent/ES2572093T3/es active Active
- 2013-04-18 EP EP13722505.8A patent/EP2841742B1/fr active Active
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