JP2018530707A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2018530707A5 JP2018530707A5 JP2018532830A JP2018532830A JP2018530707A5 JP 2018530707 A5 JP2018530707 A5 JP 2018530707A5 JP 2018532830 A JP2018532830 A JP 2018532830A JP 2018532830 A JP2018532830 A JP 2018532830A JP 2018530707 A5 JP2018530707 A5 JP 2018530707A5
- Authority
- JP
- Japan
- Prior art keywords
- casing
- shield
- manifold
- opening
- turbine
- 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
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 claims 2
- 229910052786 argon Inorganic materials 0.000 claims 1
- 238000013022 venting Methods 0.000 claims 1
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1558619A FR3041037B1 (fr) | 2015-09-15 | 2015-09-15 | Dispositif de ventilation d'un carter de turbine d'une turbomachine |
| FR1558619 | 2015-09-15 | ||
| PCT/FR2016/052292 WO2017046499A1 (fr) | 2015-09-15 | 2016-09-12 | Dispositif de ventilation d'un carter de turbine d'une turbomachine |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2018530707A JP2018530707A (ja) | 2018-10-18 |
| JP2018530707A5 true JP2018530707A5 (cg-RX-API-DMAC7.html) | 2019-09-19 |
| JP6864690B2 JP6864690B2 (ja) | 2021-04-28 |
Family
ID=54329831
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2018532830A Active JP6864690B2 (ja) | 2015-09-15 | 2016-09-12 | ターボマシンのタービンケーシングの通気のための装置 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US10677093B2 (cg-RX-API-DMAC7.html) |
| EP (1) | EP3350417B2 (cg-RX-API-DMAC7.html) |
| JP (1) | JP6864690B2 (cg-RX-API-DMAC7.html) |
| CN (1) | CN108026780B (cg-RX-API-DMAC7.html) |
| BR (1) | BR112018005031B1 (cg-RX-API-DMAC7.html) |
| CA (1) | CA2997939C (cg-RX-API-DMAC7.html) |
| FR (1) | FR3041037B1 (cg-RX-API-DMAC7.html) |
| RU (1) | RU2691241C1 (cg-RX-API-DMAC7.html) |
| WO (1) | WO2017046499A1 (cg-RX-API-DMAC7.html) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3068732B1 (fr) * | 2017-07-06 | 2020-06-26 | Safran Aircraft Engines | Dispositif de refroidissement |
| FR3081927B1 (fr) | 2018-05-30 | 2020-11-20 | Safran Aircraft Engines | Dispositif de refroidissement d'un carter de turbomachine |
Family Cites Families (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| SU452593A1 (ru) * | 1973-09-13 | 1974-12-05 | Всесоюзный Научно-Исследовательский И Проектный Институт По Очистке Технологических Газов,Сточных Вод И Использованию Вторичных Энергоресурсов Предприятий Черной Металлургии | Фурма доменной печи |
| US4525998A (en) * | 1982-08-02 | 1985-07-02 | United Technologies Corporation | Clearance control for gas turbine engine |
| US4826397A (en) * | 1988-06-29 | 1989-05-02 | United Technologies Corporation | Stator assembly for a gas turbine engine |
| US5100291A (en) * | 1990-03-28 | 1992-03-31 | General Electric Company | Impingement manifold |
| US5399066A (en) * | 1993-09-30 | 1995-03-21 | General Electric Company | Integral clearance control impingement manifold and environmental shield |
| FR2750451B1 (fr) * | 1996-06-27 | 1998-08-07 | Snecma | Dispositif de soufflage de gaz de reglage de jeux dans une turbomachine |
| FR2766232B1 (fr) * | 1997-07-18 | 1999-08-20 | Snecma | Dispositif de refroidissement ou d'echauffement d'un carter circulaire |
| FR2829176B1 (fr) * | 2001-08-30 | 2005-06-24 | Snecma Moteurs | Carter de stator de turbomachine |
| US8979477B2 (en) * | 2011-03-09 | 2015-03-17 | General Electric Company | System for cooling and purging exhaust section of gas turbine engine |
| JP5222384B2 (ja) * | 2011-09-09 | 2013-06-26 | 三菱重工業株式会社 | ガスタービン |
| US9316111B2 (en) * | 2011-12-15 | 2016-04-19 | Pratt & Whitney Canada Corp. | Active turbine tip clearance control system |
| ITTO20120519A1 (it) * | 2012-06-14 | 2013-12-15 | Avio Spa | Turbina a gas per motori aeronautici |
| US9341074B2 (en) * | 2012-07-25 | 2016-05-17 | General Electric Company | Active clearance control manifold system |
| US9068474B2 (en) * | 2013-01-25 | 2015-06-30 | GM Global Technology Operations LLC | Turbine housing |
| US20170114667A1 (en) * | 2015-10-23 | 2017-04-27 | General Electric Company | Active clearance control with integral double wall heat shielding |
-
2015
- 2015-09-15 FR FR1558619A patent/FR3041037B1/fr active Active
-
2016
- 2016-09-12 JP JP2018532830A patent/JP6864690B2/ja active Active
- 2016-09-12 EP EP16774530.6A patent/EP3350417B2/fr active Active
- 2016-09-12 CA CA2997939A patent/CA2997939C/fr active Active
- 2016-09-12 US US15/760,219 patent/US10677093B2/en active Active
- 2016-09-12 RU RU2018113308A patent/RU2691241C1/ru active
- 2016-09-12 CN CN201680052926.2A patent/CN108026780B/zh active Active
- 2016-09-12 BR BR112018005031-8A patent/BR112018005031B1/pt active IP Right Grant
- 2016-09-12 WO PCT/FR2016/052292 patent/WO2017046499A1/fr not_active Ceased