JP2018510086A5 - - Google Patents
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- Publication number
- JP2018510086A5 JP2018510086A5 JP2017541790A JP2017541790A JP2018510086A5 JP 2018510086 A5 JP2018510086 A5 JP 2018510086A5 JP 2017541790 A JP2017541790 A JP 2017541790A JP 2017541790 A JP2017541790 A JP 2017541790A JP 2018510086 A5 JP2018510086 A5 JP 2018510086A5
- Authority
- JP
- Japan
- Prior art keywords
- turbine engine
- point
- downstream
- upstream
- vane
- 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.)
- Pending
Links
- 238000011144 upstream manufacturing Methods 0.000 claims description 16
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1551011 | 2015-02-09 | ||
| FR1551011A FR3032480B1 (fr) | 2015-02-09 | 2015-02-09 | Ensemble de redressement d'air a performances aerodynamiques ameliorees |
| PCT/FR2016/050275 WO2016128665A1 (fr) | 2015-02-09 | 2016-02-09 | Ensemble de redressement d'air de turbomachine à performances aerodynamiques améliorées |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2018510086A JP2018510086A (ja) | 2018-04-12 |
| JP2018510086A5 true JP2018510086A5 (enExample) | 2019-02-21 |
Family
ID=53298504
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2017541790A Pending JP2018510086A (ja) | 2015-02-09 | 2016-02-09 | 改良された空力性能を備えたタービンエンジン空気ガイドアセンブリ |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US11149565B2 (enExample) |
| EP (1) | EP3256697B1 (enExample) |
| JP (1) | JP2018510086A (enExample) |
| CN (1) | CN107250486B (enExample) |
| BR (1) | BR112017016971A2 (enExample) |
| CA (1) | CA2975947A1 (enExample) |
| FR (1) | FR3032480B1 (enExample) |
| RU (1) | RU2715131C2 (enExample) |
| WO (1) | WO2016128665A1 (enExample) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3059735B1 (fr) | 2016-12-05 | 2020-09-25 | Safran Aircraft Engines | Piece de turbomachine a surface non-axisymetrique |
| GB201703422D0 (en) * | 2017-03-03 | 2017-04-19 | Rolls Royce Plc | Gas turbine engine vanes |
| FR3070440B1 (fr) * | 2017-08-30 | 2021-07-30 | Safran Aircraft Engines | Aube de redressement et arbre structural raccordes dans une veine primaire |
| US20190107046A1 (en) * | 2017-10-05 | 2019-04-11 | General Electric Company | Turbine engine with struts |
| FR3073891B1 (fr) | 2017-11-22 | 2019-11-22 | Safran Aircraft Engines | Mat d'un ensemble propulsif |
| CN108425887A (zh) * | 2018-04-12 | 2018-08-21 | 深圳福世达动力科技有限公司 | 超宽弦三角函数波形叶片 |
| FR3083260B1 (fr) * | 2018-06-28 | 2020-06-19 | Safran Aircraft Engines | Module d’un moteur d’aeronef a double flux dont un bras integre une aube de stator |
| FR3089550B1 (fr) * | 2018-12-11 | 2021-01-22 | Safran Aircraft Engines | Aube de turbomachine a loi d’epaisseur maximale a forte marge au flottement |
| FR3092868B1 (fr) * | 2019-02-19 | 2021-01-22 | Safran Aircraft Engines | Roue de stator d’une turbomachine comprenant des aubes présentant des cordes différentes |
| FR3093756B1 (fr) * | 2019-03-15 | 2021-02-19 | Safran Aircraft Engines | redresseur de flux secondaire a Tuyère intégréE |
| BE1027876B1 (fr) | 2019-12-18 | 2021-07-26 | Safran Aero Boosters Sa | Module pour turbomachine |
| FR3108937B1 (fr) * | 2020-04-01 | 2023-03-24 | Safran Aircraft Engines | Carter intermédiaire de turbomachine |
| CN113123834B (zh) * | 2021-06-17 | 2021-09-28 | 中国航发上海商用航空发动机制造有限责任公司 | 发动机的叶片组件及发动机 |
| US11873738B2 (en) * | 2021-12-23 | 2024-01-16 | General Electric Company | Integrated stator-fan frame assembly |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4785625A (en) * | 1987-04-03 | 1988-11-22 | United Technologies Corporation | Ducted fan gas turbine power plant mounting |
| US5123242A (en) * | 1990-07-30 | 1992-06-23 | General Electric Company | Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
| US5203163A (en) * | 1990-08-01 | 1993-04-20 | General Electric Company | Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air |
| FR2734319B1 (fr) * | 1995-05-15 | 1997-07-18 | Aerospatiale | Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef |
| US6561761B1 (en) * | 2000-02-18 | 2003-05-13 | General Electric Company | Fluted compressor flowpath |
| FR2896481B1 (fr) * | 2006-01-23 | 2009-12-04 | Aircelle Sa | Systeme de fixation pour element constitutif d'une nacelle de turboreacteur |
| US20080028763A1 (en) * | 2006-08-03 | 2008-02-07 | United Technologies Corporation | Thermal management system with thrust recovery for a gas turbine engine fan nacelle assembly |
| US8221071B2 (en) | 2008-09-30 | 2012-07-17 | General Electric Company | Integrated guide vane assembly |
| DE102010002394A1 (de) * | 2010-02-26 | 2011-09-01 | Rolls-Royce Deutschland Ltd & Co Kg | Nebenstromkanal eines Turbofantriebwerks |
| DE102010014900A1 (de) * | 2010-04-14 | 2011-10-20 | Rolls-Royce Deutschland Ltd & Co Kg | Nebenstromkanal eines Turbofantriebwerkes |
| JP6012222B2 (ja) | 2012-03-30 | 2016-10-25 | 三菱重工業株式会社 | 静翼セグメント、これを備える軸流流体機械及びその静翼連結方法 |
| US9068460B2 (en) * | 2012-03-30 | 2015-06-30 | United Technologies Corporation | Integrated inlet vane and strut |
| FR3004749B1 (fr) * | 2013-04-22 | 2015-05-08 | Snecma | Roue de stator, roue d'aubes de redresseur, turbomachine equipee d'une telle roue et procede de compensation de la distorsion dans une telle roue |
| GB201408415D0 (en) | 2014-05-13 | 2014-06-25 | Rolls Royce Plc | Bifurcation fairing |
-
2015
- 2015-02-09 FR FR1551011A patent/FR3032480B1/fr active Active
-
2016
- 2016-02-09 US US15/549,584 patent/US11149565B2/en active Active
- 2016-02-09 CN CN201680009397.8A patent/CN107250486B/zh active Active
- 2016-02-09 EP EP16705981.5A patent/EP3256697B1/fr active Active
- 2016-02-09 BR BR112017016971-1A patent/BR112017016971A2/pt not_active IP Right Cessation
- 2016-02-09 WO PCT/FR2016/050275 patent/WO2016128665A1/fr not_active Ceased
- 2016-02-09 JP JP2017541790A patent/JP2018510086A/ja active Pending
- 2016-02-09 CA CA2975947A patent/CA2975947A1/fr not_active Abandoned
- 2016-02-09 RU RU2017131460A patent/RU2715131C2/ru active
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