JP2017500487A5 - - Google Patents
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- JP2017500487A5 JP2017500487A5 JP2016541046A JP2016541046A JP2017500487A5 JP 2017500487 A5 JP2017500487 A5 JP 2017500487A5 JP 2016541046 A JP2016541046 A JP 2016541046A JP 2016541046 A JP2016541046 A JP 2016541046A JP 2017500487 A5 JP2017500487 A5 JP 2017500487A5
- Authority
- JP
- Japan
- Prior art keywords
- wing
- fin
- parts
- platform
- parts according
- 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
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- 230000003187 abdominal effect Effects 0.000 claims 2
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1362927A FR3014943B1 (fr) | 2013-12-18 | 2013-12-18 | Piece de turbomachine a surface non-axisymetrique |
| FR1362927 | 2013-12-18 | ||
| PCT/FR2014/053437 WO2015092306A1 (fr) | 2013-12-18 | 2014-12-18 | Pièce ou ensemble de pièces de turbomachine et turbomachine associée |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2017500487A JP2017500487A (ja) | 2017-01-05 |
| JP2017500487A5 true JP2017500487A5 (enExample) | 2018-02-01 |
| JP6559138B2 JP6559138B2 (ja) | 2019-08-14 |
Family
ID=50231377
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2016541046A Active JP6559138B2 (ja) | 2013-12-18 | 2014-12-18 | ターボ機械の構成要素または一群の構成要素、および関連するターボ機械 |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US10519980B2 (enExample) |
| EP (1) | EP3084134B1 (enExample) |
| JP (1) | JP6559138B2 (enExample) |
| CN (1) | CN105829653B (enExample) |
| BR (1) | BR112016013715B1 (enExample) |
| CA (1) | CA2933123C (enExample) |
| FR (1) | FR3014943B1 (enExample) |
| RU (1) | RU2666933C1 (enExample) |
| WO (1) | WO2015092306A1 (enExample) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20180017019A1 (en) * | 2016-07-15 | 2018-01-18 | General Electric Company | Turbofan engine wth a splittered rotor fan |
| FR3059735B1 (fr) * | 2016-12-05 | 2020-09-25 | Safran Aircraft Engines | Piece de turbomachine a surface non-axisymetrique |
| FR3060065B1 (fr) * | 2016-12-12 | 2020-10-23 | Safran Aircraft Engines | Ensemble de pieces de turbomachine avec une aube de soufflante a plateforme integree et turbomachine correspondante |
| FR3063119B1 (fr) * | 2017-02-21 | 2021-06-25 | Safran Aircraft Engines | Ensemble de pieces de turbomachine et turbomachine correspondante |
| FR3063118B1 (fr) * | 2017-02-21 | 2019-03-15 | Safran Aircraft Engines | Ensemble de pieces de turbomachine avec une aube de stator a plateforme integree et turbomachine correspondante |
| FR3068385B1 (fr) * | 2017-06-28 | 2021-08-06 | Safran Aircraft Engines | Ailette amovible pour un element annulaire aubage de turbomachine |
| FR3070420B1 (fr) * | 2017-08-23 | 2021-01-08 | Safran Aircraft Engines | Capot de moyeu pour structure aero-acoustique |
| DE102018200832A1 (de) | 2018-01-19 | 2019-07-25 | MTU Aero Engines AG | Rotor, insbesondere Blisk einer Gasturbine, mit aufgelöstem Rim und Verfahren zum Herstellen desselben |
| GB201806631D0 (en) * | 2018-04-24 | 2018-06-06 | Rolls Royce Plc | A combustion chamber arrangement and a gas turbine engine comprising a combustion chamber arrangement |
| BE1026276B1 (fr) * | 2018-05-14 | 2019-12-17 | Safran Aero Boosters Sa | Bosse inter-aubes de compresseur de turbomachine axiale |
| FR3081185B1 (fr) * | 2018-05-17 | 2020-09-11 | Safran Aircraft Engines | Element de stator de turbomachine |
| EP3597928A1 (en) * | 2018-07-16 | 2020-01-22 | Rolls-Royce plc | Fan unit for a turbofan engine comprising vortex-generating elements |
| US11149552B2 (en) | 2019-12-13 | 2021-10-19 | General Electric Company | Shroud for splitter and rotor airfoils of a fan for a gas turbine engine |
| FR3106614B1 (fr) * | 2020-01-23 | 2021-12-24 | Safran | Pièce ou ensemble de pièces de turbomachine |
| US20220082023A1 (en) * | 2020-09-15 | 2022-03-17 | General Electric Company | Turbine blade with non-axisymmetric forward feature |
| FR3118792A1 (fr) | 2021-01-14 | 2022-07-15 | Safran Aircraft Engines | Module pour une turbomachine d’aeronef |
| FR3126236A1 (fr) * | 2021-08-20 | 2023-02-24 | Safran | Pièce statorique d’une turbomachine comprenant une pale et une ailette définissant entre elles une surface décroissante d’amont en aval selon le sens d’écoulement des gaz. |
| FR3134415B1 (fr) * | 2022-04-11 | 2024-02-23 | Safran | Pièce statorique à ailette dans une turbomachine |
| FR3134416A1 (fr) * | 2022-04-11 | 2023-10-13 | Safran | Pièce statorique à ailette dans une turbomachine |
| US12037921B2 (en) * | 2022-08-04 | 2024-07-16 | General Electric Company | Fan for a turbine engine |
Family Cites Families (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3039736A (en) * | 1954-08-30 | 1962-06-19 | Pon Lemuel | Secondary flow control in fluid deflecting passages |
| BE631188A (enExample) | 1963-04-17 | |||
| JPS5254808A (en) * | 1975-10-31 | 1977-05-04 | Hitachi Ltd | Blade arrangement device of fluid machine |
| US4023350A (en) | 1975-11-10 | 1977-05-17 | United Technologies Corporation | Exhaust case for a turbine machine |
| JPS54151707A (en) * | 1978-05-22 | 1979-11-29 | Hitachi Ltd | Turbine blade lattice structure |
| DE3023466C2 (de) * | 1980-06-24 | 1982-11-25 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zur Verminderung von Sekundärströmungsverlusten in einem beschaufelten Strömungskanal |
| JPS6022002A (ja) * | 1983-07-18 | 1985-02-04 | Hitachi Ltd | タ−ボ機械の翼構造 |
| JPH0622002B2 (ja) | 1986-10-15 | 1994-03-23 | 株式会社タツノ・メカトロニクス | 個人情報記録用板状記憶媒体 |
| JPH04262100A (ja) * | 1991-02-18 | 1992-09-17 | Hitachi Ltd | 軸流圧縮機 |
| CN1222684C (zh) * | 1997-04-01 | 2005-10-12 | 西门子公司 | 汽轮机和汽轮机叶片 |
| EP0978632A1 (de) * | 1998-08-07 | 2000-02-09 | Asea Brown Boveri AG | Turbomaschine mit Zwischenschaufeln als Strömungsteilelemente |
| JP4441836B2 (ja) * | 2000-03-03 | 2010-03-31 | 株式会社Ｉｈｉ | 二次流れ抑制翼列 |
| RU2247839C1 (ru) * | 2003-05-26 | 2005-03-10 | Открытое акционерное общество "Невский завод" | Охлаждаемая лопатка турбины |
| FR2893268B1 (fr) * | 2005-11-15 | 2008-02-08 | Snecma Sa | Procede de realisation d'un rebord situe a l'extremite libre d'une aube, aube obtenue par ce procede et turbomachine equipee de cette aube |
| FR2907519B1 (fr) * | 2006-10-20 | 2011-12-16 | Snecma | Nageoire de plateforme de soufflante |
| DE102006057063B3 (de) | 2006-11-28 | 2008-07-31 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Stator-Stufe eines Axialverdichters einer Strömungsmaschine mit Querlamellen zur Wirkungsgradsteigerung |
| FR2927652B1 (fr) * | 2008-02-14 | 2010-03-26 | Snecma | Bord d'attaque de piece de turbomachine constitue de materiau superelastique |
| DE102008060424A1 (de) * | 2008-12-04 | 2010-06-10 | Rolls-Royce Deutschland Ltd & Co Kg | Strömungsmaschine mit Seitenwand-Grenzschicht-Barriere |
| EP2261462A1 (en) * | 2009-06-02 | 2010-12-15 | Alstom Technology Ltd | End wall structure for a turbine stage |
-
2013
- 2013-12-18 FR FR1362927A patent/FR3014943B1/fr active Active
-
2014
- 2014-12-18 CN CN201480070059.6A patent/CN105829653B/zh active Active
- 2014-12-18 US US15/105,359 patent/US10519980B2/en active Active
- 2014-12-18 JP JP2016541046A patent/JP6559138B2/ja active Active
- 2014-12-18 CA CA2933123A patent/CA2933123C/fr active Active
- 2014-12-18 WO PCT/FR2014/053437 patent/WO2015092306A1/fr not_active Ceased
- 2014-12-18 BR BR112016013715-9A patent/BR112016013715B1/pt active IP Right Grant
- 2014-12-18 RU RU2016128925A patent/RU2666933C1/ru active
- 2014-12-18 EP EP14830831.5A patent/EP3084134B1/fr active Active
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