JP2015075104A5 - - Google Patents
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- Publication number
- JP2015075104A5 JP2015075104A5 JP2014199553A JP2014199553A JP2015075104A5 JP 2015075104 A5 JP2015075104 A5 JP 2015075104A5 JP 2014199553 A JP2014199553 A JP 2014199553A JP 2014199553 A JP2014199553 A JP 2014199553A JP 2015075104 A5 JP2015075104 A5 JP 2015075104A5
- Authority
- JP
- Japan
- Prior art keywords
- lock link
- compressor
- narrow neck
- lock
- groove
- 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.)
- Ceased
Links
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/048,724 | 2013-10-08 | ||
| US14/048,724 US9546559B2 (en) | 2013-10-08 | 2013-10-08 | Lock link mechanism for turbine vanes |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JP2015075104A JP2015075104A (ja) | 2015-04-20 |
| JP2015075104A5 true JP2015075104A5 (enExample) | 2017-11-02 |
Family
ID=52693378
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2014199553A Ceased JP2015075104A (ja) | 2013-10-08 | 2014-09-30 | タービン翼用のロックリンク機構 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US9546559B2 (enExample) |
| JP (1) | JP2015075104A (enExample) |
| CH (1) | CH708703A2 (enExample) |
| DE (1) | DE102014114246A1 (enExample) |
Families Citing this family (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2887262A1 (en) | 2012-10-23 | 2014-05-01 | General Electric Company | Unducted thrust producing system architecture |
| US11300003B2 (en) | 2012-10-23 | 2022-04-12 | General Electric Company | Unducted thrust producing system |
| US9303524B2 (en) * | 2012-10-25 | 2016-04-05 | Solar Turbines Incorporated | Variable area turbine nozzle with a position selector |
| US20140119894A1 (en) * | 2012-10-25 | 2014-05-01 | Solar Turbines Incorporated | Variable area turbine nozzle |
| EP3009604B1 (en) * | 2014-09-19 | 2018-08-08 | United Technologies Corporation | Radially fastened fixed-variable vane system |
| US11391298B2 (en) | 2015-10-07 | 2022-07-19 | General Electric Company | Engine having variable pitch outlet guide vanes |
| US10352186B2 (en) * | 2016-01-22 | 2019-07-16 | United Technologies Corporation | Variable vane stabilizer |
| DE102016215807A1 (de) * | 2016-08-23 | 2018-03-01 | MTU Aero Engines AG | Innenring für einen Leitschaufelkranz einer Strömungsmaschine |
| DE102017109952A1 (de) * | 2017-05-09 | 2018-11-15 | Rolls-Royce Deutschland Ltd & Co Kg | Rotorvorrichtung einer Strömungsmaschine |
| DE102018210601A1 (de) * | 2018-06-28 | 2020-01-02 | MTU Aero Engines AG | Segmentring zur montage in einer strömungsmaschine |
| US11492918B1 (en) | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
| US11834995B2 (en) | 2022-03-29 | 2023-12-05 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US12071896B2 (en) | 2022-03-29 | 2024-08-27 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
| US12065989B2 (en) | 2022-04-11 | 2024-08-20 | General Electric Company | Gas turbine engine with third stream |
| US11834954B2 (en) | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
| US11834992B2 (en) | 2022-04-27 | 2023-12-05 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US11680530B1 (en) | 2022-04-27 | 2023-06-20 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US12366204B2 (en) | 2022-04-27 | 2025-07-22 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
| US12060829B2 (en) | 2022-04-27 | 2024-08-13 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
| US12486817B2 (en) | 2022-08-02 | 2025-12-02 | General Electric Company | Gas turbine engine with third stream |
| US12421917B2 (en) | 2022-08-02 | 2025-09-23 | General Electric Company | Gas turbine engine with third stream |
| US12031504B2 (en) | 2022-08-02 | 2024-07-09 | General Electric Company | Gas turbine engine with third stream |
| US12410763B2 (en) | 2022-08-02 | 2025-09-09 | General Electric Company | Gas turbine engine with third stream |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE916912C (de) * | 1941-05-20 | 1954-08-19 | Versuchsanstalt Fuer Luftfahrt | Vorrichtung zur Regelung des Duesenleitkanalquerschnittes von Gsturbinen, insbesondere Abgasturbinen |
| US2755064A (en) * | 1950-08-30 | 1956-07-17 | Curtiss Wright Corp | Stator blade positioning means |
| US3004750A (en) * | 1959-02-24 | 1961-10-17 | United Aircraft Corp | Stator for compressor or turbine |
| US3112916A (en) * | 1962-04-30 | 1963-12-03 | Gen Electric | Fluid flow machine assembly |
| FR2583817B1 (fr) * | 1985-06-20 | 1988-07-29 | Snecma | Biellette de commande d'aube a calage variable de stator de compresseur de turbomachine |
| DE3913102C1 (enExample) * | 1989-04-21 | 1990-05-31 | Mtu Muenchen Gmbh | |
| FR2682157B1 (fr) * | 1991-10-02 | 1995-01-20 | Snecma | Biellette de commande d'aube et reseau de telles biellettes. |
| US5211537A (en) | 1992-03-02 | 1993-05-18 | United Technologies Corporation | Compressor vane lock |
| GB2301868B (en) * | 1995-06-05 | 1999-08-11 | Rolls Royce Plc | Improved actuator mechanism for variable angle vane arrays |
| ATE486195T1 (de) * | 2005-12-22 | 2010-11-15 | Techspace Aero | Schaufelleitring einer strömungsmaschine, strömungsmaschine mit einem solchen leitring und leitschaufel |
| ATE556197T1 (de) * | 2006-12-22 | 2012-05-15 | Techspace Aero | Winkelfixierung für leitschaufeln von turbomachinen |
| US8123471B2 (en) * | 2009-03-11 | 2012-02-28 | General Electric Company | Variable stator vane contoured button |
| EP2738356B1 (fr) * | 2012-11-29 | 2019-05-01 | Safran Aero Boosters SA | Aube de redresseur de turbomachine, redresseur de turbomachine et procédé de montage associé |
-
2013
- 2013-10-08 US US14/048,724 patent/US9546559B2/en not_active Expired - Fee Related
-
2014
- 2014-09-30 JP JP2014199553A patent/JP2015075104A/ja not_active Ceased
- 2014-09-30 DE DE201410114246 patent/DE102014114246A1/de not_active Withdrawn
- 2014-10-06 CH CH01523/14A patent/CH708703A2/de not_active Application Discontinuation
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