JP2004301123A5 - - Google Patents
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- Publication number
- JP2004301123A5 JP2004301123A5 JP2004090861A JP2004090861A JP2004301123A5 JP 2004301123 A5 JP2004301123 A5 JP 2004301123A5 JP 2004090861 A JP2004090861 A JP 2004090861A JP 2004090861 A JP2004090861 A JP 2004090861A JP 2004301123 A5 JP2004301123 A5 JP 2004301123A5
- Authority
- JP
- Japan
- 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
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/402,566 US6887043B2 (en) | 2003-03-28 | 2003-03-28 | Methods and apparatus for assembling gas turbine engines |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2004301123A JP2004301123A (ja) | 2004-10-28 |
| JP2004301123A5 true JP2004301123A5 (enExample) | 2007-05-10 |
| JP4064370B2 JP4064370B2 (ja) | 2008-03-19 |
Family
ID=32825055
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004090861A Expired - Fee Related JP4064370B2 (ja) | 2003-03-28 | 2004-03-26 | ガスタービンエンジンを組立てるための方法及び装置 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US6887043B2 (enExample) |
| EP (1) | EP1462664A3 (enExample) |
| JP (1) | JP4064370B2 (enExample) |
| CA (1) | CA2460662C (enExample) |
Families Citing this family (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2869374B1 (fr) * | 2004-04-23 | 2009-01-30 | Snecma Moteurs Sa | Systeme de fixation de pieces par des goujons a collerettes |
| US20080075590A1 (en) * | 2006-09-27 | 2008-03-27 | Thomas Ory Moniz | Gas turbine engine assembly and method of assembling same |
| FR2922588B1 (fr) * | 2007-10-22 | 2013-11-01 | Snecma | Disque ou tambour de rotor d'une turbomachine |
| US20100047077A1 (en) * | 2007-12-28 | 2010-02-25 | General Electric Company | Ferry Flight Engine Fairing Kit |
| US20100043228A1 (en) * | 2007-12-28 | 2010-02-25 | James Lloyd Daniels | Method of Preparing an Engine for Ferry Flight |
| FR2933887B1 (fr) * | 2008-07-18 | 2010-09-17 | Snecma | Procede de reparation ou de reprise d'un disque de turbomachine et disque de turbomachine repare ou repris |
| FR2943726B1 (fr) * | 2009-03-31 | 2014-04-25 | Snecma | Capot d'entree tournant pour turbomachine, comprenant une extremite avant excentree |
| GB2474449B (en) * | 2009-10-14 | 2012-02-22 | Rolls Royce Plc | Annulus filler element for a rotor of a turbomachine |
| GB201119906D0 (en) * | 2011-11-18 | 2011-12-28 | Rolls Royce Plc | Stud retention |
| FR2986582B1 (fr) * | 2012-02-06 | 2014-03-14 | Snecma | Carter de soufflante pour moteur a turbine a gaz munie d'une bride pour la fixation d'equipements |
| US11073044B2 (en) * | 2013-01-21 | 2021-07-27 | Raytheon Technologies Corporation | Adjustable floating oil channel for gas turbine engine gear drive |
| US10072509B2 (en) | 2013-03-06 | 2018-09-11 | United Technologies Corporation | Gas turbine engine nose cone attachment |
| US10465519B2 (en) * | 2013-10-17 | 2019-11-05 | Pratt & Whitney Canada Corp. | Fastening system for rotor hubs |
| DE102014222060A1 (de) * | 2014-10-29 | 2016-05-04 | Siemens Aktiengesellschaft | Schraubenbolzen, Gehäuse für eine Turbine, Turbine sowie Verfahren zur Montage eines Gehäuses einer Turbine |
| US9879565B2 (en) * | 2015-01-20 | 2018-01-30 | United Technologies Corporation | Enclosed jacking insert |
| DE102016213813A1 (de) * | 2016-07-27 | 2018-02-01 | MTU Aero Engines AG | Verkleidungselement einer Strömungsmaschine und entsprechende Verbindungsanordnung |
| US10583913B2 (en) * | 2017-03-14 | 2020-03-10 | General Electric Company | Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole |
| US10670037B2 (en) * | 2017-11-21 | 2020-06-02 | General Electric Company | Turbofan engine's fan blade and setting method thereof |
| FR3140648B1 (fr) * | 2022-10-05 | 2025-10-10 | Safran Aircraft Engines | Procédé de fixation d’au moins deux brides de disques de turbine |
| FR3144849B1 (fr) * | 2023-01-05 | 2025-07-04 | Safran Aircraft Engines | Ensemble rotorique de soufflante pour turbomachine |
| FR3144848B1 (fr) * | 2023-01-05 | 2025-06-06 | Safran Aircraft Engines | Ensemble rotorique de soufflante pour turbomachine |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE507205A (enExample) * | 1950-12-08 | |||
| US3446429A (en) * | 1966-12-08 | 1969-05-27 | Tokyo Shibaura Electric Co | Readily disassembled electric fan |
| JPS5416063A (en) * | 1977-06-09 | 1979-02-06 | Illinois Tool Works | Insertable bolt and driving attach ment therefore |
| US5006025A (en) * | 1989-12-13 | 1991-04-09 | Avibank Mfg., Inc. | Self-locking nut |
| US5182906A (en) * | 1990-10-22 | 1993-02-02 | General Electric Company | Hybrid spinner nose configuration in a gas turbine engine having a bypass duct |
| US5211541A (en) * | 1991-12-23 | 1993-05-18 | General Electric Company | Turbine support assembly including turbine heat shield and bolt retainer assembly |
| USRE35358E (en) * | 1992-05-29 | 1996-10-22 | Belser; Jess L. | Fastening bolt assembly with anti-rotation device and providing both axial and radial holding forces |
| US5163796A (en) * | 1992-05-29 | 1992-11-17 | Belser Jess L | Fastening bolt assembly providing both axial and radial holding forces |
| US5281096A (en) * | 1992-09-10 | 1994-01-25 | General Electric Company | Fan assembly having lightweight platforms |
| US5232323A (en) * | 1992-09-28 | 1993-08-03 | General Electric Company | Removable threaded fastener with locking plate |
| FR2710715B1 (fr) * | 1993-09-29 | 1996-09-20 | Marc Jean Pierre | Verrou auto-bloquant pour canalisations. |
| FR2746456B1 (fr) * | 1996-03-21 | 1998-04-30 | Snecma | Dispositif de retenue du pied des aubes d'une soufflante |
| SE509758C2 (sv) * | 1996-05-24 | 1999-03-08 | Volvo Lastvagnar Ab | Anordning för rotationslåsning av ett roterbart fästelement i ett konstruktionselement samt förfarande för framställning av ett sådant |
| GB9828812D0 (en) * | 1998-12-29 | 1999-02-17 | Rolls Royce Plc | Gas turbine nose cone assembly |
| US6217283B1 (en) * | 1999-04-20 | 2001-04-17 | General Electric Company | Composite fan platform |
| US6358014B1 (en) * | 2000-03-24 | 2002-03-19 | General Electric Company | Composite spinner and method of making the same |
| US6520742B1 (en) * | 2000-11-27 | 2003-02-18 | General Electric Company | Circular arc multi-bore fan disk |
| US6416280B1 (en) * | 2000-11-27 | 2002-07-09 | General Electric Company | One piece spinner |
| US6447250B1 (en) * | 2000-11-27 | 2002-09-10 | General Electric Company | Non-integral fan platform |
| US6481971B1 (en) * | 2000-11-27 | 2002-11-19 | General Electric Company | Blade spacer |
| US6457942B1 (en) | 2000-11-27 | 2002-10-01 | General Electric Company | Fan blade retainer |
| US6557942B1 (en) * | 2001-11-20 | 2003-05-06 | First & Best Furniture Co., Ltd. | Combination lounger with easy assembly and detaching structure |
-
2003
- 2003-03-28 US US10/402,566 patent/US6887043B2/en not_active Expired - Lifetime
-
2004
- 2004-03-11 CA CA2460662A patent/CA2460662C/en not_active Expired - Fee Related
- 2004-03-26 JP JP2004090861A patent/JP4064370B2/ja not_active Expired - Fee Related
- 2004-03-26 EP EP04251806A patent/EP1462664A3/en not_active Withdrawn