JP2004353667A5 - - Google Patents
Download PDFInfo
- Publication number
- JP2004353667A5 JP2004353667A5 JP2004148940A JP2004148940A JP2004353667A5 JP 2004353667 A5 JP2004353667 A5 JP 2004353667A5 JP 2004148940 A JP2004148940 A JP 2004148940A JP 2004148940 A JP2004148940 A JP 2004148940A JP 2004353667 A5 JP2004353667 A5 JP 2004353667A5
- Authority
- JP
- Japan
- Prior art keywords
- gasket
- turbomachine
- upstream
- annular
- casing
- 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
- 238000011144 upstream manufacturing Methods 0.000 claims 11
- 238000009413 insulation Methods 0.000 claims 4
- 238000002485 combustion reaction Methods 0.000 claims 2
- 238000005219 brazing Methods 0.000 claims 1
- 238000007789 sealing Methods 0.000 claims 1
- 238000003466 welding Methods 0.000 claims 1
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0306390A FR2855559B1 (fr) | 2003-05-27 | 2003-05-27 | Systeme d'etancheite du flux secondaire a l'entree d'une tuyere d'une turbomachine avec chambre de post-combustion |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2004353667A JP2004353667A (ja) | 2004-12-16 |
| JP2004353667A5 true JP2004353667A5 (enExample) | 2005-09-02 |
| JP4146389B2 JP4146389B2 (ja) | 2008-09-10 |
Family
ID=32982397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004148940A Expired - Lifetime JP4146389B2 (ja) | 2003-05-27 | 2004-05-19 | 後燃焼室を有するターボマシンのノズルへの入口で、二次流をシーリングするためのシステム |
Country Status (18)
| Country | Link |
|---|---|
| US (1) | US6966189B2 (enExample) |
| EP (1) | EP1482127B1 (enExample) |
| JP (1) | JP4146389B2 (enExample) |
| KR (1) | KR20040102334A (enExample) |
| CN (1) | CN100346066C (enExample) |
| AT (1) | ATE333570T1 (enExample) |
| AU (1) | AU2004202177A1 (enExample) |
| BR (1) | BRPI0401807A (enExample) |
| CA (1) | CA2469853A1 (enExample) |
| DE (1) | DE602004001546T2 (enExample) |
| ES (1) | ES2270305T3 (enExample) |
| FR (1) | FR2855559B1 (enExample) |
| IL (1) | IL162142A (enExample) |
| NZ (1) | NZ533014A (enExample) |
| PL (1) | PL1482127T3 (enExample) |
| RU (1) | RU2342551C2 (enExample) |
| UA (1) | UA81234C2 (enExample) |
| ZA (1) | ZA200403929B (enExample) |
Families Citing this family (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6799739B1 (en) | 2003-11-24 | 2004-10-05 | The Boeing Company | Aircraft control surface drive system and associated methods |
| US7611099B2 (en) * | 2005-09-07 | 2009-11-03 | The Boeing Company | Seal assemblies for use with drooped spoilers and other control surfaces on aircraft |
| US7624567B2 (en) * | 2005-09-20 | 2009-12-01 | United Technologies Corporation | Convergent divergent nozzle with interlocking divergent flaps |
| FR2903151B1 (fr) * | 2006-06-29 | 2011-10-28 | Snecma | Dispositif de ventilation d'un carter d'echappement dans une turbomachine |
| US8069648B2 (en) | 2008-07-03 | 2011-12-06 | United Technologies Corporation | Impingement cooling for turbofan exhaust assembly |
| GB0908370D0 (en) * | 2009-05-15 | 2009-06-24 | Airbus Uk Ltd | A hinge sealing element and an assembly including said element |
| US9932845B2 (en) * | 2011-06-30 | 2018-04-03 | United Technologies Corporation | Impingement cooled nozzle liner |
| US9341120B2 (en) * | 2012-02-10 | 2016-05-17 | United Technologies Corporation | Channeled spring seal for sealing an air gap between moving plates |
| RU2516751C1 (ru) * | 2013-04-11 | 2014-05-20 | Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" | Поворотное осесимметричное сопло турбореактивного двигателя |
| FR3009029B1 (fr) * | 2013-07-26 | 2018-03-23 | Astrium Sas | Tuyere d'ejection de gaz de combustion d'un moteur fusee pourvue d'un dispositif d'etancheite entre une partie fixe et une partie mobile de la tuyere |
| FR3047768B1 (fr) * | 2016-02-17 | 2019-02-01 | Safran Power Units | Dispositif de liaison et d'etancheite entre deux modules d'un conduit d'echappement d'une turbomachine |
| RU2656172C1 (ru) * | 2017-04-20 | 2018-05-31 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Устройство для сочленения наружной поверхности поворотного реактивного сопла двигателя и мотогондолы самолёта |
| RU2647018C1 (ru) * | 2017-04-26 | 2018-03-13 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Устройство для сочленения наружной поверхности поворотного реактивного сопла турбореактивного двигателя и мотогондолы самолета |
| US10513939B2 (en) | 2017-09-13 | 2019-12-24 | United Technologies Corporation | Seal interface with a deflection control feature |
| FR3072908B1 (fr) * | 2017-10-26 | 2021-02-26 | Safran Nacelles | Ensemble propulsif pour aeronef |
| RU2729591C1 (ru) * | 2019-08-01 | 2020-08-11 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Поворотное осесимметричное сопло турбореактивного двигателя |
| US12345180B2 (en) * | 2022-01-20 | 2025-07-01 | General Electric Company | Stator plenum for a gas turbine engine |
| FR3136516B1 (fr) * | 2022-06-14 | 2024-08-02 | Safran Nacelles | Ensemble pour turbomachine |
| CN115143847B (zh) * | 2022-07-28 | 2024-07-19 | 西安现代控制技术研究所 | 一种远程弹箭弹尾防热密封复合结构 |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1217638A (fr) * | 1957-11-22 | 1960-05-04 | Snecma | Perfectionnements aux tuyères de réacteur |
| US3972475A (en) * | 1975-07-31 | 1976-08-03 | United Technologies Corporation | Nozzle construction providing for thermal growth |
| US4043509A (en) * | 1976-05-13 | 1977-08-23 | General Electric Company | Actuation system for a gas turbine engine exhaust device |
| US4645217A (en) * | 1985-11-29 | 1987-02-24 | United Technologies Corporation | Finger seal assembly |
| US5101624A (en) * | 1989-09-07 | 1992-04-07 | General Electric Company | Exhaust nozzle hinge |
| FR2670177B1 (fr) * | 1990-12-05 | 1993-01-22 | Snecma | Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur. |
| US5150839A (en) * | 1991-03-14 | 1992-09-29 | General Electric Company | Nozzle load management |
| US5143292A (en) * | 1991-05-09 | 1992-09-01 | General Electric Company | Cooled leaf seal |
| DE4408260A1 (de) * | 1994-03-11 | 1995-09-21 | Mtu Muenchen Gmbh | Dichtung |
| US5522546A (en) * | 1994-08-19 | 1996-06-04 | General Electric Company | Variable exhaust nozzle seal |
| US5560198A (en) * | 1995-05-25 | 1996-10-01 | United Technologies Corporation | Cooled gas turbine engine augmentor fingerseal assembly |
| US5897120A (en) * | 1997-04-15 | 1999-04-27 | General Electric Company | Outer flap elastic seal assembly |
| RU2143577C1 (ru) * | 1998-03-20 | 1999-12-27 | Открытое акционерное общество "А.Люлька-Сатурн" | Устройство для сочленения наружной поверхности поворотного реактивного сопла двигателя и мотогондолы самолета |
| JP3600912B2 (ja) * | 2001-09-12 | 2004-12-15 | 川崎重工業株式会社 | 燃焼器ライナのシール構造 |
| US6751944B2 (en) * | 2001-10-23 | 2004-06-22 | The Nordam Group, Inc. | Confluent variable exhaust nozzle |
| FR2835288B1 (fr) * | 2002-01-31 | 2006-04-28 | Snecma Moteurs | Systeme de refroidissement pour une tuyere de post-combustion de turbomachine |
-
2003
- 2003-05-27 FR FR0306390A patent/FR2855559B1/fr not_active Expired - Fee Related
-
2004
- 2004-05-11 AT AT04291200T patent/ATE333570T1/de not_active IP Right Cessation
- 2004-05-11 PL PL04291200T patent/PL1482127T3/pl unknown
- 2004-05-11 ES ES04291200T patent/ES2270305T3/es not_active Expired - Lifetime
- 2004-05-11 DE DE602004001546T patent/DE602004001546T2/de not_active Expired - Lifetime
- 2004-05-11 EP EP04291200A patent/EP1482127B1/fr not_active Expired - Lifetime
- 2004-05-13 CA CA002469853A patent/CA2469853A1/fr not_active Abandoned
- 2004-05-19 JP JP2004148940A patent/JP4146389B2/ja not_active Expired - Lifetime
- 2004-05-19 US US10/847,864 patent/US6966189B2/en not_active Expired - Lifetime
- 2004-05-19 NZ NZ533014A patent/NZ533014A/en unknown
- 2004-05-20 AU AU2004202177A patent/AU2004202177A1/en not_active Abandoned
- 2004-05-20 ZA ZA200403929A patent/ZA200403929B/xx unknown
- 2004-05-24 IL IL162142A patent/IL162142A/en not_active IP Right Cessation
- 2004-05-24 BR BR0401807-9A patent/BRPI0401807A/pt not_active IP Right Cessation
- 2004-05-25 KR KR1020040037464A patent/KR20040102334A/ko not_active Withdrawn
- 2004-05-26 RU RU2004116112/06A patent/RU2342551C2/ru active
- 2004-05-26 UA UA20040504013A patent/UA81234C2/xx unknown
- 2004-05-27 CN CNB2004100475793A patent/CN100346066C/zh not_active Expired - Lifetime
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4146389B2 (ja) | 後燃焼室を有するターボマシンのノズルへの入口で、二次流をシーリングするためのシステム | |
| JP5484474B2 (ja) | タービンエンジンにおける燃焼室とタービンディストリビュータとの間のシーリング | |
| US4553901A (en) | Stator structure for a gas turbine engine | |
| US4767267A (en) | Seal assembly | |
| JP4185476B2 (ja) | ガスタービン内のクリアランスを制御するための装置 | |
| CN102817641B (zh) | 用于燃气涡轮机的密封组件 | |
| JP6483957B2 (ja) | 燃料ノズルハウジングを備えたマルチチューブ燃料ノズルを有するシステム | |
| US8490400B2 (en) | Combustor assembly comprising a combustor device, a transition duct and a flow conditioner | |
| CN100467832C (zh) | 燃气轮机 | |
| JP5302979B2 (ja) | タービン・エンジン用高温シール | |
| JPS5924331B2 (ja) | 定置型燃焼タ−ビンの触媒燃焼装置 | |
| JP2014181901A (ja) | マルチチューブ燃料ノズルを有するシステム | |
| JP2007513281A (ja) | 燃焼器壁とノズルプラットフォームとの間の褶動ジョイント | |
| CN103052766A (zh) | 具有片密封件的涡轮机的部件以及用于进行密封以防止导流片与承载元件之间泄漏的方法 | |
| CN105917082B (zh) | 用于燃气涡轮发动机中相邻的过渡导管的出口部分之间间隙的密封组件 | |
| JP2004150325A (ja) | タービン翼環構造 | |
| CN112302730B (zh) | 具有互锁密封件的涡轮发动机 | |
| US12467628B1 (en) | Turbine engine having a combustion section | |
| JP2021526193A (ja) | ターボ機械ケーシングの冷却装置 | |
| CA1312888C (en) | Seal assembly |