JP6031116B2 - ガスタービンエンジン用の非対称半径方向スプラインシール - Google Patents
ガスタービンエンジン用の非対称半径方向スプラインシール Download PDFInfo
- Publication number
- JP6031116B2 JP6031116B2 JP2014539946A JP2014539946A JP6031116B2 JP 6031116 B2 JP6031116 B2 JP 6031116B2 JP 2014539946 A JP2014539946 A JP 2014539946A JP 2014539946 A JP2014539946 A JP 2014539946A JP 6031116 B2 JP6031116 B2 JP 6031116B2
- Authority
- JP
- Japan
- Prior art keywords
- radial
- axial
- leg
- slot
- received
- 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.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/005—Sealing means between non relatively rotating elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/11—Shroud seal segments
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/57—Leaf seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/59—Lamellar seals
Description
52 弓状底壁部
54 前方壁部
56 後方壁部
58 側壁
60 開放シュラウドキャビティ
Claims (8)
- ガスタービンエンジン用のシュラウド装置であって、
弓状内側流路面を定める弓状底壁部と、前記底壁部から半径方向外向きに延びる離間した前方及び後方壁部と、前記前方及び後方壁部間で前記底壁部から半径方向外向きに延びて、端面を各々が定める離間した前方及び後方側壁と、を有する環状シュラウドセグメントを備え、前記各端面が、
前記端面に沿って略軸方向に延びる軸方向スロットと、
前記端面に沿って略半径方向に延び、前記軸方向スロットと交差する第1の半径方向スロットと、
前記端面に沿って略半径方向に延び、前記軸方向スロットと交差する第2の半径方向スロットと、
前記軸方向スロット内に受けられる軸方向スプラインシールと、
L字形を有し、半径方向レッグ及び該半径方向レッグよりも実質的に短い軸方向レッグを備えた第1の半径方向スプラインシールと、
L字形を有し、半径方向レッグ及び該半径方向レッグよりも実質的に短い軸方向レッグを備えた第2の半径方向スプラインシールと、
を含み、
前記半径方向レッグが前記第1の半径方向スロット内に受けられ、前記軸方向レッグが前記軸方向スロット内に受けられ、
前記半径方向レッグが前記第2の半径方向スロット内に受けられ、前記軸方向レッグが前記軸方向スロット内に受けられ、
前記第1及び第2の半径方向スロットが、前記後方壁部に沿って前記弓状内側流路面まで延びる
シュラウド装置。 - 前記軸方向スロットが前記底壁部に沿って延びる、請求項1に記載のシュラウド装置。
- 前記底壁部が、前記後方壁部を通過して軸方向後方に延びて後方突出部を定める、請求項1又は2に記載の装置。
- 前記前方壁部から軸方向前方に弓状前方レールが延びる、請求項1乃至3のいずれか1項に記載の装置。
- 前記後方壁部から軸方向後方に弓状後方レールが延びる、請求項1乃至4のいずれか1項に記載の装置。
- ガスタービンエンジン用のシュラウド装置であって、
弓状内側流路面を定める弓状底壁部と、前記底壁部から半径方向外向きに延びる離間した前方及び後方壁部と、前記前方及び後方壁部間で前記底壁部から半径方向外向きに延びて、端面を各々が定める離間した前方及び後方側壁と、を各々が有する弓状シュラウドセグメントの環状アレイを備え、前記シュラウドセグメントが、隣接する前記シュラウドセグメントの他面間にギャップが存在するように配列されており、前記各端面が、
前記端面に沿って略軸方向に延びる軸方向スロットと、
前記端面に沿って略半径方向に延び、前記軸方向スロットと交差する第1の半径方向スロットと、
前記端面に沿って略半径方向に延び、前記軸方向スロットと交差する第2の半径方向スロットと、
隣接する前記端面の各ペアの軸方向スロット内に各々が受けられる複数の軸方向スプラインシールと、
各々がL字形を有し、半径方向レッグ及び該半径方向レッグよりも実質的に短い軸方向レッグを備えた複数の第1の半径方向スプラインシールと、
各々がL字形を有し、半径方向レッグ及び該半径方向レッグよりも実質的に短い軸方向レッグを備えた複数の第2の半径方向スプラインシールと、
を含み、
前記第1の半径方向スプラインシールの半径方向レッグが、前記隣接する端面の各ペアの第1の半径方向スロット内に受けられ、前記軸方向レッグが、前記隣接する端面の各ペアの軸方向スロット内に受けられ、
前記第2の半径方向スプラインシールの半径方向レッグが、前記隣接する端面の各ペアの第2の半径方向スロット内に受けられ、
前記軸方向レッグが、前記隣接する端面の各ペアの軸方向スロット内に受けられ、
前記第1及び第2の半径方向スロットが、前記後方壁部に沿って前記弓状内側流路面まで延びる
シュラウド装置。 - 前記底壁部が、前記後方壁部を通過して軸方向後方に延びて後方突出部を定める、請求項6に記載の装置。
- 前記軸方向スプラインシールが、前記第1及び第2の半径方向スプラインシールより軸方向後方まで延びる、請求項1乃至7のいずれか1項に記載のシュラウド装置。
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161556270P | 2011-11-06 | 2011-11-06 | |
US61/556,270 | 2011-11-06 | ||
US13/443,947 | 2012-04-11 | ||
US13/443,947 US9810086B2 (en) | 2011-11-06 | 2012-04-11 | Asymmetric radial spline seal for a gas turbine engine |
PCT/US2012/052185 WO2013074165A2 (en) | 2011-11-06 | 2012-08-24 | Asymmetric radial spline seal for a gas turbine engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2014532831A JP2014532831A (ja) | 2014-12-08 |
JP6031116B2 true JP6031116B2 (ja) | 2016-11-24 |
Family
ID=48223803
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2014539946A Expired - Fee Related JP6031116B2 (ja) | 2011-11-06 | 2012-08-24 | ガスタービンエンジン用の非対称半径方向スプラインシール |
Country Status (8)
Country | Link |
---|---|
US (1) | US9810086B2 (ja) |
EP (1) | EP2776681A2 (ja) |
JP (1) | JP6031116B2 (ja) |
CN (1) | CN103906896B (ja) |
BR (1) | BR112014010747A8 (ja) |
CA (1) | CA2853622C (ja) |
IN (1) | IN2014CN03298A (ja) |
WO (1) | WO2013074165A2 (ja) |
Families Citing this family (21)
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US9810086B2 (en) * | 2011-11-06 | 2017-11-07 | General Electric Company | Asymmetric radial spline seal for a gas turbine engine |
JP5717904B1 (ja) * | 2014-08-04 | 2015-05-13 | 三菱日立パワーシステムズ株式会社 | 静翼、ガスタービン、分割環、静翼の改造方法、および、分割環の改造方法 |
US9915159B2 (en) | 2014-12-18 | 2018-03-13 | General Electric Company | Ceramic matrix composite nozzle mounted with a strut and concepts thereof |
FR3041993B1 (fr) * | 2015-10-05 | 2019-06-21 | Safran Aircraft Engines | Ensemble d'anneau de turbine avec maintien axial |
US10161257B2 (en) | 2015-10-20 | 2018-12-25 | General Electric Company | Turbine slotted arcuate leaf seal |
US10494943B2 (en) * | 2016-02-03 | 2019-12-03 | General Electric Company | Spline seal for a gas turbine engine |
US10557360B2 (en) * | 2016-10-17 | 2020-02-11 | United Technologies Corporation | Vane intersegment gap sealing arrangement |
US10655495B2 (en) * | 2017-02-24 | 2020-05-19 | General Electric Company | Spline for a turbine engine |
KR101937586B1 (ko) * | 2017-09-12 | 2019-01-10 | 두산중공업 주식회사 | 베인 조립체, 터빈 및 이를 포함하는 가스터빈 |
EP3650656A1 (en) | 2017-09-15 | 2020-05-13 | General Electric Company Polska sp. z o.o. | Inner band assembly for a turbine nozzle |
US10662794B2 (en) * | 2017-10-19 | 2020-05-26 | Rolls-Royce Corporation | Strip seal axial assembly groove |
EP3486018A1 (en) | 2017-11-20 | 2019-05-22 | Agie Charmilles SA | Method and device for machining shapes using electrical machining |
US20190309643A1 (en) * | 2018-04-05 | 2019-10-10 | United Technologies Corporation | Axial stiffening ribs/augmentation fins |
US10982559B2 (en) | 2018-08-24 | 2021-04-20 | General Electric Company | Spline seal with cooling features for turbine engines |
US10794206B2 (en) * | 2018-09-05 | 2020-10-06 | Raytheon Technologies Corporation | CMC BOAS intersegment seal |
US20200141276A1 (en) * | 2018-11-07 | 2020-05-07 | General Electric Company | Turbine shroud with lapped seal segments |
US11021990B2 (en) * | 2018-12-19 | 2021-06-01 | General Electric Company | Shroud sealing for a gas turbine engine |
US11326463B2 (en) * | 2019-06-19 | 2022-05-10 | Raytheon Technologies Corporation | BOAS thermal baffle |
US11187094B2 (en) | 2019-08-26 | 2021-11-30 | General Electric Company | Spline for a turbine engine |
US11401830B2 (en) * | 2019-09-06 | 2022-08-02 | Raytheon Technologies Corporation | Geometry for a turbine engine blade outer air seal |
US11215063B2 (en) | 2019-10-10 | 2022-01-04 | General Electric Company | Seal assembly for chute gap leakage reduction in a gas turbine |
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FR2869944B1 (fr) * | 2004-05-04 | 2006-08-11 | Snecma Moteurs Sa | Dispositif de refroidissement pour anneau fixe de turbine a gaz |
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-
2012
- 2012-04-11 US US13/443,947 patent/US9810086B2/en active Active
- 2012-08-24 JP JP2014539946A patent/JP6031116B2/ja not_active Expired - Fee Related
- 2012-08-24 IN IN3298CHN2014 patent/IN2014CN03298A/en unknown
- 2012-08-24 BR BR112014010747A patent/BR112014010747A8/pt not_active IP Right Cessation
- 2012-08-24 CN CN201280054278.6A patent/CN103906896B/zh active Active
- 2012-08-24 CA CA2853622A patent/CA2853622C/en not_active Expired - Fee Related
- 2012-08-24 WO PCT/US2012/052185 patent/WO2013074165A2/en active Application Filing
- 2012-08-24 EP EP12832724.4A patent/EP2776681A2/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP2776681A2 (en) | 2014-09-17 |
JP2014532831A (ja) | 2014-12-08 |
US20130115065A1 (en) | 2013-05-09 |
WO2013074165A8 (en) | 2013-06-27 |
CA2853622A1 (en) | 2013-05-23 |
WO2013074165A3 (en) | 2013-08-15 |
WO2013074165A2 (en) | 2013-05-23 |
US9810086B2 (en) | 2017-11-07 |
BR112014010747A8 (pt) | 2017-06-20 |
CN103906896A (zh) | 2014-07-02 |
CA2853622C (en) | 2016-12-13 |
CN103906896B (zh) | 2016-08-31 |
IN2014CN03298A (ja) | 2015-10-09 |
BR112014010747A2 (pt) | 2017-06-13 |
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