JP4889123B2 - ターボ機械用可動ブレード - Google Patents
ターボ機械用可動ブレード Download PDFInfo
- Publication number
- JP4889123B2 JP4889123B2 JP2007266440A JP2007266440A JP4889123B2 JP 4889123 B2 JP4889123 B2 JP 4889123B2 JP 2007266440 A JP2007266440 A JP 2007266440A JP 2007266440 A JP2007266440 A JP 2007266440A JP 4889123 B2 JP4889123 B2 JP 4889123B2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- pressure side
- turbomachine
- rim
- edge
- 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.)
- Active
Links
- 238000001816 cooling Methods 0.000 claims description 16
- 238000000926 separation method Methods 0.000 claims description 15
- 239000012530 fluid Substances 0.000 claims description 7
- 238000012935 Averaging Methods 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Images
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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/10—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using sealing fluid, e.g. steam
-
- 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
-
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/184—Two-dimensional patterned sinusoidal
-
- 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
- F05D2250/00—Geometry
- F05D2250/60—Structure; Surface texture
- F05D2250/61—Structure; Surface texture corrugated
- F05D2250/611—Structure; Surface texture corrugated undulated
-
- 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
- F05D2250/00—Geometry
- F05D2250/70—Shape
Description
10、110 固定根元部
14、114、424、554 端部面
16、116、216、316、416、556 圧力側面
18、118 吸引側面
20、120、550 突起縁部
22、122、322、422 頂部部分
26 回転ディスク
28 筐体リング
112 エアロフォイル
129、429 凹湾曲
130、131、230、430 輪郭
130a 緩やかに傾斜する区画
130b 急峻に傾斜する区画
131、231 凸湾曲
132 開口空洞
134 端部壁
136、436 圧力側リム
138、538 吸引側リム
140、442 冷却チャネル
142、440 内部冷却通路
222 波形にされた頂部部分
229 連続的な凹湾曲
423 吸引側壁
A 主方向
B 平均縁部角度
C 乱流
F 流れ
G 平均縁部角度
I 間隙
R 回転軸
Claims (9)
- 頂部プラットフォームのないターボ機械可動ブレードであって、ブレードはエアロフォイル(112)が上に載る固定根元部(110)を含み、エアロフォイルは端部面(114)および圧力側面と吸引側面(116と118)を有し、固定根元部および前記端部面はそれぞれブレードの主軸(A)に沿って間隔を置くブレードの底部および頂端部に配置され、エアロフォイルはその圧力側面の頂部部分に突起縁部(120)を有し、突起縁部はその端部面の部分(124)と圧力側面の頂部部分(122)との間に画定され、これらの部分は互いの間に厳密に90°未満の平均縁部角度(B)を形成してターボ機械を通過する流体の流れ(F)が前記縁部で分離するのを促進し、ブレードは圧力側面の頂部部分(122)に波形が付けられ、ブレードの主要軸に直角な任意の断面で連続的に交互する凹湾曲(129)と凸湾曲(131)によって形成される輪郭(130)に従うことを特徴とする、ターボ機械可動ブレード。
- 圧力側面の前記頂部部分(122)がブレードの圧力側面の残りに対して隆起する、請求項1に記載のターボ機械ブレード。
- 頂端部に端部壁(134)と、圧力側リム(136)と、吸引側リム(138)とによって画定される開口空洞(132)を有し、前記突起縁部(120)が端部面と圧力側リムの波形を付けられた圧力側面との間の圧力側リム上に形成される、請求項1または2に記載のターボ機械ブレード。
- 内部冷却通路(142)および前記内部冷却通路に連絡する少なくとも1つの冷却チャネル(140)を含み、チャネルが、圧力側面の頂部部分(122)の波形中の隆起ゾーンに位置合わせされて、前記端部面の部分(124)に開口する、請求項1から3のいずれか一項に記載のターボ機械ブレード。
- 圧力側リム(436)が波形にされ、圧力側に向かって傾斜する、請求項3に記載のターボ機械ブレード。
- 内部冷却通路(442)および前記内部冷却通路に連絡する少なくとも1つの冷却チャネル(440)を含み、前記チャネルが、前記リムの波形の後退ゾーンに位置合わせされて圧力側リム(436)の基部に開口する、請求項5に記載のターボ機械ブレード。
- 他の突起縁部(550)が端部面と吸引側リム(538)の圧力側面との間に画定され、これらの部分はそれらの間に厳密に90°未満の平均縁部角度(G)を形成してターボ機械を通過する流体の流れ(F)が前記他の縁部で分離するのを促進し、吸引側リム(538)の圧力側面は、波形が付けられ、ブレードの主要軸に直角な任意の断面で連続的に交互する凹湾曲と凸湾曲によって形成される輪郭に従う、請求項3に記載のターボ機械ブレード。
- 請求項1から7のいずれか一項に記載のブレードを含む、タービン。
- 請求項8に記載のタービンを含む、ターボ機械。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0654257 | 2006-10-13 | ||
FR0654257A FR2907157A1 (fr) | 2006-10-13 | 2006-10-13 | Aube mobile de turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2008095695A JP2008095695A (ja) | 2008-04-24 |
JP4889123B2 true JP4889123B2 (ja) | 2012-03-07 |
Family
ID=38066650
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2007266440A Active JP4889123B2 (ja) | 2006-10-13 | 2007-10-12 | ターボ機械用可動ブレード |
Country Status (7)
Country | Link |
---|---|
US (1) | US7972115B2 (ja) |
EP (1) | EP1911934B1 (ja) |
JP (1) | JP4889123B2 (ja) |
CA (1) | CA2606072C (ja) |
DE (1) | DE602007001652D1 (ja) |
FR (1) | FR2907157A1 (ja) |
RU (1) | RU2457335C2 (ja) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB0813556D0 (en) * | 2008-07-24 | 2008-09-03 | Rolls Royce Plc | A blade for a rotor |
US8777567B2 (en) | 2010-09-22 | 2014-07-15 | Honeywell International Inc. | Turbine blades, turbine assemblies, and methods of manufacturing turbine blades |
GB201100957D0 (en) * | 2011-01-20 | 2011-03-02 | Rolls Royce Plc | Rotor blade |
US9322280B2 (en) * | 2011-08-12 | 2016-04-26 | United Technologies Corporation | Method of measuring turbine blade tip erosion |
FR2982903B1 (fr) * | 2011-11-17 | 2014-02-21 | Snecma | Aube de turbine a gaz a decalage vers l'intrados des sections de tete et a canaux de refroidissement |
CN102678189A (zh) * | 2011-12-13 | 2012-09-19 | 河南科技大学 | 一种具有叶顶防泄漏结构的涡轮冷却叶片 |
US9091177B2 (en) * | 2012-03-14 | 2015-07-28 | United Technologies Corporation | Shark-bite tip shelf cooling configuration |
EP2666968B1 (en) * | 2012-05-24 | 2021-08-18 | General Electric Company | Turbine rotor blade |
US9188012B2 (en) * | 2012-05-24 | 2015-11-17 | General Electric Company | Cooling structures in the tips of turbine rotor blades |
US9470096B2 (en) * | 2012-07-26 | 2016-10-18 | General Electric Company | Turbine bucket with notched squealer tip |
RU2529273C1 (ru) * | 2013-09-11 | 2014-09-27 | Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" | Рабочая лопатка турбины газотурбинного двигателя |
US9856739B2 (en) * | 2013-09-18 | 2018-01-02 | Honeywell International Inc. | Turbine blades with tip portions having converging cooling holes |
US9816389B2 (en) | 2013-10-16 | 2017-11-14 | Honeywell International Inc. | Turbine rotor blades with tip portion parapet wall cavities |
US9879544B2 (en) | 2013-10-16 | 2018-01-30 | Honeywell International Inc. | Turbine rotor blades with improved tip portion cooling holes |
US9528379B2 (en) | 2013-10-23 | 2016-12-27 | General Electric Company | Turbine bucket having serpentine core |
US9638041B2 (en) | 2013-10-23 | 2017-05-02 | General Electric Company | Turbine bucket having non-axisymmetric base contour |
US9551226B2 (en) | 2013-10-23 | 2017-01-24 | General Electric Company | Turbine bucket with endwall contour and airfoil profile |
US9797258B2 (en) | 2013-10-23 | 2017-10-24 | General Electric Company | Turbine bucket including cooling passage with turn |
US9670784B2 (en) | 2013-10-23 | 2017-06-06 | General Electric Company | Turbine bucket base having serpentine cooling passage with leading edge cooling |
US20150110617A1 (en) * | 2013-10-23 | 2015-04-23 | General Electric Company | Turbine airfoil including tip fillet |
FR3043715B1 (fr) * | 2015-11-16 | 2020-11-06 | Snecma | Aube de turbine comprenant une pale avec baignoire comportant un intrados incurve dans la region du sommet de pale |
US20170145827A1 (en) * | 2015-11-23 | 2017-05-25 | United Technologies Corporation | Turbine blade with airfoil tip vortex control |
US10677066B2 (en) | 2015-11-23 | 2020-06-09 | United Technologies Corporation | Turbine blade with airfoil tip vortex control |
US10253637B2 (en) * | 2015-12-11 | 2019-04-09 | General Electric Company | Method and system for improving turbine blade performance |
EP3216983A1 (de) | 2016-03-08 | 2017-09-13 | Siemens Aktiengesellschaft | Laufschaufel für eine gasturbine mit gekühlter anstreifkante |
US10465525B2 (en) * | 2016-07-22 | 2019-11-05 | General Electric Company | Blade with internal rib having corrugated surface(s) |
US10450868B2 (en) * | 2016-07-22 | 2019-10-22 | General Electric Company | Turbine rotor blade with coupon having corrugated surface(s) |
US10443399B2 (en) * | 2016-07-22 | 2019-10-15 | General Electric Company | Turbine vane with coupon having corrugated surface(s) |
US10436037B2 (en) * | 2016-07-22 | 2019-10-08 | General Electric Company | Blade with parallel corrugated surfaces on inner and outer surfaces |
US10465520B2 (en) | 2016-07-22 | 2019-11-05 | General Electric Company | Blade with corrugated outer surface(s) |
EP3361056A1 (de) | 2017-02-10 | 2018-08-15 | Siemens Aktiengesellschaft | Leitschaufel für eine strömungsmaschine |
WO2019035800A1 (en) * | 2017-08-14 | 2019-02-21 | Siemens Aktiengesellschaft | AUBES OF TURBINE |
US11365638B2 (en) * | 2017-08-14 | 2022-06-21 | Siemens Energy Global GmbH & Co. KG | Turbine blade and corresponding method of servicing |
US10787932B2 (en) | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
BE1026579B1 (fr) * | 2018-08-31 | 2020-03-30 | Safran Aero Boosters Sa | Aube a protuberance pour compresseur de turbomachine |
US11773726B2 (en) * | 2019-10-16 | 2023-10-03 | Rtx Corporation | Angled tip rods |
US11066935B1 (en) * | 2020-03-20 | 2021-07-20 | General Electric Company | Rotor blade airfoil |
US11913353B2 (en) * | 2021-08-06 | 2024-02-27 | Rtx Corporation | Airfoil tip arrangement for gas turbine engine |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU411214A1 (ja) * | 1968-05-12 | 1974-01-15 | ||
SU412388A1 (ja) * | 1972-03-07 | 1974-01-25 | ||
US4274806A (en) * | 1979-06-18 | 1981-06-23 | General Electric Company | Staircase blade tip |
US4830315A (en) * | 1986-04-30 | 1989-05-16 | United Technologies Corporation | Airfoil-shaped body |
US5282721A (en) * | 1991-09-30 | 1994-02-01 | United Technologies Corporation | Passive clearance system for turbine blades |
US5403158A (en) * | 1993-12-23 | 1995-04-04 | United Technologies Corporation | Aerodynamic tip sealing for rotor blades |
US6494678B1 (en) * | 2001-05-31 | 2002-12-17 | General Electric Company | Film cooled blade tip |
US6672829B1 (en) * | 2002-07-16 | 2004-01-06 | General Electric Company | Turbine blade having angled squealer tip |
US6994514B2 (en) * | 2002-11-20 | 2006-02-07 | Mitsubishi Heavy Industries, Ltd. | Turbine blade and gas turbine |
US6971851B2 (en) * | 2003-03-12 | 2005-12-06 | Florida Turbine Technologies, Inc. | Multi-metered film cooled blade tip |
EP1591624A1 (de) * | 2004-04-27 | 2005-11-02 | Siemens Aktiengesellschaft | Verdichterschaufel und verdichter |
US7270514B2 (en) * | 2004-10-21 | 2007-09-18 | General Electric Company | Turbine blade tip squealer and rebuild method |
FR2885645A1 (fr) * | 2005-05-13 | 2006-11-17 | Snecma Moteurs Sa | Aube creuse de rotor pour la turbine d'un moteur a turbine a gaz, equipee d'une baignoire |
US7290986B2 (en) * | 2005-09-09 | 2007-11-06 | General Electric Company | Turbine airfoil with curved squealer tip |
US7607893B2 (en) * | 2006-08-21 | 2009-10-27 | General Electric Company | Counter tip baffle airfoil |
-
2006
- 2006-10-13 FR FR0654257A patent/FR2907157A1/fr not_active Withdrawn
-
2007
- 2007-10-10 CA CA2606072A patent/CA2606072C/fr active Active
- 2007-10-11 US US11/870,614 patent/US7972115B2/en active Active
- 2007-10-11 DE DE602007001652T patent/DE602007001652D1/de active Active
- 2007-10-11 EP EP07118256A patent/EP1911934B1/fr active Active
- 2007-10-12 RU RU2007138000/06A patent/RU2457335C2/ru active
- 2007-10-12 JP JP2007266440A patent/JP4889123B2/ja active Active
Also Published As
Publication number | Publication date |
---|---|
CA2606072C (fr) | 2015-03-31 |
CA2606072A1 (fr) | 2008-04-13 |
DE602007001652D1 (de) | 2009-09-03 |
EP1911934A1 (fr) | 2008-04-16 |
US7972115B2 (en) | 2011-07-05 |
JP2008095695A (ja) | 2008-04-24 |
RU2457335C2 (ru) | 2012-07-27 |
RU2007138000A (ru) | 2009-04-20 |
FR2907157A1 (fr) | 2008-04-18 |
US20080175716A1 (en) | 2008-07-24 |
EP1911934B1 (fr) | 2009-07-22 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP4889123B2 (ja) | ターボ機械用可動ブレード | |
JP5300874B2 (ja) | 非軸対称プラットフォームならびに外輪上の陥没および突起を備えるブレード | |
JP4923073B2 (ja) | 遷音速翼 | |
JP5461439B2 (ja) | 非軸対称プラットフォームを有するブレード | |
US9140128B2 (en) | Endwall contouring | |
KR101925892B1 (ko) | 교차식 홈을 구비한 터보차저 슈라우드 및 이를 포함한 터보차저 | |
US9518467B2 (en) | Blade with 3D platform comprising an inter-blade bulb | |
US8851833B2 (en) | Blades | |
US20170089203A1 (en) | End wall configuration for gas turbine engine | |
US9017030B2 (en) | Turbine component including airfoil with contour | |
JP2010281320A (ja) | タービン段 | |
US9377029B2 (en) | Blade of a turbomachine | |
JP5449087B2 (ja) | 翼体 | |
EP2900919B1 (en) | Endwall contouring | |
US7661926B2 (en) | Turbomachine blade | |
JP7104379B2 (ja) | 軸流型のファン、圧縮機及びタービンの翼の設計方法、並びに、当該設計により得られる翼 | |
US20130315745A1 (en) | Airfoil mateface sealing | |
US20150330230A1 (en) | Tip leakage flow directionality control | |
US9951629B2 (en) | Tip leakage flow directionality control | |
US20200024984A1 (en) | Endwall Controuring | |
WO2021060093A1 (ja) | タービン翼 | |
US20210033108A1 (en) | Compressor rotor casing with swept grooves | |
US5460488A (en) | Shrouded fan blade for a turbine engine | |
JP2015081601A (ja) | ガスタービンノズルの後縁フィレット | |
US10982566B2 (en) | Turbine and gas turbine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20100921 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20111115 |
|
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20111212 |
|
R150 | Certificate of patent or registration of utility model |
Free format text: JAPANESE INTERMEDIATE CODE: R150 Ref document number: 4889123 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20141222 Year of fee payment: 3 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |