JP2020507707A - ガスタービン用のタービンブレードまたはタービンベーン - Google Patents
ガスタービン用のタービンブレードまたはタービンベーン Download PDFInfo
- Publication number
- JP2020507707A JP2020507707A JP2019541305A JP2019541305A JP2020507707A JP 2020507707 A JP2020507707 A JP 2020507707A JP 2019541305 A JP2019541305 A JP 2019541305A JP 2019541305 A JP2019541305 A JP 2019541305A JP 2020507707 A JP2020507707 A JP 2020507707A
- Authority
- JP
- Japan
- Prior art keywords
- turbine
- platform
- cooling
- wing
- vane
- 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.)
- Pending
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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
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/185—Liquid cooling
-
- 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
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/186—Film cooling
-
- 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
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
-
- 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
-
- 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
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/122—Fluid guiding means, e.g. vanes related to the trailing edge of a stator vane
-
- 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
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
-
- 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
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
Abstract
Description
12 ルート
13 高温ガス経路
14 プラットフォーム
15 中空翼
16 高温ガス流
17 プラットフォームレベル
18 前縁
20 タービンベーン
22 後縁
24 翼先端
26 冷却流体入口
28 冷却流体
29 衝突冷却機構
30 冷却キャビティ
31 交差孔
32 冷却通路
33 第1の表面
34 配列
35 サブチャネル
36 ピンフィン
37 領域
38 冷却流体出口
40 翼補強リップ
46 リップ端
Claims (5)
- ガスタービンのためのタービンブレード(10)またはタービンベーン(20)であって、
前記タービンブレード(10)またはタービンベーン(20)をキャリアに取り付けるためのルート(12)と、
プラットフォーム(14)と、
空力学的形状の中空の翼(15)であって、共通の前縁(18)から共通の後縁(22)への高温ガス流(16)の方向に関して延在し、かつ前記プラットフォーム(14)から翼先端(24)へ横方向に延在する負圧側壁および正圧側壁を備える中空の翼(15)と、
を前記ガスタービンの半径方向に沿って連続的に備え、
前記翼(15)は、プラットフォームレベル(17)から前記翼先端への冷却流体の流れ方向に従って延在する少なくとも1つの冷却キャビティ(30)を備え、前記少なくとも1つの冷却キャビティ(30)は、前記冷却キャビティ(30)と複数の冷却流体出口(38)との間に配置された衝突冷却機構の配列(34)を通り、前記後縁(22)に沿って分布した前記複数の冷却流体出口(38)と流体接続し、
前記配列(34)は、前記プラットフォーム(14)内の前記翼(15)の半径方向外側に位置する領域(37)内へ延在し、前記領域は、衝突冷却機構を備えることを特徴とする、タービンブレード(10)またはタービンベーン(20)。 - 前記衝突冷却機構が交差孔(31)として形成され、前記配列が少なくとも1列の交差孔(31)を備え、前記少なくとも1列が前記プラットフォーム(14)内に完全に配置された少なくとも1つの交差孔(31)を備える、請求項1に記載のタービンブレード(10)またはタービンベーン(20)。
- 前記衝突冷却機構がピンフィン(36)として形成され、前記配列が少なくとも1列のピンフィン(36)を備え、前記ピンフィン(36)が前記タービンブレード(10)またはタービンベーン(20)の長手方向断面で見ると、長方形の形状を有する、請求項1に記載のタービンブレード(10)またはタービンベーン(20)。
- 前記冷却キャビティ(30)がまた前記冷却流体の折り返し部分(42)におけるリブ端部(46)で半径方向内側が終端する翼補強リブによって境界付けられ、前記リブ端部(46)は、前記プラットフォームレベル(17)の半径方向内側に位置する、請求項1〜3のいずれか一項に記載のタービンブレード(10)またはタービンベーン(20)。
- リブ(40)および前記配列(34)が前記プラットフォームの高温ガス表面(33)より下の同じレベルで終端する、請求項4に記載のタービンブレード(10)またはタービンベーン(20)。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP17153962.0A EP3354850A1 (en) | 2017-01-31 | 2017-01-31 | A turbine blade or a turbine vane for a gas turbine |
EP17153962.0 | 2017-01-31 | ||
PCT/EP2018/050351 WO2018141504A1 (en) | 2017-01-31 | 2018-01-08 | A turbine blade or a turbine vane for a gas turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2020507707A true JP2020507707A (ja) | 2020-03-12 |
Family
ID=57944357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2019541305A Pending JP2020507707A (ja) | 2017-01-31 | 2018-01-08 | ガスタービン用のタービンブレードまたはタービンベーン |
Country Status (5)
Country | Link |
---|---|
US (1) | US11053802B2 (ja) |
EP (2) | EP3354850A1 (ja) |
JP (1) | JP2020507707A (ja) |
CN (1) | CN110234840B (ja) |
WO (1) | WO2018141504A1 (ja) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10787932B2 (en) * | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
US11661852B2 (en) * | 2019-02-08 | 2023-05-30 | Raytheon Technologies Corporation | Turbine blade trailing edge cooling feed |
CN113266436B (zh) * | 2021-05-14 | 2022-10-25 | 西安交通大学 | 用于燃气轮机静叶内部冷却的通道结构及燃气轮机静叶 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5387086A (en) * | 1993-07-19 | 1995-02-07 | General Electric Company | Gas turbine blade with improved cooling |
JPH08503530A (ja) * | 1992-11-24 | 1996-04-16 | ユナイテッド・テクノロジーズ・コーポレイション | 冷却可能なエアフォイル及び該エアフォイル鋳造用中子 |
JP2004308659A (ja) * | 2003-04-08 | 2004-11-04 | United Technol Corp <Utc> | タービン要素およびタービンブレードの製造方法 |
JP2007064226A (ja) * | 2005-08-31 | 2007-03-15 | General Electric Co <Ge> | パターン冷却式タービン翼形部 |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2476207A1 (fr) | 1980-02-19 | 1981-08-21 | Snecma | Perfectionnement aux aubes de turbines refroidies |
JP3238344B2 (ja) * | 1997-02-20 | 2001-12-10 | 三菱重工業株式会社 | ガスタービン静翼 |
US6174134B1 (en) * | 1999-03-05 | 2001-01-16 | General Electric Company | Multiple impingement airfoil cooling |
US6607356B2 (en) * | 2002-01-11 | 2003-08-19 | General Electric Company | Crossover cooled airfoil trailing edge |
US8292582B1 (en) * | 2009-07-09 | 2012-10-23 | Florida Turbine Technologies, Inc. | Turbine blade with serpentine flow cooling |
CN102116179A (zh) * | 2011-03-11 | 2011-07-06 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 燃气轮机的涡轮转子叶片 |
CN202055870U (zh) * | 2011-03-11 | 2011-11-30 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 燃气轮机的涡轮转子叶片 |
WO2016076834A1 (en) * | 2014-11-11 | 2016-05-19 | Siemens Aktiengesellschaft | Turbine blade with axial tip cooling circuit |
EP3232001A1 (de) * | 2016-04-15 | 2017-10-18 | Siemens Aktiengesellschaft | Laufschaufel für eine turbine |
-
2017
- 2017-01-31 EP EP17153962.0A patent/EP3354850A1/en not_active Withdrawn
-
2018
- 2018-01-08 WO PCT/EP2018/050351 patent/WO2018141504A1/en unknown
- 2018-01-08 US US16/479,572 patent/US11053802B2/en active Active
- 2018-01-08 EP EP18702067.2A patent/EP3545171B1/en active Active
- 2018-01-08 CN CN201880009283.2A patent/CN110234840B/zh active Active
- 2018-01-08 JP JP2019541305A patent/JP2020507707A/ja active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH08503530A (ja) * | 1992-11-24 | 1996-04-16 | ユナイテッド・テクノロジーズ・コーポレイション | 冷却可能なエアフォイル及び該エアフォイル鋳造用中子 |
US5387086A (en) * | 1993-07-19 | 1995-02-07 | General Electric Company | Gas turbine blade with improved cooling |
JP2004308659A (ja) * | 2003-04-08 | 2004-11-04 | United Technol Corp <Utc> | タービン要素およびタービンブレードの製造方法 |
JP2007064226A (ja) * | 2005-08-31 | 2007-03-15 | General Electric Co <Ge> | パターン冷却式タービン翼形部 |
Also Published As
Publication number | Publication date |
---|---|
EP3354850A1 (en) | 2018-08-01 |
WO2018141504A1 (en) | 2018-08-09 |
CN110234840B (zh) | 2022-08-23 |
EP3545171B1 (en) | 2020-11-04 |
US11053802B2 (en) | 2021-07-06 |
EP3545171A1 (en) | 2019-10-02 |
CN110234840A (zh) | 2019-09-13 |
US20190368358A1 (en) | 2019-12-05 |
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