JP6860383B2 - タービン翼の冷却構造 - Google Patents
タービン翼の冷却構造 Download PDFInfo
- Publication number
- JP6860383B2 JP6860383B2 JP2017045927A JP2017045927A JP6860383B2 JP 6860383 B2 JP6860383 B2 JP 6860383B2 JP 2017045927 A JP2017045927 A JP 2017045927A JP 2017045927 A JP2017045927 A JP 2017045927A JP 6860383 B2 JP6860383 B2 JP 6860383B2
- Authority
- JP
- Japan
- Prior art keywords
- cooling
- adjacent
- blade
- turbine
- wall
- 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
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
- F01D5/18—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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—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
-
- 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
- F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
-
- 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
- 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
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
-
- 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
- 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
- F05D2250/00—Geometry
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/185—Two-dimensional patterned serpentine-like
-
- 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
- F05D2260/2212—Improvement of heat transfer by creating turbulence
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2017045927A JP6860383B2 (ja) | 2017-03-10 | 2017-03-10 | タービン翼の冷却構造 |
| PCT/JP2018/008645 WO2018164150A1 (ja) | 2017-03-10 | 2018-03-06 | タービン翼の冷却構造 |
| CN201880014034.2A CN110337530B (zh) | 2017-03-10 | 2018-03-06 | 涡轮叶片的冷却结构 |
| GB1912924.6A GB2574951B (en) | 2017-03-10 | 2018-03-06 | Cooling structure for turbine airfoil |
| DE112018001266.2T DE112018001266B4 (de) | 2017-03-10 | 2018-03-06 | Kühlstruktur für turbinenschaufel |
| US16/558,706 US11384644B2 (en) | 2017-03-10 | 2019-09-03 | Cooling structure for turbine airfoil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2017045927A JP6860383B2 (ja) | 2017-03-10 | 2017-03-10 | タービン翼の冷却構造 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2018150829A JP2018150829A (ja) | 2018-09-27 |
| JP2018150829A5 JP2018150829A5 (enExample) | 2020-03-19 |
| JP6860383B2 true JP6860383B2 (ja) | 2021-04-14 |
Family
ID=63447846
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2017045927A Active JP6860383B2 (ja) | 2017-03-10 | 2017-03-10 | タービン翼の冷却構造 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US11384644B2 (enExample) |
| JP (1) | JP6860383B2 (enExample) |
| CN (1) | CN110337530B (enExample) |
| DE (1) | DE112018001266B4 (enExample) |
| GB (1) | GB2574951B (enExample) |
| WO (1) | WO2018164150A1 (enExample) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11248471B2 (en) * | 2020-01-22 | 2022-02-15 | General Electric Company | Turbine rotor blade with angel wing with coolant transfer passage between adjacent wheel space portions by additive manufacture |
| CN113623011B (zh) * | 2021-07-13 | 2022-11-29 | 哈尔滨工业大学 | 涡轮叶片 |
| CN113623010B (zh) * | 2021-07-13 | 2022-11-29 | 哈尔滨工业大学 | 涡轮叶片 |
| US11674446B2 (en) * | 2021-08-30 | 2023-06-13 | Collins Engine Nozzles, Inc. | Cooling for surface ignitors in torch ignition devices |
| US11674445B2 (en) * | 2021-08-30 | 2023-06-13 | Collins Engine Nozzles, Inc. | Cooling for continuous ignition devices |
| CN114872909B (zh) * | 2022-05-06 | 2023-03-24 | 中国航发四川燃气涡轮研究院 | 飞机型涡轮叶片冷却通道换热结构 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4407632A (en) * | 1981-06-26 | 1983-10-04 | United Technologies Corporation | Airfoil pedestaled trailing edge region cooling configuration |
| US5603606A (en) | 1994-11-14 | 1997-02-18 | Solar Turbines Incorporated | Turbine cooling system |
| JP4957131B2 (ja) * | 2006-09-06 | 2012-06-20 | 株式会社Ihi | 冷却構造 |
| CN100557199C (zh) * | 2007-07-13 | 2009-11-04 | 北京航空航天大学 | 一种适用于涡轮叶片等内冷部件中的渐宽型开槽交错肋通道 |
| JP2011085084A (ja) * | 2009-10-16 | 2011-04-28 | Ihi Corp | タービン翼 |
| EP2418357A1 (en) * | 2010-08-05 | 2012-02-15 | Siemens Aktiengesellschaft | Turbine airfoil and method for thermal barrier coating |
| CN102116178A (zh) * | 2011-01-18 | 2011-07-06 | 中国科学院工程热物理研究所 | 一种气冷涡轮的双射流孔冷却结构 |
| CN102102543B (zh) * | 2011-03-11 | 2013-05-15 | 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 |
| RU2014125561A (ru) * | 2011-11-25 | 2015-12-27 | Сименс Акциенгезелльшафт | Аэродинамический профиль с охлаждающими каналами |
| JP6036424B2 (ja) * | 2013-03-14 | 2016-11-30 | 株式会社Ihi | 冷却促進構造 |
| US9464528B2 (en) | 2013-06-14 | 2016-10-11 | Solar Turbines Incorporated | Cooled turbine blade with double compound angled holes and slots |
| WO2015147672A1 (en) * | 2014-03-27 | 2015-10-01 | Siemens Aktiengesellschaft | Blade for a gas turbine and method of cooling the blade |
| GB2533315B (en) * | 2014-12-16 | 2017-04-12 | Rolls Royce Plc | Cooling of engine components |
| JP2016125380A (ja) * | 2014-12-26 | 2016-07-11 | 川崎重工業株式会社 | タービン翼の冷却構造 |
-
2017
- 2017-03-10 JP JP2017045927A patent/JP6860383B2/ja active Active
-
2018
- 2018-03-06 DE DE112018001266.2T patent/DE112018001266B4/de active Active
- 2018-03-06 GB GB1912924.6A patent/GB2574951B/en active Active
- 2018-03-06 CN CN201880014034.2A patent/CN110337530B/zh active Active
- 2018-03-06 WO PCT/JP2018/008645 patent/WO2018164150A1/ja not_active Ceased
-
2019
- 2019-09-03 US US16/558,706 patent/US11384644B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| GB2574951B (en) | 2021-11-03 |
| US20200018173A1 (en) | 2020-01-16 |
| GB201912924D0 (en) | 2019-10-23 |
| CN110337530A (zh) | 2019-10-15 |
| GB2574951A8 (en) | 2020-02-05 |
| DE112018001266B4 (de) | 2025-02-06 |
| WO2018164150A1 (ja) | 2018-09-13 |
| WO2018164150A8 (ja) | 2019-09-06 |
| US11384644B2 (en) | 2022-07-12 |
| DE112018001266T5 (de) | 2019-11-28 |
| GB2574951A (en) | 2019-12-25 |
| CN110337530B (zh) | 2022-03-29 |
| JP2018150829A (ja) | 2018-09-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6860383B2 (ja) | タービン翼の冷却構造 | |
| JP6526166B2 (ja) | ベーンの冷却構造 | |
| JP6312929B2 (ja) | プラットフォームにおいて、前方、弦中央および後方の冷却チャンバを有する冷却されるタービンベーンプラットフォーム | |
| EP3696377B1 (en) | Gas turbine engine component comprising a trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements | |
| JP2013508610A (ja) | 冷却流路を形成するテーパ状冷却構造体を組み込んだ翼 | |
| WO2018164149A1 (ja) | タービン翼の冷却構造 | |
| JP6963626B2 (ja) | 衝突型プラットフォーム冷却を一体化したエアロフォイル冷却を有するタービンロータブレード | |
| US11708763B2 (en) | Turbine airfoil | |
| JP2018506678A (ja) | 弦方向に延びるスキーラ先端冷却チャネルを備えるタービン翼冷却システム | |
| US7300242B2 (en) | Turbine airfoil with integral cooling system | |
| US11578659B2 (en) | Cooling structure for turbine airfoil | |
| US9435212B2 (en) | Turbine airfoil with laterally extending snubber having internal cooling system | |
| JP6898104B2 (ja) | タービン翼の冷却構造 | |
| KR20190131106A (ko) | 터빈 조립체용 냉각 조립체 | |
| WO2023095721A1 (ja) | タービン静翼 | |
| KR101699887B1 (ko) | 블레이드 내·외벽 사이에 핀-휜과 결합된 립 구조를 갖는 가스터빈 블레이드 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20200205 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20200205 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20201020 |
|
| A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20201130 |
|
| 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: 20210302 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20210326 |
|
| R150 | Certificate of patent or registration of utility model |
Ref document number: 6860383 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |