JP6685425B2 - 後縁骨組み特徴を備えるタービン翼 - Google Patents
後縁骨組み特徴を備えるタービン翼 Download PDFInfo
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- JP6685425B2 JP6685425B2 JP2018549889A JP2018549889A JP6685425B2 JP 6685425 B2 JP6685425 B2 JP 6685425B2 JP 2018549889 A JP2018549889 A JP 2018549889A JP 2018549889 A JP2018549889 A JP 2018549889A JP 6685425 B2 JP6685425 B2 JP 6685425B2
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- trailing edge
- coolant
- pressure surface
- blade
- turbine blade
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- 239000002826 coolant Substances 0.000 claims description 72
- 238000001816 cooling Methods 0.000 claims description 26
- 238000004891 communication Methods 0.000 claims description 2
- 239000012530 fluid Substances 0.000 claims description 2
- 230000003796 beauty Effects 0.000 claims 1
- 239000011162 core material Substances 0.000 description 64
- 238000005266 casting Methods 0.000 description 12
- 238000012546 transfer Methods 0.000 description 6
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000009432 framing Methods 0.000 description 3
- 239000000919 ceramic Substances 0.000 description 2
- 229910010293 ceramic material Inorganic materials 0.000 description 2
- 239000011153 ceramic matrix composite Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 239000012809 cooling fluid Substances 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 231100001261 hazardous Toxicity 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 229910000601 superalloy Inorganic materials 0.000 description 1
Images
Classifications
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- 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
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
-
- 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
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/126—Baffles or ribs
-
- 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
- F05D2240/127—Vortex generators, turbulators, or the like, for mixing
-
- 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
- F05D2240/301—Cross-sectional characteristics
-
- 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
- F05D2240/303—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 leading 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
- F05D2240/20—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
- F05D2240/20—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
- F05D2240/305—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 pressure side 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
- F05D2240/20—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
- F05D2240/306—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 suction side 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
- 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
- F05D2260/221—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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
Description
Claims (6)
- タービン翼(10)であって、
翼内部(11)を画定する外壁(12)であって、該外壁(12)は、タービンエンジンの半径方向に沿って翼幅方向に延びており、前縁(18)および後縁(20)にて結合された正圧面(14)および負圧面(16)から形成されている、外壁(12)と、
前記正圧面(14)と前記負圧面(16)との間で前記翼内部(11)に配置された後縁冷却材キャビティ(41f)であって、該後縁冷却材キャビティ(41f)は、前記後縁(20)に隣接して配置されており、前記後縁(20)に沿って配置された複数の冷却材出口スロット(28)と流体連通しており、前記後縁冷却材キャビティ(41f)の翼幅方向端部に少なくとも1つの骨組み状通路(70,80)が形成されている、後縁冷却材キャビティ(41f)と、
前記骨組み状通路(70,80)内に配置された骨組み特徴(72A−72B,82A−82B)であって、リブ(72A−72B,82A−82B)として構成された前記骨組み特徴が、前記正圧面(14)および前記負圧面(16)から突出しており、前記リブ(72A−72B,82A−82B)は、前記正圧面(14)と前記負圧面(16)との間に部分的に延びている、骨組み特徴(72A−72B,82A−82B)と、
を備え、
複数の冷却特徴(22)が前記後縁冷却材キャビティ(41f)に配置され、該冷却特徴(22)は、前記冷却材出口スロット(28)に向かって流れる前記冷却材の流路に配置され、該冷却特徴(22)は、前記後縁冷却材キャビティ(41f)の翼幅方向端部の間に配置され、該冷却特徴(22)のそれぞれは、翼弦方向の幅よりも大きな半径方向の長さを有し、
前記冷却特徴は、ピン(22)の配列を含み、各ピン(22)は前記正圧面(14)から前記負圧面(16)まで延びており、前記配列は、前記ピン(22)の複数の半径方向列を有し、各列における前記ピン(22)は、該ピン(22)の間に冷却材通路(24)を画成するように半径方向に互いに離隔している、
タービン翼(10)。 - 前記骨組み状通路(70,80)は、前記後縁(20)に向かって翼弦方向に延びており、前記リブ(72A−72B,82A−82B)は、前記正圧面(14)および/または前記負圧面(16)において翼弦方向に離隔して配置されている、請求項1記載のタービン翼(10)。
- 前記リブ(72A−72B,82A−82B)は、前記正圧面(14)および前記負圧面(16)に形成されており、
前記正圧面(14)における前記リブ(72A,82A)および前記負圧面(16)における前記リブ(72B,82B)は、前記出口スロット(28)に向かって前記骨組み状通路(70,80)内を流れる冷却材のジグザグ流路(F)を画成するように翼弦方向で交互に配置されている、請求項2記載のタービン翼(10)。 - 各ピン(22)は、半径方向に延びている、請求項1から3までのいずれか1項記載のタービン翼(10)。
- 前記骨組み状通路(70,80)は、前記冷却特徴(22)と、翼の半径方向端面(52,54)との間に配置されている、請求項1から4までのいずれか1項記載のタービン翼(10)。
- 前記少なくとも1つの骨組み状通路(70,80)は、前記後縁冷却材キャビティ(41f)の翼幅方向の向かい合った端部に形成された、第1の骨組み状通路(70)および第2の骨組み状通路(80)を有する、請求項1から5までのいずれか1項記載のタービン翼(10)。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201662311628P | 2016-03-22 | 2016-03-22 | |
US62/311,628 | 2016-03-22 | ||
PCT/US2016/058361 WO2017164935A1 (en) | 2016-03-22 | 2016-10-24 | Turbine airfoil with trailing edge framing features |
Publications (2)
Publication Number | Publication Date |
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JP2019512641A JP2019512641A (ja) | 2019-05-16 |
JP6685425B2 true JP6685425B2 (ja) | 2020-04-22 |
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Application Number | Title | Priority Date | Filing Date |
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JP2018549889A Active JP6685425B2 (ja) | 2016-03-22 | 2016-10-24 | 後縁骨組み特徴を備えるタービン翼 |
Country Status (5)
Country | Link |
---|---|
US (1) | US11193378B2 (ja) |
EP (1) | EP3417153A1 (ja) |
JP (1) | JP6685425B2 (ja) |
CN (1) | CN108779678B (ja) |
WO (1) | WO2017164935A1 (ja) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2019005425A1 (en) * | 2017-06-30 | 2019-01-03 | Siemens Aktiengesellschaft | AERODYNAMIC TURBINE PROFILE HAVING LEAK EDGE CHARACTERISTICS AND CASTING CORE |
US10787932B2 (en) * | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
US11852024B2 (en) * | 2020-12-18 | 2023-12-26 | Ge Aviation Systems Llc | Electrical strut for a turbine engine |
Family Cites Families (16)
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US5752801A (en) * | 1997-02-20 | 1998-05-19 | Westinghouse Electric Corporation | Apparatus for cooling a gas turbine airfoil and method of making same |
US6974308B2 (en) * | 2001-11-14 | 2005-12-13 | Honeywell International, Inc. | High effectiveness cooled turbine vane or blade |
US6602047B1 (en) * | 2002-02-28 | 2003-08-05 | General Electric Company | Methods and apparatus for cooling gas turbine nozzles |
US7713027B2 (en) * | 2006-08-28 | 2010-05-11 | United Technologies Corporation | Turbine blade with split impingement rib |
US7785070B2 (en) | 2007-03-27 | 2010-08-31 | Siemens Energy, Inc. | Wavy flow cooling concept for turbine airfoils |
GB2452327B (en) * | 2007-09-01 | 2010-02-03 | Rolls Royce Plc | A cooled component |
EP2143883A1 (de) | 2008-07-10 | 2010-01-13 | Siemens Aktiengesellschaft | Turbinenschaufel und entsprechender Gusskern |
JP2011085084A (ja) | 2009-10-16 | 2011-04-28 | Ihi Corp | タービン翼 |
EP2378073A1 (en) | 2010-04-14 | 2011-10-19 | Siemens Aktiengesellschaft | Blade or vane for a turbomachine |
EP2426317A1 (de) * | 2010-09-03 | 2012-03-07 | Siemens Aktiengesellschaft | Turbinenschaufel für eine Gasturbine |
US8506252B1 (en) * | 2010-10-21 | 2013-08-13 | Florida Turbine Technologies, Inc. | Turbine blade with multiple impingement cooling |
US9546554B2 (en) * | 2012-09-27 | 2017-01-17 | Honeywell International Inc. | Gas turbine engine components with blade tip cooling |
US8936067B2 (en) * | 2012-10-23 | 2015-01-20 | Siemens Aktiengesellschaft | Casting core for a cooling arrangement for a gas turbine component |
WO2015020806A1 (en) * | 2013-08-05 | 2015-02-12 | United Technologies Corporation | Airfoil trailing edge tip cooling |
WO2015116338A1 (en) | 2014-01-30 | 2015-08-06 | United Technologies Corporation | Trailing edge cooling pedestal configuration for a gas turbine engine airfoil |
US10053988B2 (en) * | 2015-12-10 | 2018-08-21 | General Electric Company | Article and method of forming an article |
-
2016
- 2016-10-24 WO PCT/US2016/058361 patent/WO2017164935A1/en active Application Filing
- 2016-10-24 CN CN201680083937.7A patent/CN108779678B/zh active Active
- 2016-10-24 JP JP2018549889A patent/JP6685425B2/ja active Active
- 2016-10-24 EP EP16880177.7A patent/EP3417153A1/en active Pending
- 2016-10-24 US US16/086,226 patent/US11193378B2/en active Active
Also Published As
Publication number | Publication date |
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CN108779678A (zh) | 2018-11-09 |
WO2017164935A1 (en) | 2017-09-28 |
US20200291787A1 (en) | 2020-09-17 |
CN108779678B (zh) | 2021-05-28 |
JP2019512641A (ja) | 2019-05-16 |
US11193378B2 (en) | 2021-12-07 |
EP3417153A1 (en) | 2018-12-26 |
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