JP6093441B2 - 翼冷却回路 - Google Patents
翼冷却回路 Download PDFInfo
- Publication number
- JP6093441B2 JP6093441B2 JP2015515109A JP2015515109A JP6093441B2 JP 6093441 B2 JP6093441 B2 JP 6093441B2 JP 2015515109 A JP2015515109 A JP 2015515109A JP 2015515109 A JP2015515109 A JP 2015515109A JP 6093441 B2 JP6093441 B2 JP 6093441B2
- Authority
- JP
- Japan
- Prior art keywords
- cooling circuit
- blade
- shallow
- sectional shape
- wing
- 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
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow 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
- 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
- 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
- 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
- F05D2200/00—Mathematical features
- F05D2200/20—Special functions
-
- 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
- F05D2210/00—Working fluids
- F05D2210/40—Flow geometry or direction
-
- 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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
11 長手方向軸
12 ファン組立体
13 コアガスタービンエンジン
14 高圧圧縮機
16 燃焼器
18 高圧タービン
20 低圧タービン
21 第1ロータシャフト
22 第2ロータシャフト
24 ファンブレード
25 流線型スピナ
26 ロータディスク
28 吸気側
30 排気側
32 多段ブースタ圧縮機
34 スプリッタ
36 シュラウド
40 バイパスダクト
50 第1部分
52 第2部分
60 ファンフレーム組立体
70 出口案内ベーン
80 翼
81 内部空洞
82 内部空洞
83 外皮膜冷却孔
P 圧力側領域
S 吸入側領域
Claims (18)
- ガスタービンエンジン(13)用の翼の冷却回路であって、
複数の内部空洞(82)を備えており、
前記複数の内部空洞(82)のうちの2以上の内部空洞は、浅裂部を備える浅裂断面形状を有し、
前記浅裂断面形状を有する内部空洞の全ての前記浅裂部がそれぞれ、前記翼の1の外面側のみに向けて設けられている、翼の冷却回路。 - 前記浅裂断面形状はそれぞれ、一般超形状方程式によって特徴付けられる、請求項1に記載の翼の冷却回路。
- 極座標形式における前記一般超形状方程式は、次式
- 前記複数の内部空洞(82)のうち少なくとも1つが、2つの平行辺及び2つの半円形対向端からなる断面形状を有する、請求項1乃至3のいずれか1項に記載の翼の冷却回路。
- 前記浅裂断面形状は、翼弦方向に規定されている、請求項1乃至4のいずれか1項に記載の翼の冷却回路。
- 前記冷却回路は、蛇行冷却回路である、請求項1乃至5のいずれか1項に記載の翼の冷却回路。
- 少なくとも1つの前記浅裂断面形状が、2以上の前記浅裂部によって2より多い裂片を有する、請求項1乃至6のいずれか1項に記載の翼の冷却回路。
- 前記浅裂断面形状を有する内部空洞は、それぞれが異なる数の裂片を有する浅裂断面形状を有する、請求項1乃至7のいずれか1項に記載の翼の冷却回路。
- 前記内部空洞(82)の少なくとも1つは、翼(80)の表面上に冷却空気を排出するための少なくとも1つの外皮膜冷却孔(83)を備えている、請求項1乃至8のいずれか1項に記載の翼の冷却回路。
- ガスタービンエンジン(13)用の翼(80)であって、
前記翼(80)の外面および前記外面の内側の前記翼(80)の内部を画定する翼表面と、
前記翼(80)の前記内部に前記翼(80)の前記外面における冷却孔を通って冷却空気を供給する冷却回路と、
を備えており、
前記冷却回路は、各々が浅裂部を備える浅裂断面形状を有する複数の内部空洞(82)を有し、
前記浅裂断面形状を有する内部空洞の全ての前記浅裂部がそれぞれ、前記翼の1の外面側のみに向けて設けられている、翼(80)。 - 前記浅裂断面形状はそれぞれ、一般超形状方程式によって特徴付けられる、請求項10に記載の翼(80)。
- 極座標形式における前記一般超形状方程式は、次式
- 前記複数の内部空洞(82)のうち少なくとも1つが、2つの平行辺及び2つの半円形対向端からなる断面形状を有する、請求項10乃至12のいずれか1項に記載の翼(80)。
- 前記浅裂断面形状は、翼弦方向に規定されている、請求項10乃至13のいずれか1項に記載の翼(80)。
- 前記冷却回路は、蛇行冷却回路である、請求項10乃至14のいずれか1項に記載の翼(80)。
- 少なくとも1つの前記断面形状が、2より多い裂片を有する、請求項10乃至の15いずれか1項に記載の翼(80)。
- 前記裂断面形状を有する内部空洞は、それぞれが異なる数の裂片を有する、請求項10乃至16のいずれか1項に記載の翼(80)。
- 前記内部空洞(82)の少なくとも1つは、前記翼表面上に冷却空気を排出するための少なくとも1つの外皮膜冷却孔(83)を備えている、請求項10乃至17のいずれか1項に記載の翼(80)。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261653681P | 2012-05-31 | 2012-05-31 | |
US61/653,681 | 2012-05-31 | ||
PCT/US2013/042837 WO2013181132A1 (en) | 2012-05-31 | 2013-05-28 | Airfoil cooling circuit and corresponding airfoil |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2015518937A JP2015518937A (ja) | 2015-07-06 |
JP6093441B2 true JP6093441B2 (ja) | 2017-03-08 |
Family
ID=48626139
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015515109A Expired - Fee Related JP6093441B2 (ja) | 2012-05-31 | 2013-05-28 | 翼冷却回路 |
Country Status (7)
Country | Link |
---|---|
US (1) | US20150110611A1 (ja) |
EP (1) | EP2867474A1 (ja) |
JP (1) | JP6093441B2 (ja) |
CN (1) | CN104603399B (ja) |
BR (1) | BR112014028875A2 (ja) |
CA (1) | CA2874618A1 (ja) |
WO (1) | WO2013181132A1 (ja) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201314222D0 (en) | 2013-08-08 | 2013-09-25 | Rolls Royce Plc | Aerofoil |
US10364681B2 (en) * | 2015-10-15 | 2019-07-30 | General Electric Company | Turbine blade |
US10519779B2 (en) * | 2016-03-16 | 2019-12-31 | General Electric Company | Radial CMC wall thickness variation for stress response |
US10683762B2 (en) | 2016-07-12 | 2020-06-16 | Rolls-Royce North American Technologies Inc. | Gas engine component with cooling passages in wall |
US10808571B2 (en) | 2017-06-22 | 2020-10-20 | Raytheon Technologies Corporation | Gaspath component including minicore plenums |
CN112401865B (zh) * | 2020-11-11 | 2024-05-17 | 中国科学技术大学 | 基于超形状的电阻抗成像方法 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1350424A (en) * | 1971-07-02 | 1974-04-18 | Rolls Royce | Cooled blade for a gas turbine engine |
FR2678318B1 (fr) * | 1991-06-25 | 1993-09-10 | Snecma | Aube refroidie de distributeur de turbine. |
JP3651490B2 (ja) * | 1993-12-28 | 2005-05-25 | 株式会社東芝 | タービン冷却翼 |
US6206638B1 (en) * | 1999-02-12 | 2001-03-27 | General Electric Company | Low cost airfoil cooling circuit with sidewall impingement cooling chambers |
US7620527B1 (en) * | 1999-05-10 | 2009-11-17 | Johan Leo Alfons Gielis | Method and apparatus for synthesizing and analyzing patterns utilizing novel “super-formula” operator |
US6599092B1 (en) * | 2002-01-04 | 2003-07-29 | General Electric Company | Methods and apparatus for cooling gas turbine nozzles |
US6808367B1 (en) * | 2003-06-09 | 2004-10-26 | Siemens Westinghouse Power Corporation | Cooling system for a turbine blade having a double outer wall |
US6832889B1 (en) * | 2003-07-09 | 2004-12-21 | General Electric Company | Integrated bridge turbine blade |
GB0418906D0 (en) * | 2004-08-25 | 2004-09-29 | Rolls Royce Plc | Internally cooled aerofoils |
GB0909255D0 (en) * | 2009-06-01 | 2009-07-15 | Rolls Royce Plc | Cooling arrangements |
US8818771B2 (en) * | 2010-06-21 | 2014-08-26 | Johan Gielis | Computer implemented tool box systems and methods |
-
2013
- 2013-05-28 JP JP2015515109A patent/JP6093441B2/ja not_active Expired - Fee Related
- 2013-05-28 US US14/399,572 patent/US20150110611A1/en not_active Abandoned
- 2013-05-28 CN CN201380028607.4A patent/CN104603399B/zh active Active
- 2013-05-28 BR BR112014028875A patent/BR112014028875A2/pt not_active IP Right Cessation
- 2013-05-28 EP EP13728882.5A patent/EP2867474A1/en not_active Withdrawn
- 2013-05-28 WO PCT/US2013/042837 patent/WO2013181132A1/en active Application Filing
- 2013-05-28 CA CA2874618A patent/CA2874618A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP2867474A1 (en) | 2015-05-06 |
CN104603399A (zh) | 2015-05-06 |
CA2874618A1 (en) | 2013-12-05 |
CN104603399B (zh) | 2017-01-18 |
JP2015518937A (ja) | 2015-07-06 |
US20150110611A1 (en) | 2015-04-23 |
BR112014028875A2 (pt) | 2017-08-08 |
WO2013181132A1 (en) | 2013-12-05 |
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