JPWO2021193628A5 - - Google Patents
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- Publication number
- JPWO2021193628A5 JPWO2021193628A5 JP2022510544A JP2022510544A JPWO2021193628A5 JP WO2021193628 A5 JPWO2021193628 A5 JP WO2021193628A5 JP 2022510544 A JP2022510544 A JP 2022510544A JP 2022510544 A JP2022510544 A JP 2022510544A JP WO2021193628 A5 JPWO2021193628 A5 JP WO2021193628A5
- Authority
- JP
- Japan
- Prior art keywords
- cooling passage
- trailing edge
- suction
- pin fins
- pressure
- 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.)
- Granted
Links
- 238000001816 cooling Methods 0.000 claims description 63
- 238000005192 partition Methods 0.000 claims description 29
- 239000007787 solid Substances 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 claims description 5
- 238000003754 machining Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 3
- 239000011295 pitch Substances 0.000 claims 10
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2020053739 | 2020-03-25 | ||
| JP2020053739 | 2020-03-25 | ||
| PCT/JP2021/011983 WO2021193628A1 (ja) | 2020-03-25 | 2021-03-23 | タービン翼及びこのタービン翼を製造する方法 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JPWO2021193628A1 JPWO2021193628A1 (https=) | 2021-09-30 |
| JPWO2021193628A5 true JPWO2021193628A5 (https=) | 2022-08-05 |
| JP7258226B2 JP7258226B2 (ja) | 2023-04-14 |
Family
ID=77892205
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2022510544A Active JP7258226B2 (ja) | 2020-03-25 | 2021-03-23 | タービン翼及びこのタービン翼を製造する方法 |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US11713683B2 (https=) |
| JP (1) | JP7258226B2 (https=) |
| KR (1) | KR102734894B1 (https=) |
| CN (1) | CN114761667B (https=) |
| DE (1) | DE112021000160B4 (https=) |
| WO (1) | WO2021193628A1 (https=) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR102734896B1 (ko) * | 2020-03-25 | 2024-11-26 | 미츠비시 파워 가부시키가이샤 | 터빈 날개 |
| CN115013087B (zh) * | 2022-07-28 | 2026-03-31 | 中国联合重型燃气轮机技术有限公司 | 透平护环和燃气轮机 |
| CN116398253B (zh) * | 2023-03-03 | 2026-04-07 | 华中科技大学 | 一种涡轮叶片尾缘冷却结构及涡轮叶片 |
| CN119282036B (zh) * | 2024-10-12 | 2025-09-16 | 中国航发北京航空材料研究院 | 一种用于衡量空心叶片内腔扰流柱结构再结晶倾向的陶瓷型芯及其使用方法 |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE755567A (fr) | 1969-12-01 | 1971-02-15 | Gen Electric | Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe |
| JPS4826086A (https=) | 1971-08-04 | 1973-04-05 | ||
| JPS5023504U (https=) * | 1973-06-26 | 1975-03-17 | ||
| JPS5023504A (https=) | 1973-06-29 | 1975-03-13 | ||
| GB1564608A (en) * | 1975-12-20 | 1980-04-10 | Rolls Royce | Means for cooling a surface by the impingement of a cooling fluid |
| JPS58197402A (ja) * | 1982-05-14 | 1983-11-17 | Hitachi Ltd | ガスタ−ビン翼 |
| JPH0756201B2 (ja) * | 1984-03-13 | 1995-06-14 | 株式会社東芝 | ガスタービン翼 |
| JPH0240001A (ja) | 1988-07-29 | 1990-02-08 | Hitachi Ltd | ガスタービン冷却翼 |
| JPH07293204A (ja) * | 1994-04-27 | 1995-11-07 | Mitsubishi Heavy Ind Ltd | ガスタービン冷却翼 |
| JPH0828205A (ja) * | 1994-07-20 | 1996-01-30 | Hitachi Ltd | ガスタービン静翼 |
| US6824359B2 (en) | 2003-01-31 | 2004-11-30 | United Technologies Corporation | Turbine blade |
| US8182203B2 (en) | 2009-03-26 | 2012-05-22 | Mitsubishi Heavy Industries, Ltd. | Turbine blade and gas turbine |
| JP5107463B2 (ja) * | 2009-05-11 | 2012-12-26 | 三菱重工業株式会社 | タービン静翼およびガスタービン |
| 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 |
| US9695696B2 (en) * | 2013-07-31 | 2017-07-04 | General Electric Company | Turbine blade with sectioned pins |
| EP3047108B8 (en) * | 2013-09-17 | 2021-03-31 | Raytheon Technologies Corporation | Airfoil assembly formed of high temperature-resistant material |
| US9803488B2 (en) | 2014-01-29 | 2017-10-31 | United Technologies Corporation | Turbine vane cooling arrangement |
| US10208605B2 (en) * | 2015-10-15 | 2019-02-19 | General Electric Company | Turbine blade |
| US10487664B2 (en) * | 2015-11-09 | 2019-11-26 | General Electric Company | Additive manufacturing method for making holes bounded by thin walls in turbine components |
| US10443397B2 (en) * | 2016-08-12 | 2019-10-15 | General Electric Company | Impingement system for an airfoil |
| US10436048B2 (en) * | 2016-08-12 | 2019-10-08 | General Electric Comapny | Systems for removing heat from turbine components |
| JP2020053739A (ja) | 2018-09-25 | 2020-04-02 | シャープ株式会社 | 端末装置、および、方法 |
| CN110320002B (zh) * | 2019-07-31 | 2021-05-25 | 中国航发沈阳发动机研究所 | 一种在冰风洞内控制通道型构件来流参数的装置 |
-
2021
- 2021-03-23 DE DE112021000160.4T patent/DE112021000160B4/de active Active
- 2021-03-23 WO PCT/JP2021/011983 patent/WO2021193628A1/ja not_active Ceased
- 2021-03-23 US US17/778,228 patent/US11713683B2/en active Active
- 2021-03-23 JP JP2022510544A patent/JP7258226B2/ja active Active
- 2021-03-23 CN CN202180006737.2A patent/CN114761667B/zh active Active
- 2021-03-23 KR KR1020227016864A patent/KR102734894B1/ko active Active
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