CN108367329B - 用于自定义npr特性和改善的冷却性能的以工程化图案具有成角度的狭槽的拉胀结构 - Google Patents
用于自定义npr特性和改善的冷却性能的以工程化图案具有成角度的狭槽的拉胀结构 Download PDFInfo
- Publication number
- CN108367329B CN108367329B CN201680012297.0A CN201680012297A CN108367329B CN 108367329 B CN108367329 B CN 108367329B CN 201680012297 A CN201680012297 A CN 201680012297A CN 108367329 B CN108367329 B CN 108367329B
- Authority
- CN
- China
- Prior art keywords
- elongated holes
- elongated
- top surface
- npr
- holes
- 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
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/002—Wall structures
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/04—Air inlet arrangements
- F23R3/06—Arrangement of apertures along the flame tube
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00005—Preventing fatigue failures or reducing mechanical stress in gas turbine components
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/03041—Effusion cooled combustion chamber walls or domes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US201562101840P | 2015-01-09 | 2015-01-09 | |
| US62/101,840 | 2015-01-09 | ||
| US201562118826P | 2015-02-20 | 2015-02-20 | |
| US62/118,826 | 2015-02-20 | ||
| PCT/US2016/012769 WO2016112368A1 (en) | 2015-01-09 | 2016-01-09 | Auxetic structures with angled slots in engineered patterns for customized npr behavior and improved cooling performance |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108367329A CN108367329A (zh) | 2018-08-03 |
| CN108367329B true CN108367329B (zh) | 2021-04-09 |
Family
ID=56356521
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201680012297.0A Active CN108367329B (zh) | 2015-01-09 | 2016-01-09 | 用于自定义npr特性和改善的冷却性能的以工程化图案具有成角度的狭槽的拉胀结构 |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20180274783A1 (enExample) |
| EP (1) | EP3242758B1 (enExample) |
| JP (1) | JP2018508738A (enExample) |
| CN (1) | CN108367329B (enExample) |
| CA (1) | CA2973378A1 (enExample) |
| RU (1) | RU2017126597A (enExample) |
| WO (1) | WO2016112368A1 (enExample) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2018504557A (ja) * | 2015-01-09 | 2018-02-15 | プレジデント アンド フェローズ オブ ハーバード カレッジ | Npr挙動と改善された応力性能を提供するための、工学設計によるパターンで変形した投影スロットを有するオーゼティック構造体 |
| US11536174B2 (en) | 2017-07-20 | 2022-12-27 | President And Fellows Of Harvard College | Acoustic damper for gas turbine combustors with orthogonal slots |
| CN111299402A (zh) * | 2019-11-29 | 2020-06-19 | 湖南飞沃新能源科技股份有限公司 | 一种热墩生产线 |
| CN115621608A (zh) * | 2022-09-21 | 2023-01-17 | 南京航空航天大学 | 一种基于开闭孔负泊松比胞元混合排列的防护与散热结构 |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
| US7546737B2 (en) * | 2006-01-24 | 2009-06-16 | Honeywell International Inc. | Segmented effusion cooled gas turbine engine combustor |
| US20110059291A1 (en) * | 2009-09-07 | 2011-03-10 | Boyce Christopher M | Structured materials with tailored isotropic and anisotropic poisson's ratios including negative and zero poisson's ratios |
| GB201105790D0 (en) * | 2011-04-06 | 2011-05-18 | Rolls Royce Plc | A cooled double walled article |
| FR2979416B1 (fr) * | 2011-08-26 | 2013-09-20 | Turbomeca | Paroi de chambre de combustion |
| WO2014151045A1 (en) * | 2013-03-15 | 2014-09-25 | President And Fellows Of Harvard College | Low porosity auxetic sheet |
| US9709274B2 (en) * | 2013-03-15 | 2017-07-18 | Rolls-Royce Plc | Auxetic structure with stress-relief features |
| US9353783B2 (en) * | 2013-03-15 | 2016-05-31 | Rolls-Royce Canada, Ltd. | Auxetic locking pin |
-
2016
- 2016-01-09 CA CA2973378A patent/CA2973378A1/en not_active Abandoned
- 2016-01-09 RU RU2017126597A patent/RU2017126597A/ru not_active Application Discontinuation
- 2016-01-09 CN CN201680012297.0A patent/CN108367329B/zh active Active
- 2016-01-09 EP EP16735531.2A patent/EP3242758B1/en active Active
- 2016-01-09 JP JP2017555433A patent/JP2018508738A/ja active Pending
- 2016-01-09 US US15/542,636 patent/US20180274783A1/en not_active Abandoned
- 2016-01-09 WO PCT/US2016/012769 patent/WO2016112368A1/en not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| WO2016112368A1 (en) | 2016-07-14 |
| EP3242758A4 (en) | 2018-07-18 |
| RU2017126597A3 (enExample) | 2019-06-04 |
| CN108367329A (zh) | 2018-08-03 |
| JP2018508738A (ja) | 2018-03-29 |
| EP3242758B1 (en) | 2019-09-11 |
| US20180274783A1 (en) | 2018-09-27 |
| RU2017126597A (ru) | 2019-02-11 |
| EP3242758A1 (en) | 2017-11-15 |
| CA2973378A1 (en) | 2016-07-14 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |