TWI384185B - - Google Patents
Info
- Publication number
- TWI384185B TWI384185B TW98142883A TW98142883A TWI384185B TW I384185 B TWI384185 B TW I384185B TW 98142883 A TW98142883 A TW 98142883A TW 98142883 A TW98142883 A TW 98142883A TW I384185 B TWI384185 B TW I384185B
- Authority
- TW
- Taiwan
Links
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW98142883A TW201120383A (en) | 2009-12-15 | 2009-12-15 | Method of manufacturing combustion chamber of turbo-engine and product thereof. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TW98142883A TW201120383A (en) | 2009-12-15 | 2009-12-15 | Method of manufacturing combustion chamber of turbo-engine and product thereof. |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| TW201120383A TW201120383A (en) | 2011-06-16 |
| TWI384185B true TWI384185B (https=) | 2013-02-01 |
Family
ID=45045136
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TW98142883A TW201120383A (en) | 2009-12-15 | 2009-12-15 | Method of manufacturing combustion chamber of turbo-engine and product thereof. |
Country Status (1)
| Country | Link |
|---|---|
| TW (1) | TW201120383A (https=) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6463620A (en) * | 1987-12-16 | 1989-03-09 | Osborn Norbert L | Compressor housing |
| TW279195B (https=) * | 1993-03-11 | 1996-06-21 | Clark Ind Inc | |
| US5701670A (en) * | 1994-06-23 | 1997-12-30 | Boeing North American, Inc. | Method of making rocket engine combustion chamber utilizing "slide in" port liner |
| TW200502515A (en) * | 2003-05-20 | 2005-01-16 | Snecma Moteurs | A combustion chamber having a flexible connection between a chamber end wall and a chamber side wall |
| US6889496B2 (en) * | 2002-08-12 | 2005-05-10 | Eads Space Transportation Gmbh | Combustion chamber structure and its manufacturing process |
| CN1637248A (zh) * | 2004-01-06 | 2005-07-13 | 通用电气公司 | 减少和/或消除燃烧衬套组件中稀释空气泄漏的装置和方法 |
| CN101307915A (zh) * | 2008-06-24 | 2008-11-19 | 北京航空航天大学 | 一种燃用乙醇燃料的燃气轮机预蒸发燃烧室 |
| CN101551122A (zh) * | 2008-04-03 | 2009-10-07 | 斯奈克玛动力部件公司 | 陶瓷基复合材料制成且细分为多区域的燃气涡轮机燃烧室 |
-
2009
- 2009-12-15 TW TW98142883A patent/TW201120383A/zh not_active IP Right Cessation
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6463620A (en) * | 1987-12-16 | 1989-03-09 | Osborn Norbert L | Compressor housing |
| TW279195B (https=) * | 1993-03-11 | 1996-06-21 | Clark Ind Inc | |
| US5701670A (en) * | 1994-06-23 | 1997-12-30 | Boeing North American, Inc. | Method of making rocket engine combustion chamber utilizing "slide in" port liner |
| US6889496B2 (en) * | 2002-08-12 | 2005-05-10 | Eads Space Transportation Gmbh | Combustion chamber structure and its manufacturing process |
| TW200502515A (en) * | 2003-05-20 | 2005-01-16 | Snecma Moteurs | A combustion chamber having a flexible connection between a chamber end wall and a chamber side wall |
| CN1637248A (zh) * | 2004-01-06 | 2005-07-13 | 通用电气公司 | 减少和/或消除燃烧衬套组件中稀释空气泄漏的装置和方法 |
| CN101551122A (zh) * | 2008-04-03 | 2009-10-07 | 斯奈克玛动力部件公司 | 陶瓷基复合材料制成且细分为多区域的燃气涡轮机燃烧室 |
| CN101307915A (zh) * | 2008-06-24 | 2008-11-19 | 北京航空航天大学 | 一种燃用乙醇燃料的燃气轮机预蒸发燃烧室 |
Also Published As
| Publication number | Publication date |
|---|---|
| TW201120383A (en) | 2011-06-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | Annulment or lapse of patent due to non-payment of fees |