BE705251A - - Google Patents
Info
- Publication number
- BE705251A BE705251A BE705251DA BE705251A BE 705251 A BE705251 A BE 705251A BE 705251D A BE705251D A BE 705251DA BE 705251 A BE705251 A BE 705251A
- Authority
- BE
- Belgium
Links
Classifications
-
- 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
- F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US618455A US3408812A (en) | 1967-02-24 | 1967-02-24 | Cooled joint construction for combustion wall means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BE705251A true BE705251A (US07655688-20100202-C00086.png) | 1968-03-01 |
Family
ID=24477769
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BE705251D BE705251A (US07655688-20100202-C00086.png) | 1967-02-24 | 1967-10-17 |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3408812A (US07655688-20100202-C00086.png) |
| BE (1) | BE705251A (US07655688-20100202-C00086.png) |
| DE (1) | DE1601571A1 (US07655688-20100202-C00086.png) |
Families Citing this family (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3751910A (en) * | 1972-02-25 | 1973-08-14 | Gen Motors Corp | Combustion liner |
| US3854285A (en) * | 1973-02-26 | 1974-12-17 | Gen Electric | Combustor dome assembly |
| US4077205A (en) * | 1975-12-05 | 1978-03-07 | United Technologies Corporation | Louver construction for liner of gas turbine engine combustor |
| US4184326A (en) * | 1975-12-05 | 1980-01-22 | United Technologies Corporation | Louver construction for liner of gas turbine engine combustor |
| US4527397A (en) * | 1981-03-27 | 1985-07-09 | Westinghouse Electric Corp. | Turbine combustor having enhanced wall cooling for longer combustor life at high combustor outlet gas temperatures |
| US4407205A (en) * | 1982-04-30 | 1983-10-04 | Beaufrere Albert H | Regeneratively cooled coal combustor/gasifier with integral dry ash removal |
| US4944151A (en) * | 1988-09-26 | 1990-07-31 | Avco Corporation | Segmented combustor panel |
| US5129447A (en) * | 1991-05-20 | 1992-07-14 | United Technologies Corporation | Cooled bolting arrangement |
| JP2597800B2 (ja) * | 1992-06-12 | 1997-04-09 | ゼネラル・エレクトリック・カンパニイ | ガスタービンエンジン用燃焼器 |
| US5261223A (en) * | 1992-10-07 | 1993-11-16 | General Electric Company | Multi-hole film cooled combustor liner with rectangular film restarting holes |
| DE4335413A1 (de) * | 1993-10-18 | 1995-04-20 | Abb Management Ag | Verfahren und Vorrichtung zur Kühlung einer Gasturbinenbrennkammer |
| US5596870A (en) * | 1994-09-09 | 1997-01-28 | United Technologies Corporation | Gas turbine exhaust liner with milled air chambers |
| DE10114619B4 (de) * | 2000-03-27 | 2006-07-27 | Cummins Inc., Columbus | Belüftendes Befestigungselement |
| ES2278847T3 (es) * | 2002-08-16 | 2007-08-16 | Siemens Aktiengesellschaft | Tornillo refrigerable interiormente. |
| FR2905166B1 (fr) * | 2006-08-28 | 2008-11-14 | Snecma Sa | Chambre de combustion annulaire d'une turbomachine. |
| GB201222311D0 (en) * | 2012-12-12 | 2013-01-23 | Rolls Royce Plc | A combusiton chamber |
| US20160153282A1 (en) * | 2014-07-11 | 2016-06-02 | United Technologies Corporation | Stress Reduction For Film Cooled Gas Turbine Engine Component |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2794319A (en) * | 1953-03-02 | 1957-06-04 | Westinghouse Electric Corp | Afterburner shell construction |
| US3307354A (en) * | 1965-10-01 | 1967-03-07 | Gen Electric | Cooling structure for overlapped panels |
-
1967
- 1967-02-24 US US618455A patent/US3408812A/en not_active Expired - Lifetime
- 1967-10-17 BE BE705251D patent/BE705251A/xx unknown
- 1967-10-26 DE DE19671601571 patent/DE1601571A1/de active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| DE1601571A1 (de) | 1970-06-18 |
| US3408812A (en) | 1968-11-05 |
