GB2384046B - A double wall combuster tile arrangement - Google Patents
A double wall combuster tile arrangementInfo
- Publication number
- GB2384046B GB2384046B GB0200778A GB0200778A GB2384046B GB 2384046 B GB2384046 B GB 2384046B GB 0200778 A GB0200778 A GB 0200778A GB 0200778 A GB0200778 A GB 0200778A GB 2384046 B GB2384046 B GB 2384046B
- Authority
- GB
- United Kingdom
- Prior art keywords
- combuster
- double wall
- tile arrangement
- tile
- arrangement
- 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
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
-
- 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)
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0200778A GB2384046B (en) | 2002-01-15 | 2002-01-15 | A double wall combuster tile arrangement |
| US10/330,329 US20030145604A1 (en) | 2002-01-15 | 2002-12-30 | Double wall combustor tile arrangement |
| US10/880,463 US20050034399A1 (en) | 2002-01-15 | 2004-07-01 | Double wall combustor tile arrangement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB0200778A GB2384046B (en) | 2002-01-15 | 2002-01-15 | A double wall combuster tile arrangement |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB0200778D0 GB0200778D0 (en) | 2002-03-06 |
| GB2384046A GB2384046A (en) | 2003-07-16 |
| GB2384046B true GB2384046B (en) | 2005-07-06 |
Family
ID=9929059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB0200778A Expired - Fee Related GB2384046B (en) | 2002-01-15 | 2002-01-15 | A double wall combuster tile arrangement |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20030145604A1 (en) |
| GB (1) | GB2384046B (en) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP1312865A1 (en) * | 2001-11-15 | 2003-05-21 | Siemens Aktiengesellschaft | Gas turbine annular combustion chamber |
| DE10214570A1 (en) * | 2002-04-02 | 2004-01-15 | Rolls-Royce Deutschland Ltd & Co Kg | Mixed air hole in gas turbine combustion chamber with combustion chamber shingles |
| US7464554B2 (en) * | 2004-09-09 | 2008-12-16 | United Technologies Corporation | Gas turbine combustor heat shield panel or exhaust panel including a cooling device |
| US7954325B2 (en) * | 2005-12-06 | 2011-06-07 | United Technologies Corporation | Gas turbine combustor |
| GB2444947B (en) * | 2006-12-19 | 2009-04-08 | Rolls Royce Plc | Wall elements for gas turbine engine components |
| US20100095679A1 (en) * | 2008-10-22 | 2010-04-22 | Honeywell International Inc. | Dual wall structure for use in a combustor of a gas turbine engine |
| US20100095680A1 (en) * | 2008-10-22 | 2010-04-22 | Honeywell International Inc. | Dual wall structure for use in a combustor of a gas turbine engine |
| US8161752B2 (en) * | 2008-11-20 | 2012-04-24 | Honeywell International Inc. | Combustors with inserts between dual wall liners |
| US8739404B2 (en) | 2010-11-23 | 2014-06-03 | General Electric Company | Turbine components with cooling features and methods of manufacturing the same |
| US9068748B2 (en) | 2011-01-24 | 2015-06-30 | United Technologies Corporation | Axial stage combustor for gas turbine engines |
| US8479521B2 (en) | 2011-01-24 | 2013-07-09 | United Technologies Corporation | Gas turbine combustor with liner air admission holes associated with interspersed main and pilot swirler assemblies |
| US9958162B2 (en) | 2011-01-24 | 2018-05-01 | United Technologies Corporation | Combustor assembly for a turbine engine |
| GB201114745D0 (en) * | 2011-08-26 | 2011-10-12 | Rolls Royce Plc | Wall elements for gas turbine engines |
| JP5821550B2 (en) * | 2011-11-10 | 2015-11-24 | 株式会社Ihi | Combustor liner |
| GB201222311D0 (en) * | 2012-12-12 | 2013-01-23 | Rolls Royce Plc | A combusiton chamber |
| GB201303057D0 (en) * | 2013-02-21 | 2013-04-03 | Rolls Royce Plc | A combustion chamber |
| CA2904200A1 (en) * | 2013-03-05 | 2014-09-12 | Rolls-Royce Corporation | Dual-wall impingement, convection, effusion combustor tile |
| US20160025010A1 (en) * | 2013-03-26 | 2016-01-28 | United Technologies Corporation | Turbine engine and turbine engine component with cooling pedestals |
| WO2015002686A2 (en) * | 2013-06-14 | 2015-01-08 | United Technologies Corporation | Gas turbine engine combustor liner panel |
| GB201322838D0 (en) | 2013-12-23 | 2014-02-12 | Rolls Royce Plc | A combustion chamber |
| CN106605101A (en) * | 2014-07-30 | 2017-04-26 | 西门子公司 | Multiple feed platefins within a hot gas path cooling system in a combustor basket in a combustion turbine engine |
| US20160258623A1 (en) * | 2015-03-05 | 2016-09-08 | United Technologies Corporation | Combustor and heat shield configurations for a gas turbine engine |
| US10480787B2 (en) | 2015-03-26 | 2019-11-19 | United Technologies Corporation | Combustor wall cooling channel formed by additive manufacturing |
| US10386067B2 (en) * | 2016-09-15 | 2019-08-20 | United Technologies Corporation | Wall panel assembly for a gas turbine engine |
| JP6737895B2 (en) * | 2016-11-11 | 2020-08-12 | 川崎重工業株式会社 | Combustor liner |
| CA3047746A1 (en) * | 2018-12-20 | 2020-06-20 | Pratt & Whitney Canada Corp. | Stand-off device for double-skin combustor liner |
| GB202000870D0 (en) | 2020-01-21 | 2020-03-04 | Rolls Royce Plc | A combustion chamber, a combustion chamber tile and a combustion chamber segment |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2298267A (en) * | 1995-02-23 | 1996-08-28 | Rolls Royce Plc | An arrangement of heat resistant tiles for a gas turbine engine combustor |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2087065B (en) * | 1980-11-08 | 1984-11-07 | Rolls Royce | Wall structure for a combustion chamber |
| FR2646880A1 (en) * | 1989-05-11 | 1990-11-16 | Snecma | THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR |
| US5259758A (en) * | 1992-11-25 | 1993-11-09 | Wisconsin Oven Corporation | Industrial oven with expandable surfaces |
| US5289677A (en) * | 1992-12-16 | 1994-03-01 | United Technologies Corporation | Combined support and seal ring for a combustor |
| GB9926257D0 (en) * | 1999-11-06 | 2000-01-12 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
| GB2361303B (en) * | 2000-04-14 | 2004-10-20 | Rolls Royce Plc | Wall structure for a gas turbine engine combustor |
-
2002
- 2002-01-15 GB GB0200778A patent/GB2384046B/en not_active Expired - Fee Related
- 2002-12-30 US US10/330,329 patent/US20030145604A1/en not_active Abandoned
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2298267A (en) * | 1995-02-23 | 1996-08-28 | Rolls Royce Plc | An arrangement of heat resistant tiles for a gas turbine engine combustor |
Also Published As
| Publication number | Publication date |
|---|---|
| GB0200778D0 (en) | 2002-03-06 |
| US20030145604A1 (en) | 2003-08-07 |
| GB2384046A (en) | 2003-07-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20090115 |