JPS57124620A - Combustor - Google Patents
CombustorInfo
- Publication number
- JPS57124620A JPS57124620A JP865581A JP865581A JPS57124620A JP S57124620 A JPS57124620 A JP S57124620A JP 865581 A JP865581 A JP 865581A JP 865581 A JP865581 A JP 865581A JP S57124620 A JPS57124620 A JP S57124620A
- Authority
- JP
- Japan
- Prior art keywords
- heat
- support ring
- insulating plates
- insulating
- legs
- 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.)
- Pending
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
- F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
PURPOSE:To simplify partial replacement of a damaged heat-insulating plate or plates and to cool the heat-insulating plates efficiently, by employing such an arrangement that a multiplicity of legs of the heat-insulating plates are fitted in freely disengageable manner, into through-holes formed in a support ring which is fastened to the outer casing of a gas-turbine combustor by the aid of support means. CONSTITUTION:A support means 2 is arranged in the outer casing of a combustor (not shown) and a flange 7a of a support ring 7 is fixed to the support means 2. The support ring 7 and a retainer plate 8 are formed with substantially 8-shaped through-holes 10, 11 consisting respectively of a large-diameter portion 10a, 11a, and a small-diameter portion 10b, 11b. Further, each of heat-insulating plates 6 are formed with legs 9 consisting of a large-diameter flange portion 9a and a small-diameter shaft portion 9b. The heat-insulating plates 6 are fixed in place by inserting the legs 9 into through- holes 10, 11 formed in the retainer plate 8 and support ring 7, in the manner that the support ring 7 is interposed between the retainer plate 8 and the heat-insulating plates 6. By thus securing the heat-insulating plates 6 to the support ring 7 such that they can be disengaged from the support ring 7 independently from each other, it is enabled to replace only a damaged heat-insulating plate partially.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP865581A JPS57124620A (en) | 1981-01-23 | 1981-01-23 | Combustor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP865581A JPS57124620A (en) | 1981-01-23 | 1981-01-23 | Combustor |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS57124620A true JPS57124620A (en) | 1982-08-03 |
Family
ID=11698941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP865581A Pending JPS57124620A (en) | 1981-01-23 | 1981-01-23 | Combustor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS57124620A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0604021A1 (en) * | 1992-12-21 | 1994-06-29 | United Technologies Corporation | Individually removable combustor liner panel for a gas turbine engine |
EP1413831A1 (en) * | 2002-10-21 | 2004-04-28 | Siemens Aktiengesellschaft | Annular combustor for a gas turbine and gas turbine |
EP2778532A4 (en) * | 2011-11-10 | 2015-07-08 | Ihi Corp | Combustor liner |
EP3372790A1 (en) * | 2017-03-10 | 2018-09-12 | General Electric Company | Component having a hybrid coating system and method for forming a component |
-
1981
- 1981-01-23 JP JP865581A patent/JPS57124620A/en active Pending
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0604021A1 (en) * | 1992-12-21 | 1994-06-29 | United Technologies Corporation | Individually removable combustor liner panel for a gas turbine engine |
EP1413831A1 (en) * | 2002-10-21 | 2004-04-28 | Siemens Aktiengesellschaft | Annular combustor for a gas turbine and gas turbine |
US6938424B2 (en) | 2002-10-21 | 2005-09-06 | Siemens Aktiengesellschaft | Annular combustion chambers for a gas turbine and gas turbine |
EP2778532A4 (en) * | 2011-11-10 | 2015-07-08 | Ihi Corp | Combustor liner |
US10551067B2 (en) | 2011-11-10 | 2020-02-04 | Ihi Corporation | Combustor liner with dual wall cooling structure |
EP3372790A1 (en) * | 2017-03-10 | 2018-09-12 | General Electric Company | Component having a hybrid coating system and method for forming a component |
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