FR2133041A5 - Pierced refractory plate prodn - for radiant heaters - Google Patents
Pierced refractory plate prodn - for radiant heatersInfo
- Publication number
- FR2133041A5 FR2133041A5 FR7112159A FR7112159A FR2133041A5 FR 2133041 A5 FR2133041 A5 FR 2133041A5 FR 7112159 A FR7112159 A FR 7112159A FR 7112159 A FR7112159 A FR 7112159A FR 2133041 A5 FR2133041 A5 FR 2133041A5
- Authority
- FR
- France
- Prior art keywords
- plate
- mould
- pierced
- ceramic
- radiant heaters
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B28—WORKING CEMENT, CLAY, OR STONE
- B28B—SHAPING CLAY OR OTHER CERAMIC COMPOSITIONS; SHAPING SLAG; SHAPING MIXTURES CONTAINING CEMENTITIOUS MATERIAL, e.g. PLASTER
- B28B7/00—Moulds; Cores; Mandrels
- B28B7/34—Moulds, cores, or mandrels of special material, e.g. destructible materials
- B28B7/342—Moulds, cores, or mandrels of special material, e.g. destructible materials which are at least partially destroyed, e.g. broken, molten, before demoulding; Moulding surfaces or spaces shaped by, or in, the ground, or sand or soil, whether bound or not; Cores consisting at least mainly of sand or soil, whether bound or not
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Mechanical Engineering (AREA)
- Gas Burners (AREA)
Abstract
A ceramic plate pierced with a number of holes across the plate to permit flow of gaseous fuel for the burner, is produced by a method in which a horizontal mould plate is surmounted with a number of projections of material fusible or vaporisable at below the firing temp. of the ceramic, vertical mould plates of height appropriate to the thickness of ceramic plate required are placed or fastened around the horizontal plate, and a refractory ceramic casting slip is poured into the mould and allowed to set. The assembly is then dried and fired in the mould, when the needles melt or vaporise away leaving holes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7112159A FR2133041A5 (en) | 1971-04-06 | 1971-04-06 | Pierced refractory plate prodn - for radiant heaters |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7112159A FR2133041A5 (en) | 1971-04-06 | 1971-04-06 | Pierced refractory plate prodn - for radiant heaters |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2133041A5 true FR2133041A5 (en) | 1972-11-24 |
Family
ID=9074845
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7112159A Expired FR2133041A5 (en) | 1971-04-06 | 1971-04-06 | Pierced refractory plate prodn - for radiant heaters |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2133041A5 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2286258A1 (en) * | 1974-09-25 | 1976-04-23 | Asakura Kensuke | PROCESS FOR DEMOLITION OF A CONSTRUCTION AND APPARATUS FOR ITS IMPLEMENTATION |
FR2852003A1 (en) * | 2003-03-04 | 2004-09-10 | Snecma Propulsion Solide | Production of a multi-perforated component in a composite material with a ceramic base involves the insertion and elimination of pins in a consolidated fibrous preformer, notably for the combustion chamber of a jet engine |
-
1971
- 1971-04-06 FR FR7112159A patent/FR2133041A5/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2286258A1 (en) * | 1974-09-25 | 1976-04-23 | Asakura Kensuke | PROCESS FOR DEMOLITION OF A CONSTRUCTION AND APPARATUS FOR ITS IMPLEMENTATION |
FR2852003A1 (en) * | 2003-03-04 | 2004-09-10 | Snecma Propulsion Solide | Production of a multi-perforated component in a composite material with a ceramic base involves the insertion and elimination of pins in a consolidated fibrous preformer, notably for the combustion chamber of a jet engine |
US7238247B2 (en) | 2003-03-04 | 2007-07-03 | Snecma Propulsion Solide | Method of making a multi-perforated part out of ceramic matrix composite material |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |