WO1999054660A1 - Modular ceramic combustion reactor - Google Patents
Modular ceramic combustion reactor Download PDFInfo
- Publication number
- WO1999054660A1 WO1999054660A1 PCT/HU1999/000028 HU9900028W WO9954660A1 WO 1999054660 A1 WO1999054660 A1 WO 1999054660A1 HU 9900028 W HU9900028 W HU 9900028W WO 9954660 A1 WO9954660 A1 WO 9954660A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- connection
- segments
- reactor according
- reactor
- plates
- Prior art date
Links
- 239000000919 ceramic Substances 0.000 title claims abstract description 30
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 25
- 230000014759 maintenance of location Effects 0.000 claims description 9
- 229910010293 ceramic material Inorganic materials 0.000 claims description 5
- 230000000979 retarding effect Effects 0.000 claims description 4
- 230000000284 resting effect Effects 0.000 claims 1
- 239000000463 material Substances 0.000 description 14
- 238000004519 manufacturing process Methods 0.000 description 11
- 239000007789 gas Substances 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 230000035882 stress Effects 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000007373 indentation Methods 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 238000005266 casting Methods 0.000 description 1
- 230000003197 catalytic effect Effects 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000003779 heat-resistant material Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 229910052573 porcelain Inorganic materials 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C3/00—Combustion apparatus characterised by the shape of the combustion chamber
- F23C3/002—Combustion apparatus characterised by the shape of the combustion chamber the chamber having an elongated tubular form, e.g. for a radiant tube
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
- F23M2900/00—Special features of, or arrangements for combustion chambers
- F23M2900/05004—Special materials for walls or lining
Definitions
- the invention relates to a ceramic combustion reactor.
- the reactor of the invention has a tubular body, consisting of modules.
- the modules are fixed to each other with rigid connection means.
- US patent No 5,041,268 discloses a combustion reactor having an elongated tubular body.
- the tubular body is enclosed in a steel outer shell. During the combustion process, the tubular body is heated up to high temperatures. Only materials which are suitably heat-resistant can be considered as materials for the tubular body of this type of reactor.
- this special type of reactor is a complete combustion reactor. It has been found that the reactor type disclosed in the US patent No. 5,041,268 performs best if the wall of the tubular body is relatively thin, preferably less than 10 mm, so that the heat generated in the combustion process is quickly dissipated through intense IR radiation of the tubular wall.
- US patent No. 4,416,619 discloses a ceramic combustion reactor with a tubular body, which is used in a heating system.
- the combustion is not on the inside, but on the outside of the reactor.
- the outer surface of the reactor has a plurality of indentations to break up the surface continuity. Thereby the heat- induced stresses in the ceramics material are substantially reduced, and scaling and cracking of the surface is prevented.
- this reactor is of a small size only, and therefor the problem of size need not be solved.
- Ceramics ovens and kilns for the burning of clay and porcelain are known in the art. These ceramics ovens are usually constructed of several blocks of ceramics, which are encased by a steel frame or box. In these known ovens the blocks constituting the walls of the oven are very thick, and are therefore self- supporting. But due to the thickness of the walls, this structure in not practical for the inner combustion reactor, because the generated heat can not dissipate through the thick walls.
- US patent No. 5,687,572 teaches a thin wall combustor with backside impingement cooling.
- This combustor is used for a gas turbine engine having a thin-walled nonporous ceramic liner whose backside is impingement cooled.
- the ceramic shell is supported by a porous outer metallic shell. This cooling is necessary in order to protect the outer metallic shell from the high temperatures.
- the necessity of the cooling system makes this type of ceramic shell unusable in the complete combustion reactor, because the clean burning process needs the presence of the high temperature walls, where the catalytic oxidation and reduction of the combustion products takes place.
- a reactor consisting of drum-shaped modules connected by rigid connection means, where the drum- shaped modules are comprising several segments together forming a drum-shaped module, the segments and/or the modules are connected together by connection means.
- connection means are comprising connection plates and connection clamps, where a, the connection plates are positioned on the segments in the vicinity of the corners of the segments and extending radially outwards, and b, the connection clamps are provided with at least one recess receiving at least two connection plates.
- connection plates and/or the connection clamps are provided with retention means for preventing the connection clamps from falling off from the connection plates.
- the retention means may be made of ceramic pins, which are insertable into openings in the connection plate and the connection clamp.
- connection clamps comprise co-operating flanges on the edge of the connection plates and in the recess of the connection clamps.
- connection plates and/or the connection clamps are made of ceramic material. It has been found that one drum-shaped module may consist of as much as eight segments, but smaller numbers are also applicable. As a general rule, fewer segments are sufficient for smaller reactors, while reactors with larger diameters may require the use of more segments.
- the tubular reactor body comprises a cone-shaped flame- retarding insert.
- This insert is of principal importance for the proper functioning of those complete combustion reactors which are disclosed in the US patent no. 5,041,268, among others.
- the insert is provided with radially extending supports, and the segments of at least one module being provided with recesses receiving the supports of the insert.
- connection clamp is provided with two symmetric recesses, each recess receiving two connection plates of two neighbouring segments.
- one connection clamp is holding together four segments at their corners, so the number of connection clamps used may be kept low.
- connection clamp is provided with stiffening ribs. It has been found most practical if the connection plates are integral with the segments.
- FIG. 1. is a perspective view of the reactor in the preferred embodiment of the invention
- FIG. 2a-c is a perspective, side, and front view of a segment in the center modules of the reactor of Fig. 1, - 5 -
- FIG. 3a-c is a perspective, side, and front view of a segment in the top module of the reactor of Fig. 1
- FIG. 4a-d is a perspective, an upside-down perspective, side, and top view of a connection clamp used as connection means for the reactor of Fig. 1
- Fig. 4e is top view of a modified connection clamp used as connection means for certain parts of the reactor of Fig. 1
- FIG. 5a-d is a perspective, side, top, and front view of a retention pin for the connection clamp of Figs. 4a-e
- FIG. 6 is another perspective view of the reactor in the preferred embodiment of the invention, with two segments taken away for showing the interior of the reactor with the flame retardation insert in position
- Fig. 7 is a perspective view of a modified embodiment of the cone-shaped insert used in the modules of a reactor having a similar structure to that shown in Fig. 1
- Fig. 8 is a cross-section of a further reactor module made of universal segments.
- Fig. 1 shows a perspective view of the reactor 1 of the invention.
- This reactor is a so-called complete combustion reactor. Smaller versions of this reactor are manufactured by the RCWO Complete Combustion Reactor Bureau Ltd. of
- the reactor 1 in Fig. 1 depicts a larger version, which consist of two drum-shaped center modules 2 and one top module 3. The modules 2 and 3 are fixed to each other with rigid connection means 5. On the right side, a top module 3 having a domed end 31 is visible. The reactor 1 is supported on the U-shaped rail 9, which receives the connection means 5 on the underside of the reactor 1. The reactor also comprises a bottom module, which is not shown in Fig.
- the segments 6 and 61 are made of high-grade ceramics, usually a silica-based compound.
- the bottom module need not tolerate such high temperatures as the other modules, hence it may be manufactured of high-grade steel, but ceramics may also be used as material for the bottom module.
- connection means 5 are comprising connection plates 51 (see also Fig. 2 and 3) and connection clamps 52 (see also Fig. 4.).
- the connection plates 51 are positioned on the segments 6 and 61 in the vicinity of the corners 53 of the segments 6 and 61.
- the connection plates 51 are extending radially outwards, so that the plane of the touching surface 62 of the connection plates 51 is containing the central axis of the reactor 1.
- the connection plates 51 are integral with the segments, and they have the same thickness as the thickness of the wall of the segments. As it is best seen in Figs.
- connection plates are formed as a part of a wide edge 65, which is blushed out" on the straight sides of the segments, perpendicularly to the arched wall of the segments 6 and 61. Comparing Figs. 2a and 3a, it is also clear that the segments 6 and 61 have an almost identical construction, except for the domed end 31 on the segments 61. The form of the domed end 31 plays an important part in forming the proper turbulence conditions within the cavity of the reactor 1.
- One arched side of the segment 6 and 61 comprise an arched band 66, which forms a part of an annular ring 10 when the segments are assembled into a tubular body.
- the ring 10 has a larger inner diameter than the outer diameter of the drum modules 20. When the modules 20 are assembled into the tubular body, the rings 10 overlap the edges 1 1 of the segments 6.
- connection clamps 52 are provided with at least one recess 54 receiving two connection plates 51.
- the connection plates 51 and/or the connection clamps 52 are provided with retention means 7.
- the retention means 7 comprise ceramic pins - 7 -
- connection plate 70 which are insertable into openings 55 in the connection plate 51 and the connection clamp 52.
- the ceramic pins 70 are provided with oval end-plates 71.
- the openings 55 on the connection plates 51 and the connection clamps 52 are shaped oval, so that their size and shape corresponds to the oval end-plates. After insertion into the oval openings, the retention pins 70 are rotated 90°, so that the oval end-plates 71 will keep the retention pins 70 from falling out.
- connection means 5 comprise flanges 56 on the edge of the connection plates 51, and co-operating flanges 57 in the recess 54 of the connection clamps 52. It is the flanges 56 and 57 which provide the connecting force between the modules 20 and the segments 6 and 61.
- the dimensions of the parts constituting the connection means 5, especially the flanges, are made somewhat loosely, in order to leave room for some dilatation or displacement of the different parts. This dilatation is necessary, due to the differences in the thermal expansion and the rigidity of the ceramics material.
- the pins 70 are also allowed to move sideways in the oval openings 55, and thus allow some degree of displacement of the segments 6 and 61 relative to the other segments in the adjoining module. This arrangement prevents the thermally induced mechanical stresses between adjoining modules 2 and 3. It must be noted that the relative movement between the segments must not be too large either. Since there is no sealing between the segments and modules, small gaps are unavoidable. The efficiency of the combustion process within the reactor will decrease if too much of the gases escape through the gaps between the modules or segments.
- connection means 5 Due to the high thermal load on the tubular body of a complete combustion reactor, the connection means 5 must be made of a heat-resistant material. It has been found best if the connection plates 51 and/or the connection clamps 52 are made of ceramic material, preferably with identical or similar properties to the ceramic material of the reactor. Especially, the suggested material for the segments is high- - 8 - grade SiSiC. This is an expensive type of ceramics, but it is heat resistant until 1800 C°. An alternative material for the segments is SiC, which is slightly cheaper, but may be used only for combustion temperatures below 1300 C°.
- the suggested material for the connection clamps is Corderite, which is cheap to manufacture by pressing. Corderite is also preferred because it slightly more resilient, and therefor less likely to break under stress.
- connection clamps from SiC or SiSiC as well.
- connection clamps made of Corderite are fully acceptable. It is also more economical, because larger quantities are cheaper to manufacture by pressing.
- SiC and SiSiC need expensive die- fabrication procedures. The invention therefore provides the important advantage, that broken parts of a reactor 1 may be replaced easily, without the expense of replacing the entire reactor. Alternatively, the segments may be manufactured of Corderite as well, if the combustion process is kept at relatively low temperatures.
- connection clamp 52 is provided with two symmetric recesses 54. Each recess 54 receives two connection plates 51 of two neighbouring segment 6 or 61 , i. e. one connection clamp 52 connects four segments 6 or 61 at their corners.
- Fig. 4e shows a connection clamp 52', which has only one recess 54.
- the connection clamp 52' is practically one half of a connection clamp 52, and it is used for connecting the connection plates 51 ' adjacent to the domed end 31 part of the segments 61.
- the bottom module (not shown), or a support plate of the bottom module is equipped with similar connection plates as the connection plates 51, and therefore may be fixed to the adjoining drum-shaped module 2 by ordinary connection clamps 52.
- the recess 54 of a connection clamp 52 and 52' is formed as an elongated slit.
- the slit receives two connection plates 51 with appropriate tolerance, so that the connection clamp 52 may slide smoothly on the connection plates 51 , without being too tight or too loose.
- the elongated slit has an arrow-like cross section. The widening at the head of the arrow forms the flange 56, which engages the flange 57 of the connection plate 51.
- stiffening ribs 58 To improve the mechanical - 9 - strength of the connection clamps 52, they are equipped with stiffening ribs 58.
- the underside of the clamp is provided with a recess 59, which leaves room for band 66 forming the ring 10.
- one drum-shaped module consists of two to eight segments. From a designing and manufacturing point of view, even numbers are preferred, but there is nothing preventing the manufacturing of modules consisting of three, five, seven or even greater number of segments within one module.
- a speciality of the complete combustion reactor is a a cone-shaped flame-retarding insert 8.
- This insert is shown in Fig. 6.
- the insert 8 divides the reactor cavity into two chambers.
- the special turbulence caused by the insert 8 increases the efficiency of the reactor, and produces a complete, soot-free burning of the fuel.
- the segments 6 of at least one module 2 or 3 are provided with recesses 81 receiving the supports 80 of the insert 8.
- all segments 6 and 61 are provided with the recesses 81, as it is shown in Fig. 1 and Fig. 6.
- the recesses 81 are created by two indentations 82 on the walls of the segments.
- the supports 80 are integral with the cone of the insert 8.
- the supports of the flame-retarding insert 8 are provided with separate supports (not shown). The separate supports are properly attached to the cone by one end, and the other end or the separate supports are inserted into the recess 81 of the segments. In this case the separate supports have corresponding recesses in the cone of the insert 8.
- the separate supports of the insert are constructed as hollow rods, where the hole of the rod receives pins extending from the cone insert on one end and pins extending from the segments towards the cone on the other end.
- the recesses receiving the supports 80 are formed between the connection plates of the segments.
- Fig. 7 shows a further advantageous realisation of the cone-shaped flame retarding insert 8.
- the insert 8 is also integral with the supports 83, similar to the embodiment in Fig. 6, but here the supports 83 have an annular or U-shaped cross section.
- the insert 8 and the supports 83 are cast together.
- This type of insert 8 is especially suitable for use in reactors combined with gas turbines, where the gas pressure on the cone of the insert 8 is much greater. This is an important application, because the gas turbines are used for the burning of low cost fuels and waste.
- the hollow support structure is able to prevent the breaking of the supports even in the presence of minor casting faults. This specific embodiment is shown with reference to a segment 61 for a top module 3, but the very same construction may be realised on the segments 6 as well.
- Fig. 8 illustrates how larger modules with different diameters may be constructed using the same type of universally applicable segments.
- a reactor module 90 which is made up of eight segments 91. Actually, only four or six segments 91 would constitute a perfect circular module, depending on the design of the universal segment 91. However, with appropriately designed connecting means, more segments 91 may be connected to form a module with larger diameter. (It must be noted that smaller modules still must be made of two to four segments)
- the segments 91 are designed so that any number (in practice at least four) thereof may be connected together to form modules with different diameters. In this manner modules with a flower-like cross section are created, as shown in Fig. 8.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Ceramic Engineering (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
- Muffle Furnaces And Rotary Kilns (AREA)
- Ceramic Products (AREA)
- Solid-Sorbent Or Filter-Aiding Compositions (AREA)
- Devices And Processes Conducted In The Presence Of Fluids And Solid Particles (AREA)
- Gas Burners (AREA)
Abstract
Description
Claims
Priority Applications (10)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL13903399A IL139033A0 (en) | 1998-04-17 | 1999-04-16 | Modular ceramic composition reactor |
KR1020007011535A KR20010042792A (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
CA002328717A CA2328717A1 (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
EP99915963A EP1080326A1 (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
SK1540-2000A SK15402000A3 (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
UA2000105841A UA54589C2 (en) | 1998-04-17 | 1999-04-16 | Ceramic combustion reactor with complete burning |
JP2000544966A JP2002512355A (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
AU34375/99A AU3437599A (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
NO20005134A NO320092B1 (en) | 1998-04-17 | 2000-10-12 | Modules ceramic combustion reactor |
HK02100599.3A HK1042335A1 (en) | 1998-04-17 | 2002-04-15 | Modular ceramic combustion reactor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HU9800902A HUP9800902A1 (en) | 1998-04-17 | 1998-04-17 | Modular ceramic combustion reactor |
HUP9800902 | 1998-04-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1999054660A1 true WO1999054660A1 (en) | 1999-10-28 |
Family
ID=89996442
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/HU1999/000028 WO1999054660A1 (en) | 1998-04-17 | 1999-04-16 | Modular ceramic combustion reactor |
Country Status (16)
Country | Link |
---|---|
EP (1) | EP1080326A1 (en) |
JP (1) | JP2002512355A (en) |
KR (1) | KR20010042792A (en) |
CN (1) | CN1305575A (en) |
AU (1) | AU3437599A (en) |
CA (1) | CA2328717A1 (en) |
CZ (1) | CZ300872B6 (en) |
HK (1) | HK1042335A1 (en) |
HU (1) | HUP9800902A1 (en) |
IL (1) | IL139033A0 (en) |
NO (1) | NO320092B1 (en) |
PL (1) | PL192179B1 (en) |
SK (1) | SK15402000A3 (en) |
UA (1) | UA54589C2 (en) |
WO (1) | WO1999054660A1 (en) |
ZA (1) | ZA200005672B (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020060188A1 (en) * | 2018-09-19 | 2020-03-26 | 한국생산기술연구원 | Modular pressurized pure oxy-fuel combustion apparatus and control method therefor |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2015161428A1 (en) * | 2014-04-22 | 2015-10-29 | 朱宏锋 | Stove having segmented burner |
CN116412419A (en) * | 2021-12-30 | 2023-07-11 | 中国科学院宁波材料技术与工程研究所 | Modularized combustion cavity |
CN114484504A (en) * | 2022-01-19 | 2022-05-13 | 中国航发沈阳发动机研究所 | Flame tube easy to repair |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2940245A1 (en) * | 1979-10-04 | 1981-04-16 | Brown, Boveri & Cie Ag, 6800 Mannheim | Flame tube for industrial furnace radiant-heating tube - is highly heat-resistant ceramic lattice frame with more conductive ceramic in openings |
EP0534104A2 (en) * | 1991-09-27 | 1993-03-31 | WS Wärmeprozesstechnik GmbH | Radiant tube with jacket |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1551762B1 (en) * | 1967-08-17 | 1972-03-09 | Aichelin Fa J | Flame tube for a radiant heating tube of an industrial furnace |
DE2314118C2 (en) * | 1973-03-21 | 1979-10-11 | Fa. J. Aichelin, 7015 Korntal | Flame tube for a jacket radiant heating tube of an industrial furnace |
US5687572A (en) * | 1992-11-02 | 1997-11-18 | Alliedsignal Inc. | Thin wall combustor with backside impingement cooling |
-
1998
- 1998-04-17 HU HU9800902A patent/HUP9800902A1/en unknown
-
1999
- 1999-04-16 CA CA002328717A patent/CA2328717A1/en not_active Abandoned
- 1999-04-16 UA UA2000105841A patent/UA54589C2/en unknown
- 1999-04-16 CN CN99807483A patent/CN1305575A/en active Pending
- 1999-04-16 JP JP2000544966A patent/JP2002512355A/en active Pending
- 1999-04-16 AU AU34375/99A patent/AU3437599A/en not_active Abandoned
- 1999-04-16 IL IL13903399A patent/IL139033A0/en unknown
- 1999-04-16 SK SK1540-2000A patent/SK15402000A3/en unknown
- 1999-04-16 WO PCT/HU1999/000028 patent/WO1999054660A1/en not_active Application Discontinuation
- 1999-04-16 KR KR1020007011535A patent/KR20010042792A/en not_active Application Discontinuation
- 1999-04-16 PL PL343568A patent/PL192179B1/en not_active IP Right Cessation
- 1999-04-16 CZ CZ20003816A patent/CZ300872B6/en not_active IP Right Cessation
- 1999-04-16 EP EP99915963A patent/EP1080326A1/en not_active Withdrawn
-
2000
- 2000-10-12 ZA ZA200005672A patent/ZA200005672B/en unknown
- 2000-10-12 NO NO20005134A patent/NO320092B1/en unknown
-
2002
- 2002-04-15 HK HK02100599.3A patent/HK1042335A1/en unknown
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2940245A1 (en) * | 1979-10-04 | 1981-04-16 | Brown, Boveri & Cie Ag, 6800 Mannheim | Flame tube for industrial furnace radiant-heating tube - is highly heat-resistant ceramic lattice frame with more conductive ceramic in openings |
EP0534104A2 (en) * | 1991-09-27 | 1993-03-31 | WS Wärmeprozesstechnik GmbH | Radiant tube with jacket |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020060188A1 (en) * | 2018-09-19 | 2020-03-26 | 한국생산기술연구원 | Modular pressurized pure oxy-fuel combustion apparatus and control method therefor |
Also Published As
Publication number | Publication date |
---|---|
ZA200005672B (en) | 2001-12-04 |
NO320092B1 (en) | 2005-10-24 |
HK1042335A1 (en) | 2002-08-09 |
HUP9800902A1 (en) | 2000-02-28 |
SK15402000A3 (en) | 2001-05-10 |
HU9800902D0 (en) | 1998-06-29 |
NO20005134L (en) | 2000-10-12 |
PL192179B1 (en) | 2006-09-29 |
CZ20003816A3 (en) | 2001-12-12 |
JP2002512355A (en) | 2002-04-23 |
CA2328717A1 (en) | 1999-10-28 |
AU3437599A (en) | 1999-11-08 |
KR20010042792A (en) | 2001-05-25 |
CZ300872B6 (en) | 2009-09-02 |
EP1080326A1 (en) | 2001-03-07 |
CN1305575A (en) | 2001-07-25 |
PL343568A1 (en) | 2001-08-27 |
NO20005134D0 (en) | 2000-10-12 |
UA54589C2 (en) | 2003-03-17 |
IL139033A0 (en) | 2001-11-25 |
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