GAS-TIGHT, HEAT-PERMEABLE MULTILAYER CERAMIC COMPOSITE TUBE
20220152584 · 2022-05-19
Inventors
- Grigorios Kolios (Ludwigshafen, DE)
- Heinrich Laib (Ludwigshafen, DE)
- Frederik SCHEIFF (Ludwigshafen, DE)
- Bernd Zoels (Ludwigshafen, DE)
- Matthias Kern (Ludwigshafen, DE)
Cpc classification
C04B2235/5228
CHEMISTRY; METALLURGY
B01D69/02
PERFORMING OPERATIONS; TRANSPORTING
B32B2597/00
PERFORMING OPERATIONS; TRANSPORTING
C01B32/05
CHEMISTRY; METALLURGY
C04B2235/9607
CHEMISTRY; METALLURGY
B01D2325/22
PERFORMING OPERATIONS; TRANSPORTING
B01D67/0041
PERFORMING OPERATIONS; TRANSPORTING
C01B3/34
CHEMISTRY; METALLURGY
C01C3/02
CHEMISTRY; METALLURGY
C04B2237/704
CHEMISTRY; METALLURGY
C01B2203/0283
CHEMISTRY; METALLURGY
B01D2325/02
PERFORMING OPERATIONS; TRANSPORTING
C01B2203/0238
CHEMISTRY; METALLURGY
C04B2237/84
CHEMISTRY; METALLURGY
B32B18/00
PERFORMING OPERATIONS; TRANSPORTING
F16L9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C01B2203/0233
CHEMISTRY; METALLURGY
C04B2237/64
CHEMISTRY; METALLURGY
C04B2237/586
CHEMISTRY; METALLURGY
B01D69/12
PERFORMING OPERATIONS; TRANSPORTING
Y02P20/141
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F16L9/14
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B3/30
PERFORMING OPERATIONS; TRANSPORTING
International classification
B01D69/02
PERFORMING OPERATIONS; TRANSPORTING
B01D69/12
PERFORMING OPERATIONS; TRANSPORTING
B01J35/00
PERFORMING OPERATIONS; TRANSPORTING
B32B18/00
PERFORMING OPERATIONS; TRANSPORTING
B32B3/30
PERFORMING OPERATIONS; TRANSPORTING
C01B32/05
CHEMISTRY; METALLURGY
C01C3/02
CHEMISTRY; METALLURGY
F16L9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Described herein is a gaslight multilayered composite tube having a heat transfer coefficient of >500 W/m.sup.2/K which in its construction over the cross section of the wall of the composite tube includes as an inner layer a nonporous monolithic oxide ceramic surrounded by an outer layer of oxidic fiber composite ceramic, where this outer layer has an open porosity of 5%<ε<50%, and which on the inner surface of the composite tube includes a plurality of depressions oriented towards the outer wall of the composite tube. Also described herein is a method of using the multilayered composite tube as a reaction tube for endothermic reactions, jet tubes, flame tubes or rotary tubes.
Claims
1. A multilayered composite tube having a heat transfer coefficient of >500 W/m.sup.2/K comprising at least two layers which in its construction over the cross section of the wall of the composite tube comprises as an inner layer a zero-open-porosity monolithic oxide ceramic surrounded by an outer layer of oxidic fiber composite ceramic, wherein this outer layer has an open porosity ε of 5%<ε<50%, and which on the inner surface of the composite tube comprises a plurality of depressions oriented towards the outer wall of the composite tube.
2. The composite tube according to claim 1, wherein the thermal shock resistance according to DIN EN 993-11 of the composite tube is greater than 50 K/h.
3. The composite tube according to claim 1, wherein the depressions have a depth of 0.5 mm to 2 mm.
4. The composite tube according to claim 1, wherein the depressions are uniformly distributed over the inner surface of the composite tube.
5. The composite tube according to claim 1, wherein the depressions are nonuniformly distributed over the inner surface of the composite tube.
6. The composite tube according to claim 1, wherein the inner surface of the composite tube is provided with depressions to an extent of 10% to 95% based on the total inner surface of the composite tube.
7. The composite tube according to claim 1, wherein the depressions are concave.
8. The composite tube according to claim 1, wherein the depressions have a construction that is circular in cross section and have a diameter of 2 mm to 30 mm.
9. The composite tube according to claim 1, wherein the total wall thickness of the composite tube is 0.5 mm to 50 mm.
10. The composite tube according to claim 1, wherein the tube internal diameter of the composite tube is 10 mm to 1000 mm.
11. The composite tube according to claim 1, wherein the employed oxidic fiber composite ceramic is SiC/Al.sub.2O.sub.3, SiC/mullite, C/Al.sub.2O.sub.3, C/mullite, Al.sub.2O.sub.3/Al.sub.2O.sub.3, Al.sub.2O.sub.3/mullite, mullite/Al.sub.2O.sub.3 and/or mullite/mullite.
12. The composite tube according to claim 1, wherein the composite tube contains two layers, including an inner layer and an outer layer, wherein the inner layer is constructed from nonporous monolithic oxide ceramic and the outer layer is constructed from oxidic fiber composite ceramic.
13. The composite tube according to claim 1, wherein the composite tube has a structure in which the nonporous monolithic oxide ceramic is covered by oxidic fiber composite ceramic.
14. The composite tube according to claim 1, wherein the inner layer has a minimum layer thickness of 0.5 mm to 45 mm.
15. A method of using the composite tube according to claim 1, the method comprising using the composite tube in the production of synthesis gas by reforming of hydrocarbons with steam and/or carbon dioxide, coproduction of hydrogen and pyrolysis carbon by pyrolysis of hydrocarbons, production of hydrocyanic acid from methane and ammonia or from propane and ammonia, production of olefins by steamcracking of hydrocarbons and/or coupling of methane to ethylene, acetylene and to benzene.
16. A method of using the composite tube according to claim 1, the method comprising using the composite tube as a reaction tube in reactors with axial temperature control, countercurrent reactors, membrane reactors, jet tubes, flame tubes and/or rotary tubes for rotary tube furnaces.
17. A process for producing the multilayered composite tube according to claim 1, the process comprising impressing the depressions by pressing processes.
18. The composite tube according to claim 1, wherein the outer layer has an open porosity ε of 10%<ε<30%.
Description
EXAMPLE 1: COMPARISON OF TEMPERATURE DISTRIBUTION ON AN INVENTIVE MULTILAYERED COMPOSITE TUBE WITH DEPRESSIONS AND A MULTILAYERED COMPOSITE TUBE WITHOUT DEPRESSIONS
[0151] The temperature distribution in a steam-conducting tube was determined by numerical simulation (CFD=computational fluid dynamics). In this example a 1 m-long multilayered ceramic composite tube of 0.047 m internal diameter and tube wall thicknesses of 4 mm for the monolithic ceramic and 1.5 mm for the fiber ceramic were simulated.
[0152] The following table 3 shows the properties of the tube materials employed here.
TABLE-US-00003 Fiber Metal Material data at 900° C. Al.sub.2O.sub.3 ceramic tube ρ (density, kg/m3) 2800 2900 7600 c.sub.p (specific heat capacity, J/kgK) 900 900 663 λ (thermal conductivity, W/mK) 706.1*T’.sup.(−0.672) 58.9*T’.sup.(−0.479) 24 T’ = local temperature in ° C.
[0153] In addition to a tube with inventive depressions a tube of identical structure without depressions was simulated. In the tube with depressions 8 depressions per circumferential segment with a radius of in each case 13.8 mm and a displaced arrangement in the axial direction with a distance of 12.5 mm between the centers of the depressions were modelled.
[0154] An entry temperature of the fluid of 750° C., a mass flow of 8 kg/s and a constant outer tube wall temperature of 950° C. were specified in the simulation.
[0155] The results of the simulation are shown in
EXAMPLE 2: COMPARISON OF THE TEMPERATURE DISTRIBUTION ON AN INVENTIVE MULTILAYERED COMPOSITE TUBE WITH DEPRESSIONS AND A METALLIC TUBE (MATERIAL S+C CENTRALLOY® HT-E) WITH DEPRESSIONS
[0156] In a second example the above inventive multilayered composite tube with depressions was compared to a geometrically identical metallic tube with depressions. The results of the simulation are shown in