Gas-tight, heat-permeable multilayer ceramic composite tube

Patent metadata

Field	Value
Publication number	US-2022152584-A1
Application number	US-202017439540-A
Country	US
Kind code	A1
Filing date	Mar 6, 2020
Priority date	Mar 15, 2019
Publication date	May 19, 2022
Grant date	—

Abstract

Described herein is a gaslight multilayered composite tube having a heat transfer coefficient of >500 W/m2/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.

First claim

1 . A multilayered composite tube having a heat transfer coefficient of >500 W/m 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 2 O 3 , SiC/mullite, C/Al 2 O 3 , C/mullite, Al 2 O 3 /Al 2 O 3 , Al 2 O 3 /mullite, mullite/Al 2 O 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%.

Assignees

• Basf Se

Inventors

• Kolios Grigorios
• Laib Heinrich
• Scheiff Frederik
• Zoels Bernd
• Kern Matthias

Classifications

• C04B2237/58

  Forming a gradient in composition or in properties across the laminate or the joined articles · CPC title

• C04B2237/365

  Silicon carbide · CPC title

• C04B2237/363

  Carbon · CPC title

• B01D71/024

  Oxides · CPC title

• B01D71/021

  Carbon · CPC title