Pyrolytic reactor

Patent metadata

Field	Value
Publication number	US-9737870-B2
Application number	US-201615131316-A
Country	US
Kind code	B2
Filing date	Apr 18, 2016
Priority date	Aug 21, 2012
Publication date	Aug 22, 2017
Grant date	Aug 22, 2017

Abstract

A pyrolytic reactor comprising a fuel injection zone, a combustion zone adjacent to the fuel injections zone, an expansion zone adjacent to the combustion zone, a feedstock injection zone comprising a plurality of injection nozzles and disposed adjacent to the expansion zone, a mixing zone configured to mix a carrier stream and feed material and disposed adjacent to the feedstock injection zone, and a reaction zone adjacent to the mixing zone. The plurality of injection nozzles are radially distributed in a first assembly defining a first plane transverse to the feedstock injection zone and in a second assembly transverse to the feedstock injection zone.

First claim

What is claimed is:

1. A method to produce acetylene, comprising:
introducing a fuel and an oxidizer into a fuel injection zone;
combusting said fuel and said oxidizer in a combustion zone to create a carrier stream;
accelerating the carrier stream to supersonic speed in an expansion zone;
injecting first feedstock material using a first plurality of injection nozzles arranged annularly on a first transverse plane into a feedstock injection zone;
delivering said first feedstock material from each of said first plurality of injection nozzles to a first radial depth within said carrier stream;
injecting second feedstock material using a second plurality of injection nozzles annularly on a second transverse plane of the feedstock injection zone;
delivering said second feedstock material from each of said second plurality of injection nozzles to a second radial depth within said carrier stream; and
wherein a feedstock target radial penetration depth for each nozzle in said first and second plurality of injection nozzles is different from a feedstock target radial penetration depth for all other injection nozzles in said first and second plurality of injection nozzles.

2. The method of claim 1 , further comprising transitioning, in a reaction zone, said carrier stream from supersonic speed to subsonic speed to create a shockwave.

3. The method of claim 1 , further comprising transitioning, in a reaction zone, said carrier stream from supersonic speed to subsonic speed to create a shock train.

4. The method of claim 1 , further comprising reducing a velocity of said carrier stream, in a reaction zone, to convert kinetic energy to thermal energy, while maintaining said velocity above supersonic speed.

5. The method of claim 1 , wherein said first plurality of injection nozzles comprises at least two injection nozzles and said second plurality of injection nozzles comprises at least four injection nozzle.

6. The method of claim 1 , wherein:
said feedstock injection zone has a pipe diameter; and
said first transverse plane is spaced from the second transverse plane by a distance of between about 0.5 to about 5 pipe diameters.

7. The method of claim 1 , wherein said injecting feedstock further comprises:
providing third feedstock material to a third plurality of injection nozzles arranged annularly on a third transverse plane of the feedstock injection zone;
delivering said third feedstock material from each of said third plurality of injection nozzles to a third radial depth within said carrier stream; and
said first transverse plane, said second transverse plane, and said third transverse plane are located within between about 0.5 to about 5 pipe diameters from each other.

8. The method of claim 1 , further comprising introducing steam into said fuel injection zone.

9. The method of claim 1 , wherein the feedstock injection zone comprises an annular cross section.

10. A method to produce acetylene, comprising:
introducing a fuel and an oxidizer into a fuel injection zone;
combusting said fuel and said oxidizer in a combustion zone to create a carrier stream;
accelerating the carrier stream to supersonic speed in an expansion zone;
injecting first feedstock material using a first plurality of injection nozzles arranged annularly on a first transverse plane into a feedstock injection zone;
delivering said first feedstock material from each of said first plurality of injection nozzles to a first radial depth within said carrier stream;
injecting second feedstock material using a second plurality of injection nozzles annularly on a second transverse plane of the feedstock injection zone;
delivering said second feedstock material from each of said second plurality of injection nozzles to a second radial depth within said carrier stream;
injecting third feedstock material using a third plurality of injection nozzles arranged annularly on a third transverse plane of the feedstock injection zone;
delivering said third feedstock material from each of said third plurality of injection nozzles to a third radial depth within said carrier stream; and
said first transverse plane, said second transverse plane, and said third transverse plane are located within between about 0.5 to about 5 pipe diameters from each other.

11. The method of claim 10 , further comprising transitioning, in a reaction zone, said carrier stream from supersonic speed to subsonic speed to create a shockwave.

12. The method of claim 10 , further comprising transitioning, in a reaction zone, said carrier stream from supersonic speed to subsonic speed to create a shock train.

13. The method of claim 10 , further comprising reducing a velocity of said carrier stream, in a reaction zone, to convert kinetic energy to thermal energy, while maintaining said velocity above supersonic speed.

14. The method of claim 10 , wherein said first plurality of injection nozzles comprises at least two injection nozzles and said second plurality of injection nozzles comprises at least four injection nozzle.

15. The method of claim 10 , further comprising introducing steam into said fuel injection zone.

16. The method of claim 10 , wherein the feedstock injection zone comprises an annular cross section.

Assignees

• Uop Llc

Inventors

• Stevens Carl J
• Negiz Antoine
• Kuchana Vinayender

Classifications

• B01J2219/0204

  comprising coatings on the surfaces in direct contact with the reactive components · CPC title

• B01J2219/00094

  Jackets · CPC title

• B01J2219/0263

  Ceramic · CPC title

• B01J4/002

  Nozzle-type elements (nozzle-type reactors B01J19/26) · CPC title

• B01J2219/0286

  Steel · CPC title