US2024010493A1PendingUtilityA1
Thermal Reactor Comprising a Gas Permeable Cage Arranged to Influence a Flow Path of Gas
Est. expiryJan 19, 2041(~14.5 yrs left)· nominal 20-yr term from priority
C01B 21/40C01B 21/203C01B 21/20C01B 21/38C01B 21/30
45
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Claims
Abstract
There is provided a method for the synthesis of nitrogen oxides (NOx) comprising the steps of providing a gas mixture comprising oxygen and nitrogen; and heating the gas mixture to a temperature of at least 2300 K at a pressure of 10-100 bar in a thermal reactor forming a gas mixture comprising NOx. There is also provided a method for the production of HNO3.
Claims
exact text as granted — not AI-modified1 . A thermal reactor ( 100 ) comprising:
a vessel ( 101 ), said vessel comprising: a gas inlet ( 102 ),
a gas permeable cage ( 104 ) arranged in the vessel ( 101 ), and in fluid connection to the gas inlet ( 102 ), wherein the vessel ( 101 ) and the cage ( 104 ) are provided with a mutual gas outlet ( 103 ), and
temperature generating means ( 105 ; 105 ′) arranged to create a thermal reaction zone ( 106 ) within the cage ( 104 ),
wherein the cage ( 104 ) is provided with holes ( 107 ), and
wherein a first subset of the holes ( 107 ′) is arranged along at least a portion of a first circumferential surface ( 110 ) of the cage ( 104 ) and a second subset of the holes ( 107 ″) is arranged along at least a portion of a second circumferential surface ( 111 ) of the cage ( 104 ),
wherein the first ( 110 ) and second ( 111 ) circumferential surfaces are offset and non-parallel,
and the first subset of holes ( 107 ′) and the second subset of holes ( 107 ″) are mutually distinct.
2 . The thermal reactor according to claim 1 , wherein the thermal reactor ( 100 ) is a plasma reactor ( 100 ), the thermal reaction zone is a plasma zone ( 106 ) and the temperature generating means ( 105 ; 105 ′) are plasma generating means ( 105 ; 105 ′).
3 . The thermal reactor according to claims 1 , wherein the vessel ( 101 ) is a pressurized vessel arranged to operate at different pressure than atmospheric pressure.
4 . The thermal reactor according to claim 1 , wherein the vessel ( 101 ) further comprises cooling means ( 108 ).
5 . The thermal reactor according to claim 4 , wherein the cooling means ( 108 ) are arranged in the outlet ( 103 ) or in direct connection to the outlet ( 103 ).
6 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) is porous.
7 . The thermal reactor according claim 1 , wherein the cage ( 104 ) is a metal cage.
8 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) is a ceramic cage.
9 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) is made of a non-metallic conductive material.
10 . The thermal reactor according to claim 1 , wherein the temperature generating means ( 105 ; 105 ′) are electrodes.
11 . The thermal reactor according to claim 1 , wherein the temperature generating means ( 105 ; 105 ′) are antennas.
12 . The thermal reactor according to claim 1 , wherein the thermal reaction zone ( 106 ) is produced using electromagnetic waves of radio frequency or microwaves.
13 . The thermal reactor according to claim 1 , wherein at least 80% of the holes ( 107 ), such as at least 90% of the holes ( 107 ), have a central axis (Y) that is angled at an angle a being between 80°-100° relative to a tangential plane (X) at an outer surface of the cage around respective hole ( 107 ).
14 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) has rounded edges.
15 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) is an ellipsoid.
16 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) is a cylinder.
17 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) has a central longitudinal axis around which the cage ( 104 ) is symmetrical.
18 . The thermal reactor according to claim 1 , wherein the surface geometry of the cage ( 104 ) can be described by a continuous function.
19 . The thermal reactor according to claim 18 , wherein the derivative of the continuous function describing the surface geometry of the cage ( 104 ) is a continuous function.
20 . The thermal reactor according to claim 19 , wherein the second derivative of the continuous function describing the surface geometry of the cage ( 104 ) is a continuous function.
21 . The thermal reactor according to claim 1 , wherein at least 30%, such as at least 40%, such as at least 50%, such as at least 60%, such as at least 70%, such as at least 80%, such as at least 90%, of the surface of the cage ( 104 ) is provided with holes ( 107 ).
22 . The thermal reactor according to claim 21 , wherein the entire surface of the cage ( 104 ) is provided with holes ( 107 ).
23 . The thermal reactor according to claim 1 , wherein the holes ( 107 ) are substantially circular.
24 . The thermal reactor according to claim 1 , wherein the cage ( 104 ) is spaced from the walls of the vessel ( 101 ).
25 . The thermal reactor according to claim 1 , wherein the gas permeable cage ( 104 ) is a first gas permeable cage ( 104 - 1 ) and the thermal reactor further comprises:
a second gas permeable cage ( 104 - 2 ), wherein the holes ( 107 ) of the first gas permeable cage ( 104 - 1 ) are first holes ( 107 - 1 ), and the second gas permeable cage ( 104 - 2 ) is provided second holes ( 107 - 2 ), wherein the second gas permeable cage ( 104 - 2 ) is smaller than the first gas permeable cage ( 104 - 1 ), so that the second gas permeable cage ( 104 - 2 ) is arranged inside the first gas permeable cage ( 104 - 1 ).
26 . The thermal reactor according to claim 25 , wherein the first and second holes ( 107 - 1 , 107 - 2 ) of the first and second gas permeable cages ( 104 - 1 , 104 - 2 ) are arranged offset so that the first and second holes ( 107 - 1 , 107 - 2 ) are not aligned.
27 . The thermal reactor according to claim 25 , wherein the first gas permeable cage ( 104 - 1 ) and the second gas permeable cage ( 104 - 2 ) have the same geometrical shape.Join the waitlist — get patent alerts
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