GB1575444A - Producing sulphur dioxide and oxygen from sulphur trioxide - Google Patents

Producing sulphur dioxide and oxygen from sulphur trioxide Download PDF

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Publication number
GB1575444A
GB1575444A GB604577A GB604577A GB1575444A GB 1575444 A GB1575444 A GB 1575444A GB 604577 A GB604577 A GB 604577A GB 604577 A GB604577 A GB 604577A GB 1575444 A GB1575444 A GB 1575444A
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sulfur trioxide
space velocity
reaction
conversion
sulfur dioxide
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GB604577A
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CBS Corp
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Westinghouse Electric Corp
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    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B17/00Sulfur; Compounds thereof
    • C01B17/48Sulfur dioxide; Sulfurous acid
    • C01B17/50Preparation of sulfur dioxide
    • C01B17/501Preparation of sulfur dioxide by reduction of sulfur compounds
    • C01B17/502Preparation of sulfur dioxide by reduction of sulfur compounds of sulfur trioxide
    • CCHEMISTRY; METALLURGY
    • C01INORGANIC CHEMISTRY
    • C01BNON-METALLIC ELEMENTS; COMPOUNDS THEREOF; METALLOIDS OR COMPOUNDS THEREOF NOT COVERED BY SUBCLASS C01C
    • C01B13/00Oxygen; Ozone; Oxides or hydroxides in general
    • C01B13/02Preparation of oxygen
    • C01B13/0203Preparation of oxygen from inorganic compounds

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  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Catalysts (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Exhaust Gas Treatment By Means Of Catalyst (AREA)
  • Oxygen, Ozone, And Oxides In General (AREA)

Description

(54) PRODUCING SULFUR DIOXIDE AND OXYGEN FROM SULFUR TRIOXIDE.
(71) We, WESTINGHOUSE ELECTRIC CORPORATION of Westinghouse Building, Gateway Center, Pittsburgh, Pennsylvania, United States of America, a company organised and existing under the laws of the Commonwealth of Pennsylvania, United States of America, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement: This invention relates to the production of sulfur dioxide and oxygen from sulfur trioxide.
The demands on electric power plants are cyclical, peaking during the day and diminishing during the night. More efficient use can be made of the facilities if power produced in off hours can be stored for use during peak hours.
One way to accomplish this is to use energy produced during the off hours to decompose water into hydrogen and oxygen, producing a clean, easily stored fuel. Many of the processes which decompose water use as one step in the process the decomposition of sulfur trioxide into sulfur dioxide and oxygen. That reaction proceeds without a catalyst but the reaction rate is low and the reaction time is long.
The reduction of sulfur dioxide into sulfur dioxide using magnetite is disclosed in an article titled "The Reduction of Sulfur Trioxide By Constituents Of Boiler Flue Dust" by H. E. Crossley, A. Poll, and F. Swett in The Institute Of Fuel, April 1968, pages 206 to 213.
According to the present invention a method for the net conversion of gaseous sulfur trioxide into sulfur dioxide and oxygen according to the equation 2S03 > 2SO2 + 02 comprises passing said gaseous sulfur trioxide over a sulfuric acid contact catalyst at a temperature of 750 to 10000C at a space velocity (as hereinafter defined) of at least 100 hr-; and preventing sulfur dioxide and oxygen produced from contacting said catalyst at a temperature of less than 750"C.
It has been discovered that sulfuric acid contact catalysts greatly facilitate the decomposition of sulfur trioxide, but only when they are heated to 750 to 1000"C.
Equilibrium conversion of SOX to SO2 and 02 is effected at space velocities of at least 10,000 hr-l which is a relatively high space velocity for equilibrium conversion compared to most chemical reactions.
In order that the invention can be more clearly understood, a convenient embodiment thereof will now be described, by way of example, with reference to the accompanying drawing in which: Figure 1 is a diagram of apparatus for performing the process of this invention.
In Figure 1 liquid S03 from line 1 is heated in evaporator 2 to produce gaseous SO3 in line 3. A valve 4 controls the flow of the gas and a flowmeter 5 measures the flow rate. The gas passes through tube 6 containing sulfuric acid contact catalyst 7, the tube 6 being heated by decomposition reactor 8. In line 9 undecomposed SOX and the SO2 and 02 products move to condenser 10 where the SOB is condensed and returned to evaporator 2 by line 11. The SO, and 02 products continue through line 12 to separator 13 where the SO2 is condensed, separating it from the 02.
Sulfuric acid contact catalysts are a well-known and well-defined group of catalysts.
These are catalysts which catalyze the oxidation of SO2 to SO3 according to the equation 2S02 + 02 < 2S03 This oxidation reaction is conducted.at relatively low temperatures ( < 650 C) because at higher temperatures the yield decreases. We have found that the same catalysts will catalyze the reverse reaction, 2SO3 e 2SO2 + 2, but only in practical yields at temperatures of 750 to 1000"C. Below 750"C the reaction does not proceed at a significant rate and above 1000"C heat is wasted because no significant increase in reaction rate is obtained Thus, the temperature range of 750 to 1000"C is to be regarded as critical in this invention.
Examples of sulfuric acid contact catalysts include Fe2O3, V205, Pt, including finely divided Pt, platinized asbestos, platinized silica gel, and platinized magnesium sulfate, compounds of chromium, especially Cr-Sn-Ba, Cr-Sn-K, and Cr-Sn, iron, and metal oxides such as CrO, WO2, and CuO. The preferred catalysts are V2O5 and Pt (usually on a binder or support) due to their relatively low cost, long life, high reaction rate, and high yield. The catalyst should of course be as finely divided as possible.
It is also very important that the SO2 and 2 product not be permitted to contact the catalyst at a temperature of less than 750"C once they have formed, in order to prevent their recombination.
As shown in the drawing, the undecomposed SO3 can be recovered by condensation. It can also be recovered by the addition of water which reacts with it to produce (liquid) H2SO4. The separation of the SO2 from the oxygen can be accomplished as shown in the drawing by condensation.
A carrier gas, such as water vapor, may be intermixed with the sulfur trioxide as a result of preceding processes. However, preferably no carrier gas is present as heating the carrier is a waste of energy.
) It is necessary that the space velocity be at least 100 hr-l because at lower space velocities an impractically large reaction vessel is required. The space velocity, which is equal to the flow rate divided by the volume of catalyst, is a measurement of the contact time between the sulfur trioxide and the catalyst. Equilibrium conversions at high space velocity means that large quantities of sulfur dioxide can be decomposed quickly in a small vessel. In the process of this invention equilibrium conversion at space velocities of at least 10,000 hr-' are attainable, which is high relative to most chemical processes.
The invention will now be illustrated by the following Example: Example Liquid SO3 was gradually heated to about 51"C in a three necked round bottom flask. At this temperature its vapor pressure was 3 to 5 psig. Gaseous SO3 passed vertically from the flask through a check valve and a flowmeter to a differential pressure valve. Beyond this valve a flow of argon was maintained to purge the equipment following a run and to entrain the SOA gas. When the SO3 and argon gas pressures were equal, SO3 passed through the valve and was entrained in the argon. A run was initiated by setting the argon flow at the valve to correspond to the space velocity of interest. The volume ratio of argon to S03 was 12 to 1.This mixed stream flowed at constant pressure through a reaction tube centered in a split tube furnace which contained a V205 catalyst ground to -18 to +25 US standard .mesh. The SOX was decomposed catalytically to SO2 and 2 which passed through a -three-way stopcock upon leaving the furnace: The gases could then pass through a trap and scrubber series and be vented or they could be bubbled through a sintered glass frit into a stirred aqueous titrating solution containing Kl, HCl, and starch. Sulfur dioxide was titrated zwith 0.1 M Kilo3. The following equations give the titration reactions.
KIO3 + 5 KI + 6 HCI < 6 KC1 + 3 H2O + 3 I2 SO2 + I2 + 2 H29 < 2 HI + H2SO4 The SO2 titration- was dynamic and was conducted intermittently while the run was in progress. Titration was maintained just beyond the end point (indicated by a slight blue color). A colorless solution indicated that SO2 was not being reacted due to lack of iodine in the solution.
Data was obtained by recording the volume of titrant used in a given time period. Six or more such titrating runs were made at each temperature. From the titration reactions and the molarity of the KIO3 solutions, the number of moles of S02 produced per minute, and thus the SO? flow rate was calculated.
At a given space velocity the system was purged with argon between the set of runs at each temperature. The volume of catalyst was changed when runs at different space velocities were required.
The first experiments run on this apparatus were to determine the degree of reaction reversal to be expected upon quenching the high temperature gas mixture expected from the thermal reducer. This information was vital to an interpretation of the thermal reduction rate data taken later. Even more important, however, was the fact that if significant reoxidation of SO2 occurred following the thermal reduction reaction, the entire process concept would be either useless or highly inefficient.
The degree of reaction reversal to be expected was estimated by passing SO2 at a constant rate through the reactor, without catalyst present, with N2 and air carrier gases at various rates. Both hot and cold tests were performed. Under hot conditions, the mixture spent approximately two minutes flowing through the furnace (500-1000"C) and an additional two minutes in flowing from the 500"C furnace and to the analytical train. Under cold conditions, the gas mixtures traversed the system at room temperature. Residence times lower than four minutes were obtained by increasing the carrier flow while maintaining constant the SO2 rate.
A statistical analysis of the resultant data indicated identical S02 rates into the analytic train for the SO2/N2 hot runs and the SO2/air cold runs. No effect upon residence time, up to four minutes, was observed in the 8O2/air hot runs. Additionally, the S02 rate into the analytic train for the hot runs with air at all residence times was identical with that for the cold runs and the inert runs. Since over 100 determinations of S02 rate were made during this period, none of which showed any sifnificant statistical departure from the delivery rate, it is certain that SO2 reoxidation during quench will not be a problem so long as contact catalysts are not present.
The kinetics of the V2O5 catalyst was also investigated in the experimental apparatus.
The reaction order was determined by testing integrated mass balance and reaction rate equations against the integral reactor data obtained in the system. Once the reaction order is known, the rate constant can be expressed as a function of a reaction group. This group contains a complex function of initial and final sulfur trioxide concentrations and varies with reaction order.
Constructing a mass balance over a differential volume element of the reactor gives Fd2 = -Acs rrxn where F = volumetric flow rate, cc/hr x = mole fraction S03 Acs = reactor cross sectional area, cm2 rrxn = rate of reaction, cc/hr multiplied by S03 reacted volume Assuming that the decomposition rate is first order with respect to S03 concentration one obtains rrxn = ktCso3 = (ktCso3) x = kx where CsOo3 is the initial S03 concentration at the reactor inlet.
Substitutmg yields dg - ] X where k = reaction rate const., hr-' Sv = space velocity = AcsL/F, hr- g = dimensionless reactor length Z/L, where L = physical length of reactor, and Z = fractional length of reactor.
Using the boundary condition that x = x0 at g = 0, the solution becomes
The mole fraction of S03 leaving the reactor is given as XL = x0e kefff1S,, where
kg = gas phase mass transfer coefficient Under conditions of the present investigation, the mass transfer rate was much greater than the rate of chemical reaction, and the effect of kg can be neglected.The reaction rate constant, k, can be expected to follow the Arrhemus equation, that is, k = AeE/RT As a result, the pre-exponential factor, A, and the activation energy E, can be determined from a semilog plot of en(x,/xl) vs. 1/T. Under these conditions, Cnkn(x)] = - ens ~ El K If this model accurately describes the reaction, several predictions can be made.First, a plot on semilog paper of en x,/x vs. 1/T should yield a straight line with a slope proportional to E/R and an intercept proportional to (SV/A). Second, the slopes of the lines drawn for all three space velocities should be identical. Only the intercepts should differ.
In Figure 2 the ordinate, en (x,/x), is a measurement of the amount of conversion, as hereinbefore explained, and the abscissa is the inverse of the temperature times a thousand.
The curves show that the conversion rate increases as the temperature rises.
The top solid line is the calculated equilibrium curve for sulfur trioxide decomposition under the conditions used in these experiments. The points surrounding the top solid line were obtained experimentally at space velocity of 10,000 hr~l. The coincidence of these points with the equilibrium curve show that equilibrium conversion was obtained at that space velocity.
The lower curve was experimentally obtained at a space velocity of 60,000 hr-l.
Equilibrium conversion was not obtained at that space velocity, but the curve supports the conclusion that the reaction follows first order kinetics.
WHAT WE CLAIM IS: 1. A method for the net conversion of gaseous sulfur trioxide into sulfur dioxide and oxygen according to the equation 2S03 o 2SO2 + 2 which comprises passing said gaseous sulfur trioxide over a sulfuric acid contact catalyst at a temperature of 750 to 1000"C at a space velocity (as hereinbefore defind) of at least 100 hr-'; and preventing sulfur dioxide and oxygen produced from contacting said catalyst at a temperature of less than 750"C.
2. A method according to claim 1 which comprises the additional last steps of condensing uni'exacted sulfur trioxide followed by condensing the sulfur dioxide.
3. A method according to claim 1, which comprises the additional last steps of adding water to produce sulfuric acid from unreacted sulfur trioxide followed by condensing the sulfur dioxide.
4. A method according to claim 1, 2 or 3, wherein the catalyst is at least one of vanadium pentoxide and platinum.
5. A method, as claimed in claim 1, for the net conversion of gaseous sulfur trioxide into sulfur dioxide and oxygen, substantially as described herein with reference to the foregoing Example and the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (5)

**WARNING** start of CLMS field may overlap end of DESC **. Under conditions of the present investigation, the mass transfer rate was much greater than the rate of chemical reaction, and the effect of kg can be neglected. The reaction rate constant, k, can be expected to follow the Arrhemus equation, that is, k = AeE/RT As a result, the pre-exponential factor, A, and the activation energy E, can be determined from a semilog plot of en(x,/xl) vs. 1/T. Under these conditions, Cnkn(x)] = - ens ~ El K If this model accurately describes the reaction, several predictions can be made.First, a plot on semilog paper of en x,/x vs. 1/T should yield a straight line with a slope proportional to E/R and an intercept proportional to (SV/A). Second, the slopes of the lines drawn for all three space velocities should be identical. Only the intercepts should differ. In Figure 2 the ordinate, en (x,/x), is a measurement of the amount of conversion, as hereinbefore explained, and the abscissa is the inverse of the temperature times a thousand. The curves show that the conversion rate increases as the temperature rises. The top solid line is the calculated equilibrium curve for sulfur trioxide decomposition under the conditions used in these experiments. The points surrounding the top solid line were obtained experimentally at space velocity of 10,000 hr~l. The coincidence of these points with the equilibrium curve show that equilibrium conversion was obtained at that space velocity. The lower curve was experimentally obtained at a space velocity of 60,000 hr-l. Equilibrium conversion was not obtained at that space velocity, but the curve supports the conclusion that the reaction follows first order kinetics. WHAT WE CLAIM IS:
1. A method for the net conversion of gaseous sulfur trioxide into sulfur dioxide and oxygen according to the equation 2S03 o 2SO2 + 2 which comprises passing said gaseous sulfur trioxide over a sulfuric acid contact catalyst at a temperature of 750 to 1000"C at a space velocity (as hereinbefore defind) of at least 100 hr-'; and preventing sulfur dioxide and oxygen produced from contacting said catalyst at a temperature of less than 750"C.
2. A method according to claim 1 which comprises the additional last steps of condensing uni'exacted sulfur trioxide followed by condensing the sulfur dioxide.
3. A method according to claim 1, which comprises the additional last steps of adding water to produce sulfuric acid from unreacted sulfur trioxide followed by condensing the sulfur dioxide.
4. A method according to claim 1, 2 or 3, wherein the catalyst is at least one of vanadium pentoxide and platinum.
5. A method, as claimed in claim 1, for the net conversion of gaseous sulfur trioxide into sulfur dioxide and oxygen, substantially as described herein with reference to the foregoing Example and the accompanying drawings.
GB604577A 1976-02-25 1977-02-14 Producing sulphur dioxide and oxygen from sulphur trioxide Expired GB1575444A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002059596A2 (en) * 2001-01-02 2002-08-01 President And Fellows Of Harvard College Method and apparatus for measurement of the sulfate concentration in air samples
EP3448807A4 (en) * 2016-04-28 2019-11-06 Indian Institute of Technology Delhi Catalyst composition for conversion of sulfur trioxide and hydrogen production process

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4331632A (en) * 1980-11-18 1982-05-25 The United States Of America As Represented By The United States Department Of Energy Catalytic cartridge SO3 decomposer
GB2099805B (en) * 1981-05-22 1985-10-30 Us Energy System for thermomechanical hydrogen production

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE631150A (en) * 1963-04-17

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002059596A2 (en) * 2001-01-02 2002-08-01 President And Fellows Of Harvard College Method and apparatus for measurement of the sulfate concentration in air samples
WO2002059596A3 (en) * 2001-01-02 2003-04-24 Harvard College Method and apparatus for measurement of the sulfate concentration in air samples
EP3448807A4 (en) * 2016-04-28 2019-11-06 Indian Institute of Technology Delhi Catalyst composition for conversion of sulfur trioxide and hydrogen production process

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JPS54109094A (en) 1979-08-27
FR2342248B1 (en) 1981-10-30
BE851498A (en) 1977-08-16
FR2342248A1 (en) 1977-09-23
DE2708242A1 (en) 1977-09-08

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