CA1224941A - Method and apparatus for the calorimetry of chemical processes - Google Patents

Abstract

METHOD AND APPARATUS FOR THE CALORIMETRY
OF CHEMICAL PROCESSES
ABSTRACT OF THE DISCLOSURE
A calorimeter for measuring the thermodynamic and kinetic characteristics of chemical reactions, microbial fermentations, and other processes of industrial importance is described. The present invention also relates to a method of operation of this apparatus.

Description

29, " ~,2~

METHOD AND APPARATUS FOR THE CALORIMETRY
_ OF CHEMICAL PROCESSES
Chemical reactions are accompanied by the liber-ation or absorption of energy in the form of heat, and this "heat of reaction" is a definite, reproducible characteristic of a given chemical change. Morever, chemical reactions occur at widely differing rates of speed, and the characteristic time variation of the reaction rate is referred to as "reaction kinetics". The measurement of reaction heat and reaction kinetics is a fundamental part of the experimental development oE
large-scale chemical manufacturing processes, relating to the optimization and saEety of the process and providing design parameters for the manufacturing facility. Any apparatus used for measuring heat is called a calorimeter and numerous prior-art calorimeters have been described covering a wide variety oE specific applications. An example of a prior-art calorimeter applied to the study of chemical reactions is described in U.S. Patent 3,994,164.
The invention herein described relates to a new and improved calorimeter designed and optimized for the study of chemical manufacturing processes on a laboratory scale. It is capable of providing accurate measurements of heats of reaction and instantaneous reaction rates.
This apparatus offers superior performance and safety of use. The incorporation oE a chemically inert, metallic reaction vessel rather than a glass vessel provides a greatly reduced thermal time constant due to the one-, thousand fold higher thermal conductivity of the metal.
. .

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- 2 - 1109-7320 This allows the calorimeter to respond more quickly to thermal fluctuations in the reaction mass, thus lowering the thermal detecti.on threshold and raising the satura-ting heat Elux level.
The provision of a thermostatting mechanism for several chemical feed streams external to the reaction vessel provides accurate measurement oE the characteristic reaction heat. In the absence of such a mechanism, the reaction mass will be heated or cooled due to the different temperatures of the chemical feed streams.
This causes significant measurement errors. The provision of an adiabatic shield makes the present invention impervious to environmental temperature fluctuations, whereas the prior art calorimeter is sensitive to ambient temperature changes. From the point of view of operator safety, the present invention uses a five to ten-fold smaller reaction mass, avoids completely the use : of fragile glass vessels, and provi.des an outstanding pressure : relief mechanism of novel design with -the largest possible vent orifice for the reaction vessel. These design qualities combine to create a superior calorimeter with a greatly reduced potential explosion hazard, providing a scientific instrument which can be operated with utmost safety in a conventional chemical laboratory.
Therefore, the present invention constitutes an advance in the technology of reaction calorimetry and satisfies a need which exists in the art.
In accordance with this invention, there is provided a calorimeter for use in examining chemical processes comprising:
a. ~ flat-bottomed reaction vessel equipped with a gas-tight cover, an agitator mechanism, a temperature 9~L

- 3 - 1109-7320 sensor, a calibration hea-ter, several chemical inle-t ports, and a two-stage pressure rellef mechanism;
b. A heat exchanger in intimate contact with the base of said reaction vessel to regulate heat flow to the vessel and its reaction mass, where said heat exchanger comprises an electrical heater attached to a circular metal plate which is cooled by a fluid circulating at a definite temperature;
c. An adiabatic shield to preven-t uncontrolled heat leakage from the vessel, where said adiabatic shield comprises a cylindrical barrier surrounded by an electrical heater and cooled by a flowing gas, and equipped with a temper-ature sensor;
d. An incubation mechanism to equilibrate the -temperature of the chemical feed streams, comprising a tubular heat exchanger attached to said adiabatic shield and in close thermal contact with same;
e. A facile means -to assemble and disassemble the apparatus and to gain access to the reaction vessel wherein the various covers to the cylindrical chambers are connected as a single assembly and the agitator drive shaft is separated in two parts which are coupled by a gear-tooth coupler;
f. A reservoir for said circulation fluid equipped with a pump, a heater, a refrigeration system, and a temper-ature sensor;

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- 3a - 1109-7320 g. An electronic regulation means responsive to said temperature sensors and adapted to control the temperatures of the reaction mass, Tr~ the adiabatic shield, Ts, and the circulating fluid, To~ wherein said electronic regulation means regulates the balance between heating and cooling by adjusting -the power dissipated in the heating element while under constan-t cooling from the cooling elemen-t, in each control device b, c, and f aforementioned.
Heat can be added to or subtracted from the reaction mass to compensate for the heat of reaction and hold the sys-tem isothermal by use of the heat exchanger which preferably comprises a thin insulated metal foil resistive heater attached to a rigid metal plate, the underside of which is cooled by a circulating fluid flowing at a very high rate and maintained at a constant temper-ature below that of the reaction mass. The electrical power dissipated in the control heater is adjusted to exactly eliminate heat flow fxom the vessel to the circulating fluid heat sink and to maintain constant the temperature of the reaction mass. When the reaction begins, the power dissipation in the control heater is adjusted to offset the heat flux due to the heat of reaction.
Thus, the change in the power dissipation in the control heater is linearly proportional to the rate at which heat is evolved or absorbed by the reaction, where the slope of this proportionality is related to the ratio of the thermal resistances between the heater and the circulating fluid and between the heater and the .

- 3b - 1109-7320 reaction mass, and the intercept depends upon the temperature differen-tial between -the vessel and the circulating fluid. There-fore, the characteristics of the calorimeter can be adjus-ted during design by selection of values for the above mentioned para-meters to maximize sensitivity or, conversely the saturating hea-t flux. The thermal characteristics of the calorimeter are further controlled and adjusted by selection of materials of high and low thermal impedance and appropriate dimensions to channel the flow of heat in a desixed direction, and, also by the use of thermal barriers such as the aforementioned adiabatic shield.

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In the preferred embodiment of the invention, a digital computer is commissioned to acquire the thermal measurements and provide control of the electrical power supplied to the various heat exchanger devices, as well as controlling the delivery of feedstocks and the agitation rate, and performing the calculation and graphical presentation of thermal and kinetic results.
In an alternative embodiment of the invention, an analog controller is used in each area where electronic control is required, and the measurements are displayed on an analog recording device.
The design of the preferred embodiment of the invention is optimized for isothermal operation, as heretofore described. However, both adiabatic and temperature scanning modes of operation are also possible. In the isothermal mode, heat is removed from or added to the reaction mass to offset the heat of reaction and maintain the temperature constant. In the adiabatic mode, heat flow to or from the reaction mass is prevented, the heat of reaction remains in the reaction mass, and the temperature of the reaction mass is allowed to rise exponentially as dictated by the thermodynamics and kinetics of the reaction, by tracking the reaction temperature with the adiabatic shield and circulating oil temperatures. In the temperature scanning mode, the temperature of the reaction mass is increased in a stepwise, linear, or other predetermined fashion as required, by raising the temperature of the circulating fluid and adiabatic shield according to a temperature program.

, FIGURE 1 is a schematic illustration of the -mechanical arrangement of the exemplary embodiment of the inventive apparatus, in a cross-sectional view.
FIGURE 2 is an illustration of the facile means of assembly and disassembly of the apparatus through the connection of the various covers and gear coupling of the agitator drive shafts.
FIGURE 3 is a block diagram of the interconnec-tion of the electronic control and measurement components in the preferred embodiment of the invention FIGURE 4 is a graphical illustration of the linear response of the control heater power as a function of the power dissipated in the calibration heater of the apparatus.
FIGURE 5 is a graphical illustration of a typical use of the apparatus in the study of a rapid acid-base reaction.
FIGURE 6 is a graphical illustration of a slow organic reaction conducted in the apparatus.
The chemical reaction calorimeter was Eabricated on a design principle of cylindrical symmetry, as shown in FIGURE I. Viewed from above, the device appears as a set of concentric metal canisters acting as thermal barriers serving different purposes as discussed below. The heart of the calorimeter is a removable reaction vessel, (1), and its cover, (2), which are fabricated from a chemically resistant metal. In the prototype calorimeter, zirconium was used to ensure corrosion resistance to strong mineral acids and bases.
The reaction vessel is equipped with a number of devices which are attached to the cover, (2). A high-precision platinum resistance thermometer (RTD), (3), is used to sense the temperature of the reaction mass with a reso-lution of 5 x 10-4C. The reaction mixture is stirred by an agitator blade, (4), driven by a stepping motor, (5), through a shaft, (6). The vessel contains a resistive heater, (7), used in the calibration of the calorimeter.
The temperature of the reaction mass is carefully regulated by a heat exchanger device made up of heating and cooling elements. This design principle of simultaneous heating and cooling is used in all thermostated regions of the calorimeter to ensure superior temperature control and a short thermal time constant. The vessel's heating is achieved by a circular metal foil resistance heater insulated with O.OQl inch polymer film, and bonded to the topside of a metal disk, (8). The underside of the metal plate, (8), is cooled by a circulating fluid (low viscosity silicone oil in the prototype) flowing from an inlet pipe, (9), flowing radially through the gap between the two circular plates, (8) and (10), and discharging from the outlet pipe (11). The circulating fluid, serving as a heat sink, is supplied from and returned to a reservoir which is simultaneously heated and refrigerated to provide excellent temperature regulation. The constant temperature difference between the circulating oil and the chemical reaction mass is an important design parameter, as discussed below.
All heat flow to or from the reaction vessel takes place by conduction through its flat base, which is in intimate contact with the heat exchanger mechanism.
Heat flow through the walls and cover of the vessel is effectively eliminated by the provision of an adiabatic shield, which maintains the temperature of the space surrounding the reaction vessel equal to the temperature inside the vessel. The adiabatic shield is an air oven contained within a metal canister, (12), and its cover, (13). An insulated foil heater, (14), is bonded to the outer wall of canister, (12), and is cooled by compressed air flowing from numerous ducts, (15). The cooling air is contained by a second canister, (16), and cover, (17), and exhausted throug~ a vent pipe (not shown). The temperature of the air space inside the adiabatic shield is sensed by a second platinum resistance thermometer (RTD), (18), and maintained at the temperature oE the chemical reaction mass by electronic control.
The heat exchanger mechanism and adiabatic shield canisters are supported by a base block, (19), fabricated from polytetrafluoroethylene, chosen because of its high thermal impedance and suitability for high temperature operation. The body of the heat exchanger, (20), is also made of this material. The entire calorimeter is housed in an outer metal shell, (21), equipped with a cover, (22), and base, (23). The space insi~e this shell is filled with glass fiber insulation, (24).
The assembly and disassembly of the calorimeter is extremely simple since the inner covers, (13) and (17), are attached to the outer cover, (22), by tubular stand-offs, (25). Thus, all three covers are removed and inserted as a single assembly, as shown in FIGURE (2).
The agitator shaft, (5), which is supported by integral needle bearings and lip seals, (26), is broken just above the reaction vessel cover, (2), and rejoined by a gear-tooth coupler, (27). The upper gear of the coupler is removed with the outer and inner covers, (13), (17) and (22), and drive motor, (5), and shaft, (8). The lower gear of the coupler is attached to the lower shaft and remains with the reaction vessel, (l), which can be removed separately.

During operation of the calorimeter, fluid chemicals can be added sequentially or simultaneously to the reaction vessel through multiple inlet pipes, (28).
The temperature of these "titrants" is pre-equilibrated in a tubular heat exchanger (not shown) which is in intimate contact with the adiabatic shield canister, (12). This heat exchanger is a stainless steel pipe coiled and bonded to the inside of the canister, and a separate pipe is used for each reactant. The chemicals are mechanically pumped from external reservoirs through the equilibration pipes and into the reaction vessel.
Pressure relief venting of the reaction vessel is achieved on tWQ levels. A small spring loaded relieE
valve (not shown in FIGURE 1) is installed in the cover, (2), and provides a 1/8 inch diameter vent to relieve small overpressures. In the event of a large overpressure exceeding the capacity of the primary vent, the entire cover, (2), of the reaction vessel will move upwards, providing the largest possible vent orifice.
The movement of the cover is made possible by the spring loaded cover retainers, (29), and the bellows coupling, (30), for the agitator shaft. The vented vapours exit through pipes in the base of the calorimeter (not shown in FIGURE 1).
In the preferred embodiment of the calorimeter, all control and measurement functions are performed using a digital computer to simplify operator interaction and to provide flexibility in the design and application of the control algorithms. In addition, a microprocessor-based controller was incorporated to facilitate timing,switching, and control functions, as well as communication to the host computer.

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FIGURE 3 illustrates the block diagram for the electronic control system. Two different digital interface buses are used: the 16-bit parallel interface allows communication between the computer and the microprocessor, while a standard IEEE-488 interface (8-bit parallel/byte serial) was used Eor communication between the computer and several peripheral devices supplied with this inter~ace protocol.
The microprocessor controller comprises a central processing unit (CPU), a real time clock/inter-rupt generator, (CLOCK), a digital interface controller (I/O), a relay multiplexer (MIJX), four high stability digital to analog converters (DAC), random access memory (RAM), and erasable programmable read only memory (EPROM). The microprocessor provides a convenient means of implementing the interconnection and switching of system components. The acquisition of data, decision making and control functions are performed independently by the digital computer.
A high precision digital voltmeter is used to make voltage and resistance measurements throughout the system, and is switched between the various input lines by the relay multiple~er (MUX) under computer control.
The resistance measurements of the platinum RTD's are true 4-wire measurements with D.C. ofEset compensation for junction effects, providing a resistance thermometer resolution of 5 x 10~4C. The platinum RTD's are cali-brated against a Quartz reference thermometer (QUA~TZ) with an ~BS traceable response curve. Power dissipation in the various resistance heaters is determined by measuring the applied voltage across the heater and multiplying by the current flowing in the circuit. The current is measured independently as the voltage across a precision series current sense resistor divided by its known resistance. Thus, the powe~ measurements are absolute with very high precision.

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Electrical power to the heaters is supplied by three programmable power supplies, which are programmed from the computer via three of the four DAC's.
The fourth ~AC is used to control and program the oil bath temperature. These 16-bit DAC's provide a control resolution of 216 or one part in 65,536.
~ or the calorimeter described above to provide quantitative thermochemical information, regardless of whether the operating mode is isothermal or temperature scanned, it is necessary for the temperature diEference between the chemical reaction mass and the circulating oil heat sink to remain constant. The operation under isothermal conditions is most easily understood. If the temperature set point for the reaction is Tr and that for the oil bath To~ then Tr7To and the difference~ To =
Tr-To is positive and constant. If the thermal resistance between the heater and the circulating oil is Ro (deg.
Watt~l), then the power dissipation qh in the control heater (part 8 in FIGURE 1) is given by:

I' -1' qh R ( 1 ) Under these steady state conditions, no heat will flow into or out of the reaction vessel and Tr will remain constant. The value f qh given by Equation (1) represents the baseline for the experiment at a point where no reaction is occurring.

~9~2 ~

When heat is generated in the reaction vessel at a rate qr, due to either chemical reaction or applying electrical power to the calibration heater (part 7 in FIGURE l), this heat must be quickly removed to avoid raising the temperature of the reaction mass. The only available conduction path for heat dissipation is through the bottom of the reaction vessel, through the control heater, into the rapidly circulating oil, and eventual dissipation in the oil reservoir refrigeration system.
If the thermal resistance between the reaction mass and the heater is Rr~ then:

Tr-To ~ qr (Rr o) qh (2) Equation (2) rearranges to:

T - T Rr 2 0 r ~ q h ~ q ~ R ) ( 3 ) Since equation (1) indicates that the baseline qh when qr=O is (Tr-To)/Ro, then the change in qh when qr~O is 25 given by the left hand side oE Equation (3). Thus, ~qh qr(l + R ) (4) Equation (4) suggests that the change in power dissipation in the control heater, ~qh, is linearly proportional to the heat generated in the reaction, qr, with a slope determined by the ratio of the thermal ~2~
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resistances Rr and Ro and an intercept of zero. Thus, it is apparent that the heat of a chemical reaction ~Hr can be measured by integrating the change in power dissipation in the control heater during the course of the reaction:

r ~C J ~q h d t ( 5 ~

where the constant K = Ro/(Ro + Rr) is determined during the electrical calibration of the calorimeter.
These observations lead to a number of interest-ing speculations. The maximum power dissipation in the calorimeter is limited by Ro~ which should be minimized for a reasonable ~ To~ The thermal sensitivity of the calorimeter is maximized by making the ratio Rr/Ro large, so that a small reaction heat qr produces a large change in the control heater power qh. On the other hand, making Rr/Ro small maximizes the heat flux that can be handled by the calorimeter. Since the ratio of the thermal resistances Rr/Ro is adjustable during the fabrication of the calorimeter, an instrument with any desirable characteristic can be constructed.

The dynamic characteristics of the calorimeter can be deduced by constructing a formulation Eor a resis-tance/capacitance equivalent circuit which contains an exponential term [(l-exp (-t/T)], whereT is the system time constant. However, as discussed below, the response of the calorimeter is not limited by this natural time constant due to the use of a control algorithm which gives a greatly reduced effective time constant.

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The computer program used to control the calorimeter acquires the temperature measurements from the various sensors, relates the actual temperatures to the desired temperatures (set points), and causes the appropriate response to correct any differences. The mathematical relationship between the error signal A T (-set point - actual temperature) and the corresponding power level in the particular control heater is called the control algorithm. For the adiabatic shield, a con-ventional PID (proportional/integral/derivative) algor-ithm is used and found to be satisfactory. The functional form of this algorithm is:

qh KZ . ~T6 ~ 1C2 r ~T6 dt + K3 . d(J~T ) (6) d~ .

Where ~Ts is the error signal for the adiabatic shield.
The coefficients of the three terms in Equation 20 (6), Kl, K2, and K3, were optimized experimentally to give a rapid response with minimum overshoot and ringing.
The use of the PID algorithm "forces" the calorimeter to respond more quickly than the natural time constant would suggest. The effective time constant can be made a small 25 fraction of the natural constant by adjustment of the coefficients in Equation (6).
The control algorithm for the vessel control heater is novel and was found by experience to give the best control. A PI type of algorithm (no derivative term) with a quadratic dependence on the vessel error signal ~Tc was used:

qh ~ K3 ~TC I~TC I + K4 ~Tc. ¦~TC ¦

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where IATclsignifies the absolute value of the error signal.
The effect of this algorithm is to make the heater power qh essentially constant when ~Tc is insigni-ficantly smal], but to change qh more rapidly for largerTc's than a linear dependence would allow. The consequence of this approach is a noise-free b-aseline (constant qh) and very rapid return to the set point temperature following a thermal disturbance (e.g., reaction onset). In order to make the thermal responses identical during heating and cooling cycles, diEferent values of the coefficients K3 and K4 were used for positive and negative error signals, ^Tc. This efEectively compensates for the different efficiencies of the heatillg and cooling elements of the control device.
The operation of the chemical reaction calori meter is based on a power compensation principle. In order to establish the validity of the heat generation data provided by the calorimeter, it was necessary to determine the linearity of the controller response by calibration and to determine the accuracy of the heat flow measurement by examination of a known chemical system.
The linearity of the controller power response was determined using a vessel which contained 150 g of water. In this experiment the temperature difference between the reaction vessel and circulating fluid was maintained at 30K. Electrical power was applied to the calibration heater over a range of 0 to 40 watts. The power response of the control heater was found to be ~
linear function of calibration heater power, as shown in FIGURE 4. The composite thermal resistances, Ro and Rr can be deduced from the slope of this calibration plot and the baseline power qh.

Tr - To ( B ) qh rRo 1~-- ~3 ~ Ro ~ ~slope -1) (9) The value of the calibration constant K (see Equation 5) iS:

K Ro ., I ( 10 ) The performance of the calorimeter was tested by examination of an acid-base neutralization reaction.
Four replicate determinations of the enthalpy of neutral-ization of tris-(hydroxymethyl) aminomethane (TRIS) and hydrochloric acid yielded a mean experimental value oE
25 -11. 55 kcal/mole, which is in excellent agreement with the reported literature value, -11.55 kcal/mole (1). A
typical plot of time vs controller power for this experiment appears in FIGURE 5.

~HOCH2)3CNH2 + HCl 2 3 3 TRIS

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The regions of the plot delineated by a-b, c-d, e-f, and g-h represent the baseline for the experiment.
The power excursions in regions b-c and f-g are due to electrical power dissipated in the calibration heater, and the response in region d-e is due to the acid-base neutralization reaction. Because the rate of this proton-exchange reaction is extremely fast relative to the response time of the calorime~er, a boxcar power response curve is obtained with edges corresponding to the start and finish of the titration. Thus, kinetic analysis is not pertinent for this reaction.
Verification of the performance of the calori-meter has been obtained for an organic chemical reaction in a non-aqueous system. The heat of reaction for the ethanolysis of acetic anhydride using p-toluene sulfonic acid (p-TSA) as a catalyst has been determined as -14.38 kcal/mole in four experiments.

CH3~--CHJ + CH3cH20u P ~ CH3~CH2CH3 -t CH3~--OH

An experimentally determined heat oE reaction has not been reported in the literature. However, the heat of reaction has been estimated as -14.26 kcal/mole using the computation method of Handrick based on averaged functional group contributions to the heat of combustion of organic compounds (2). The time vs heat flow curve is given in FIGURE 6.

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As in the previous example, electrical calibra-tion pulses are applied before and after the reaction, which occurs during region d e. The onset of the power excursion is rapid and a plateau is reached determined by the rate of addition. However, as reagents are consumed, the reaction slows down and the power response decreases.
After the reagent addition is complete, the reaction continues for some time with second-order kinetics and the power response decays in concert with this rate law.
Analysis of the power curve yields the second-order rate constant for the reaction.

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Claims (10)

1. WHAT IS CLAIMED IS:
   
   l. A calorimeter for use in examining chemical processes comprising:
   a. A flat-bottomed reaction vessel equipped with a gas-tight cover, an agitator mechan-ism, a temperature sensor, a calibration heater, several chemical inlet ports, and a two-stage pressure relief mechanism;
   b. A heat exchanger in intimate contact with the base of said reaction vessel to regulate heat flow to the vessel and its reaction mass, where said heat exchanger comprises an electrical heater attached to a circular metal plate which is cooled by a fluid cir-culating at 2 definite temperature;
   c. An adiabatic shield to prevent uncontrolled heat leakage from the vessel, where said adiabatic shield comprises a cylindrical barrier surrounded by an electrical heater and cooled by a flowing gas, and equipped with a temperature sensor;
   d. An incubation mechanism to equilibrate the temperature of the chemical feed streams, comprising a tubular heat exchanger attached to said adiabatic shield and in close ther-mal contact with same;
   e. A facile means to assemble and disassemble the apparatus and to gain access to the reaction vessel wherein the various covers to the cylindrical chambers are connected as a single assembly and the agitator drive shaft is separated in two parts which are coupled by a gear-tooth coupler;
   
   f. A reservoir for said circulation fluid equipped with a pump, a heater, a refrigeration system, and a temper-ature sensor;
   g. An electronic regulation means responsive to said temperature sensors and adapted to control the tempera-tures of the reaction mass, Tr, the adiabatic shield, Ts, and the circulating fluid, To, wherein said electronic regulation means regulates the balance between heating and cooling by adjusting the power dissipated in the heating element while under constant cooling from the cooling element, in each control device b, c, and f aforementioned.
2. 2. The apparatus of Claim 1, wherein said heat exchanger comprises a flat circular insulated foil heater bonded to a supporting plate which is cooled by a fluid flowing radially between the said plate and a second plate, from the center to the edge or vice versa, wherein the cooling efficiency of the fluid is unvaried and the heating efficiency of the heater is adjusted to regulate the temperature of the reaction mass contained within said vessel.
3. 3. The apparatus according to Claim 2, wherein said adiabatic shield comprises a covered cylindrical chamber wrapped with a bonded foil heater and cooled uniformly by pressurized gas flowing from numerous ducts surrounding said adiabatic shield, and the balance of heating and cooling maintains the temperature with-in said chamber equal to the temperature of the reaction mass.
4. 4. The apparatus according to Claim 3, wherein the temperature of one or more chemical feedstreams is equilibrated with the reaction mass already within the vessel by use of tubular heat exchangers bonded to the interior surface of the adiabatic shield in intimate ther-mal communication with the heating and cooling mechanisms of said adiabatic shield.
5. 5. The apparatus according to Claim 2, wherein the cooling fluid is supplied by a reservoir equipped with a circulatory system and a temperature regulation mechan-ism comprising a temperature sensor, an electrical heater, and a refrigeration system, manifesting suitable means to closely regulate the temperature of the circulating fluid.
6. 6. The apparatus according to Claim 1, wherein excessive pressure build up can be relieved by a two-stage mechanism comprising:
   a. A small adjustable valve, located in the cover of the reaction vessel, providing a vent orifice of 0.125 inch diameter to re-lieve small overpressures, and;
   b. A collapsible retaining mechanism for the cover of the reaction vessel comprising spring loaded retainers for the cover and a bel-lows-coupling for the agitator shaft, which combine to permit verticle displacement of the said cover and said shaft to provide the largest possible vent orifice to relieve large overpressures and ensure utmost safety during operation of the calorimeter.
7. 7. A method of operating the apparatus of Claim 1, wherein the temperature difference between the oil reservoir and chemical reaction mass is maintained con-by the heat exchanger in Claim 2 working in concert with the fluid thermostat and circulatory system in Claim 5, wherein the temperature of the reaction mass is either held constant or forced to follow a prescribed variaton, and during which the heat of reaction and reaction kinetics are measured by the proportional adjustment of the power dissipation in the electrical control heater located in said heat exchanger.
8. 8. A method of operating the apparatus of Claim 1, wherein the electrical power dissipation, qh, in the control heater located in the heat exchanger in Claim 2 is regulated in proportion to the signed square of the temperature error signal, .DELTA.T, plus the time integral of the signed square of the temperature error signal, wherein said temperature error signal is the difference between the instantaneous temperature of the chemical reaction mass and the specified temperature set point, in accordance with the relationship:
   where Kl and K2 are constants of different magnitude for positive and negative temperature error signals and ¦.DELTA.T¦ signifies the absolute value of the temperature error signal.
9. 9. The apparatus according to Claim 1, 2 or 3, wherein said electronic regulating means is a digital computer controller.
10. 10. The apparatus according to Claim 1, 2 or 3, wherein said electronic regulation means is an analog controller.