System for determining process parameters relating to thermal processes such as, for instance, waste incineration

Abstract
The invention relates to a system for thermal combustion processes of matter such as, for instance, waste incineration. The system comprises a computer for measuring parameters of the combustion of the matter, wherein use, matter, such as for instance waste, is supplied to the system and combusted, thereby forming a flue gas. The system further comprises means for determining the concentration of CO2, O2 and H2O in the flue gas. The computer is arranged for determining, on the basis of the measured concentrations, the rate of combustion and/or the composition of the combustible part CHyOz of the waste supplied to the system, for the purpose of process control.
Description




This application is the U.S. National Phase of International Application Number PCT/NL00/00377 filed on Jun. 5, 2000, which is incorporated herein by reference.




BACKGROUND OF THE INVENTION




This invention relates to a system for determining process parameters relating to thermal combustion processes of matter such as, for instance, waste in an incinerator, comprising sensor means and a computer coupled thereto for determining the parameters, wherein, in use, matter having a combustible part CH


Y


O


z


is supplied to the incinerator and combusted, thereby forming a flue gas.




This invention relates to a system for determining process parameters relating to thermal combustion processes of matter such as, for instance, waste in an incinerator, comprising sensor means and a computer coupled thereto for determining the parameters, wherein, in use, matter having a combustible part CH


y


O


z


is supplied to the incinerator and combusted, thereby forming a flue gas.




Operational management of the existing plants for waste incineration is rendered more difficult by the varying composition of the waste that is supplied to an incinerator of the plant. Due to the circumstance that changes in the properties of the waste are not recognized timely in the process behavior, the existing control systems are not properly able to regulate the process.




If, however, the waste composition of the waste in the incinerator could be derived on-line, this would enable better adjustment to variations in the waste composition, thereby rendering the waste incineration process better controllable. Such a derivation, however, is highly complicated.




SUMMARY OF THE INVENTION




The object of the invention is to provide a system that can be utilized in a plant for combustion of matter to meet the drawbacks outlined. Accordingly, the system for determining process parameters relating to the thermal combustion of matter is characterized in that the sensor means are arranged for measuring the fractions X


CO2


, X


O2


and XH


2O


in the flue gas and that the computer is arranged for determining, on the basis of the measured fractions, the composition (y/z) and/or the heat of combustion (H


CHyOz


, [J/kg]) of the combustible part CH


y


O


z


, with X


O2


, X


H2O


, X


CO2


respectively representing the fractions of O


2


, H


2


O and CO


2


in the flue gas.




The object of the invention is to provide a system that can be utilized in a plant for combustion of matter to meet the drawbacks outlined. Accordingly, the system for determining process parameters relating to the thermal combustion of matter is characterized in that the sensor means are arranged for measuring the fractions X


CO2


, X


O2


and X


H2O


in the flue gas and that the computer is arranged for determining, on the basis of the measured fractions, the composition (y/z) and/or the heat of combustion (H


CHyOz


, [J/kg]) of the combustible part CH


y


O


z


, with X


O2


, X


H2O


, X


CO2


respectively representing the fractions of O


2


, H


2


O and CO


2


in the flue gas.




By measuring, in accordance with the invention, just the fractions X


CO2


, X


O2


and X


H2O


in the flue gas, relevant parameters (the heat of combustion and/or the composition of the combustible part) for possible regulation of the matter combustion can be determined. More particularly, it holds that, in use, the computer calculates the value of Z on the basis of the formulae:







z
=


2
·
Xc

+


1
2

·
y

-


2
·

X
C

·

X

N

2


·

X

02
,
air





X

CO

2


·

X

N2
,
air




+


2
·

X
C

·

X

O

2




X

CO

2





;










and








X




N2


=1


−X




O2




−X




H2O




−X




CO2








wherein X


O2,air


(the oxygen fraction in air supplied to the incinerator), X


N2,air


(the nitrogen fraction in air supplied to the incinerator), X


c


(the uncombusted fraction of carbon) and y are predetermined values. Preferably, it will then hold that the predetermined value of X


c


is inbetween 0.9 and 1. Further, it holds in particular that, in use, the computer calculates the value of H


CHyOz


on the basis of the formulae








H
CHyOz

=



408.4
+

102.4
·
y

-

156.8
·
z



M
CHyOz


·

10
3



;










and








M




CHyOz


=0.012+0.001


y


+0.016


z.








According to a further advanced embodiment of the system, it holds that the system further comprises sensor means for determining the air flow Φ


tot


of the air which, in use, is supplied to the incinerator, the computer being arranged to determine on the basis of the measured fractions X


CO2


, X


O2


and X


H2O


, the ash-free heating value (H


waste,ash-free


, [J/kg ash-free]) and/or, further on the basis of the measured air flow Φ


tot


, the amount of heat (Q


heat


, [W]) which is released upon the combustion. More particularly, it holds further that the computer is further arranged for further determining, on the basis of the predetermined value of the inert fraction of the waste (X


inert


, [kg inert/kg waste]), the following four parameters: the waste flow (Φ


waste


, [kg/s]), the moisture fraction of the waste (X


H2O,waste


, [kg water/kg waste]), the heating value of the total waste (H


waste


, [J/kg waste]) and/or the fraction of uncombusted (X


uncombusted


, [kg uncombusted/kg ash]).




On the basis of one or more of the above-mentioned parameters as determined by the computer, the waste incineration plant can be controlled in a manner known per se, such that combustion is optimal.











BRIEF DESCRIPTION OF THE DRAWINGS




The invention will presently be further elucidated with reference to the drawings. In the drawings:





FIG. 1

shows a possible embodiment of a plant for waste incineration comprising a system according to the invention; and





FIG. 2

shows a simplified representation of the waste incineration process of the system according to FIG.


1


.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




In

FIG. 1

, a plant for waste incineration is designed by reference numeral


1


. The plant comprises an incinerator


2


, known per se, comprising an entrance


4


to which the waste is supplied. The incinerator


2


further comprises an exit


6


for discharge of the combustion products formed upon combustion. The plant further comprises a conveying device


8


which conveys the waste for combustion from the entrance


4


to the exit


6


. The plant in this example further comprises means


10


, known per se, for controlling the amount of air and/or optionally the temperature of the air which is supplied to the incinerator. The plant further comprises a control unit


12


, which in this example comprises a computer for controlling various settings of the incinerator. Thus the computer


12


can, for instance, control the air supply means


10


and/or the speed of the conveying device


8


. These controls can, in this example, be carried out via line


14


.




The incinerator may further comprise a chimney


16


with a controllable outlet


18


. The outlet


18


in this example is likewise controlled by the computer


12


, via a line


20


. In the chimney, further, a dust catcher


22


known per se is included. Via a conduit


24


at least a portion of the flue gases which leave the incinerator via the chimney


16


and which have been stripped of dust by means of the device


22


can be fed back to the incinerator. This involves so-called flue gas recirculation. Further, adjacent the chimney


16


an inlet


25


may be arranged via which inlet secondary air can be supplied to the incinerator. The computer


12


may further be arranged to control a control valve


28


, arranged in the return conduit


24


, via a line


26


.




In

FIG. 2

the combustion process of the plant according to

FIG. 1

is schematically indicated. The incinerator proper is represented here by a square. The waste that is supplied to the incinerator via the entrance is designated by reference numeral


30


. The primary air that is supplied to the incinerator via the air supply means


10


is designated by reference numeral


32


. The secondary air that is supplied via inlet


25


to the incinerator is designated by reference numeral


34


. The flue gas that leaves the incinerator via the chimney


16


is designated by reference numeral


36


, whilst the portion of the flue gas that is recirculated to the incinerator via the conduit


24


is designated by reference numeral


38


. The portion of the waste that is not burnt in the incinerator is designated by reference numeral


40


. Output streams therefore consist of the flue gas and the uncombusted waste. The waste consists of a fraction of combustible (CH


y


O


z


), moisture and inert. The values of y and z are to be further determined. In the primary and secondary air, also the water present in the air is included. The composition of the flue gas recirculation is equal to the composition of the flue gas. It has been assumed that the uncombusted waste consists solely of carbon. The combustible part of the waste reacts with oxygen to form carbon dioxide, water and carbon. Here, a carbon conversion (X


c


, [mol/mol]) is assumed.




The fraction of moisture in the primary and secondary air can be calculated if the temperature and the relative humidity of the air are known. The saturated vapor pressure of water (P


0




H2O


, [Pa]) can be calculated using the temperature of the (T


air


, [K]).










P
H2O
0

=

133.32






exp


(

18.3036
-

·

3816.44


T

air
,


-
46.13




)







(
1
)













The fraction of moisture in the air (X


H2O,air


, [mol/mol]) can now be calculated using the relative humidity (RH


air


, [%]) and the total pressure (P, [Pa]).










X

H2O
,
air


=



P
H2O
o

,

RHair
100


P





(
2
)













The fraction of oxygen and nitrogen in the air can now be calculated as follows.








X




O2,air


=0.2095(1


−X




H2O,air


)  (3)










X




N2,air


=0.7905(1


−X




H2O,air


)  (4)






If the other gases present in the flue gas are disregarded, the fraction of nitrogen in the flue gas (X


N2


, [mol/mol]) can be calculated from the fraction of oxygen, water and carbon dioxide (X


O2


, X


H2O


, X


CO2


, [mol/mol]):








X




N2


=1


−X




O2




−X




H2O




−X




CO2


  (5)






For calculating the waste composition using the mass balances, presently the following data are needed. First, the molar flow rates of the primary and secondary air and of the flue gas recirculation (Φ


primary


, Φ


secondary


, Φ


recirculation


, [mol/s]). Next, it was chosen to fix the carbon conversion and a value for y. Realistic values for these constants will be discussed later on.




The flue gas flow (Φ


flue gas


, [mol/s]) can be calculated using a mole balance over the nitrogen.








X




N2,air





primary





secondary


)+


X




N2


Φ


recirculation




=X




N2


Φ


flue gas


  (6)






Describing this equation gives:
















Φ
fluegas

=


X

N2
,
air



X
N2



,


(


Φ
primary

+

Φ
secondary


)

+

Φ
recirculation






(
7
)













The molar flow of combustible (Φ


CHyOz


, [mols]) can be calculated using a mole balance over carbon:






Φ


CHyOz




+X




CO2


Φ


recirculation




=X




CO2


Φ


flue gas


+(1


−X




c


).Φ


CHyOz


  (8)






Combination of the carbon balance and nitrogen balance yields










Φ
CHyOz

=




X
CO2

·

X

N2
,
air





X
C

·

X
N2





(


Φ
primary

+

Φ
secondary


)






(
9
)













z can be calculated using the mole balance over oxygen.












X

O2
,
air


·

(


Φ
primary

+

Φ
secondary


)


+


X
O2

·

Φ
recirculation

·


=



X
O2

·

Φ
fluegas


+


1
2

·

(


2
·

X
C


+


1
2


y

-
z

)

·

Φ
CHyOz







(
10
)













Combination of the carbon balance, nitrogen balance and oxygen balance yields









z
=


2
·

X
C


+


1
2

·
y

-


2
·

X
C

·

X
N2

·

X

02
,
air





X
CO2

·

X

N2
,
air




+


2
·

X
C

·

X
O2



X
CO2







(
11
)













From this equation it follows that z is not dependent on the primary and secondary air flow rates (Φ


primary


, Φ


secondary


, and Φ


tot


) and the flue gas circulation flow rates. For the calculation of z, only the flue gas composition needs to be measured. A logical consequence of this is that for instance leakage airs do not have any influence on the calculation of z either. In fact, additional air translates into a change of the flue gas composition, such that z remains equal.




The molar flow of water in the waste (Φ


H2O


, [mol/s] can be calculated using the mole balance over water:






Φ


H




2O




+X




H2O,air


.(Φ


primary





secondary


)+


X




H2O





recirculation





.y





CHyOz




=X




H2O





fluegas


  (12)






Description of this equation gives:










Φ
H2O

=


(




X
H2O

·

X

N2
,
air




X
N2


-

X

H2O
,
air


-


1
2

·
y
·



X
CO2

·

X

N2
,
air





X
C

·

X
N2





)

·

(


Φ
primary

+

Φ
secondary


)






(
13
)













The mole mass of the combustible part of the waste (M


CHyOz


, [kg/mol]) is equal to








M




CHyOz


=0.012+0.001


y


+0.016


z


  (14)






The heat of combustion of the combustible part of the waste (H


CHyOz


, [J/kg]) can be calculated using Michel's equation:










H
CHyOz

=



408.4
+

102.4
·
y

-

156.8
·
z



M
CHyOz


·

10
3






(
15
)













Formula 15 too is independent of the flow rates mentioned.




Next, it is chosen to characterize the combustion process on the basis of the ash-free waste composition. The inert part of the waste will therefore initially not be included in the calculations. There are two reasons for this. First, inclusion of the inert part introduces an additional uncertainty into the calculation because the exact value of the inert fraction is not known. Second, only the heat capacity of the inert part has any influence on the energy balance of the incinerator. This heat capacity, however, is small with respect to the total energy content of the incinerator.




The moisture fraction based on the ash-free waste (X


H2O,ash-free


, [kg water/kg ash-free] can now be calculated as follows:










X

H2O
,
ashfree


=



Φ
H2O

·

M
H2O





Φ
H2O

·

M
H2O


+


Φ
CHyOz

·

M
CHyOz








(
16
)













Elaboration of this equation yields:










X

H2O
,
ashfree


=


M
H2O



M
H2O

+


1

(




X
H2O

·

X
C



X
CO2


-



X

H2O
,
air


·

X
c

·

X
N2




X
CO2

·

X

N2
,
air




-


1
2

·
y


)




M
CHyOz








(
17
)













From this equation, it follows that the moisture fraction is also independent of the flow rates.




The ash-free heating value (H


waste,ash-free


, [J/kg ash-free]) is now equal to:







H




waste,ash-free


=(1


−X




H2O,ash-free


).


H




CHyOz




−X




H2O,ash-free




.H




evap


  (18)




H


evap


is the evaporative value of water and is equal to 2,444, 10


6


J/kg. The ash-free heating value can therefore be calculated if the flue gas composition is measured and if a particular value is chosen for y and X


c


. Also needed are the constant values determined on the basis of the formulae 1 to 4. The amount of heat (Q


heat


, [W]) which is released upon the combustion is equal to:










Q
heat

=


H

waste
,
ashfree


·



Φ
CHyOz

·

M
CHyOz



1
-

X

H2O
,
ashfree









(
19
)













If the inert fraction of the waste (X


inert


, [kg inert/kg waste]) is known, the following four calculations can be carried out. First, the waste flow (Φ


waste


, [kg/s]) can be calculated using the following formula:










Φ
waste

=




Φ
CHyOz

·

M
CHyOz


+


Φ
H2O

·

M
H2O




1
-

X
inert







(
20
)













The moisture fraction of the waste (X


H2O


, [kg water/kg waste]) can now be calculated as follows:










X
H2O

=



Φ
H2O

·

M
H2O



Φ
waste






(
21
)













The heating value of the total waste (H


waste


, [J/kg waste]) is now equal to:








H




waste


=(1


−X




inert




−X




H2O,waste


).


H




CHyOz,




−X




H20,waste




.H




evap


  (22)






For this heating value, in principle the same holds true as for the ash-free heating value. The heating value of the total waste is independent of the value of the flow rates.




The fraction of uncombusted (X


uncombusted


, [kg C/kg ash]) can be calculated using the following relation:










X
uncombusted

=



(

1
-

X
C


)

·
0.012





M
CHy



Oz
·

X
inert




1
-

X
inert

-

X

H2O
,
waste




+


(

1
-

X
C


)

·
0.012







(
23
)













Since it has been chosen to fix the y value, an analysis of the waste composition was carried out. On the basis of the standard composition of waste as used in the FACE model, an estimate of the variation in y and z was made. In Table 1 the composition of different components of combustible is represented.












TABLE 1











Standard composition of the FACE model
















Component




C




H




O




Water




Inert









Paper




0.3313




0.0473




0.3026




0.2364




0.0824






Plastic




0.6917




0.1039




0.0209




0.1000




0.0835






GFT




0.1860




0.0251




0.1394




0.5114




0.1381






Inert




0.0000




0.0000




0.0000




0.0000




1.0000














On the basis of the data from Table 1, the values of y and z for the different components can be calculated. These values are represented in Table 2.












TABLE 2











y and z values of CHyOz for combustible components















Component




y




z











Paper




1.713




0.685







Plastic




1.803




0.023







GFT




1.619




0.562















The value of y therefore varies at a maximum between 1.6 and 1.8 and the value of z between 0.0 and 0.7. On the basis of the waste composition of the waste in random waste incineration plants, an estimate was made of the average waste composition. In Table 3, three different waste compositions are represented in which the plastic and GFT (Vegetables/Fruit/Garden Refuse) fraction are strongly varied.












TABLE 3









Waste composition




























Component










Paper




0.34




0.34




0.34







Plastic




0.11




0.25




0.05







GFT




0.37




0.23




0.43







Inert




0.18




0.18




0.18







Total waste







y




1.71




1.75




1.69







z




0.46




0.32




0.54







Inert




0.27




0.26




0.27







Water




0.28




0.22




0.31















Accordingly, the value of y is fairly constant for different waste compositions. A good estimate of y is 1.72.




Another fixed variable is the carbon conversion. The value of X


c


is directly coupled to the percentage of uncombusted. In practice, this value varies between 0 and 5%, which corresponds to a value of 1 to 0.95 for X


c


. A good estimate of X


c


is 0.98.




The plant according to

FIG. 1

further comprises sensor means for measuring the concentrations of CO


2


, O


2


, and H


2


O in the flue gas. Further, the sensor means


42


are suitable for measuring the concentration of the flue gas. Thus, on the basis of the concentration of CO


2


and the concentration of the flue gas, the fraction X


CO2


is known. The fraction X


CO2


indicates the number of moles of CO


2


per mol of flue gas. Entirely by analogy, therefore, the fractions X


O2


and X


H2O


in the flue gas are known. The information obtained by means of the sensor means is supplied via line


44


to the computer


12


.




The computer


12


is arranged for determining, on the basis of the fractions X


CO2


, X


O2


and X


H2O


in the flue gas, the composition (y/z) and/or the heating value (H


CHyOz


, [J/kg]) of the combustible part CH


y


O


z


of the matter supplied to the system. In use, the computer calculates the value of z on the basis of the formulae:









z
=


2
·
Xc

+


1
2

·
y

-


2
·

X
C

·

X

N

2


·

X

02
,
air





X

CO

2


·

X

N2
,
air




+


2
·

X
C

·

X

O

2




X

CO

2








(
11
)













and








X




N2


=1


−X




O2




−X




H2O




−X




CO2


  (5)






The predetermined constant values X


O2,air


and X


N2,air


can be determined beforehand on the basis of the formulae 1 to 4 and be inputted into the computer.




Also, an estimate of the value of y can be inputted into the computer beforehand. As noted, a good estimate is y=1.72. An estimate of the carbon conversion X


c


can also have been inputted into the computer beforehand. As noted, a good estimate is X


c


=0.98.




In use, the computer calculates the value of H


CHyOz


.










H
CHyOz

=



408.4
+

102.4
·
y

-

156.8
·
z



M
CHyOz


·

10
3






(
15
)













and








M




CHyOz


=0.012+0.001


y


+0.016


z


  (14)






The system further comprises sensor means


46


and


48


, schematically indicated in

FIG. 1

, for respectively determining the flow rate Φ


primary


of the primary amount of air which is supplied to the incinerator by means of the air supply means


10


, as well as the flow rate Φ


secondary


of the secondary amount of air which is supplied to the incinerator via the inlet


25


. The sensor means


46


and


48


are likewise connected to the computer


12


for transmitting the flow rates to the computer. The computer


12


is arranged for determining the total flow rate of the air supplied to the incinerator, with Φ


tot





primary





secondary


. The computer is further arranged for determining on the basis of the measured fractions X


CO2


, X


O2


and X


H2O


as well as the measured air flow Φ


tot


, the ash-free heating value H


waste,ash-free


, [J/kg ash-free]) and/or the amount of heat (Q


heat


, [W]) which is released upon the combustion.




More particularly, in use, the computer determines the ash-free heating value H


waste,ash-free


on the basis of the formula:










X

H2O
,
ashfree


=


M
H2O



M
H2O

+


1

(




X
H2O

·

X
C



X
CO2


-



X

H2O
,
air


·

X
c

·

X
N2




X
CO2

·

X

N2
,
air




-


1
2

·
y


)




M
CHyOz








(
17
)













wherein M


H2O


represents the molar mass of water and H


evap


the evaporative heat of water. It is noted that for calculating the other heating values the value of Φ


tot


is not relevant. The constant values for M


H2O


and H


evap


have been priorily inputted into the computer. Further, the computer determines, in use, the amount Q


heat


which is released upon the combustion, on the basis of the formulae:











Q
heat

=


H

waste
,




ashfree


·



Φ
CHyOz

·

M
CHyOz



1
-

X

H2O
,
ashfree






;
and




(
19
)







Φ
CHyOz

=




X
CO2

·

X

N2
,
air





X
C

·

X
N2





(


Φ
primary





+





Φ
secondary


)






(
9
)













For carrying out this calculation, the measured value of Φ


tot


therefore is relevant.




The computer is further arranged to determine, on the basis of the predetermined value of the inert fraction of the waste (X


inert


, [kg inert/kg waste]), the following four parameters on the basis of the formulae 20 to 23, respectively: the waste flow Φ


waste


, [kg/s]), the moisture fraction of the waste (X


H2O,waste


, [kg water/kg waste]), the heating value of the total waste (H


waste


, [J/kg waste]) and/or the fraction of uncombusted (X


unombusted


, [kg C/kg ash]). The computer therefore determines, in use, Φ


waste


on the basis of the following formula:







Φ
waste

=




Φ
CHyOz

·

M
CHyOz


+


Φ
H2O

·

M
H2O




1




-





X
inert













In use, the computer calculates the value of X


H2O


on the basis of the following formula:







X
H2O

=



Φ
H2O

·

M
H2O



Φ
waste












Further, it holds that, in use, the computer calculates H


waste


on the basis of the following formula:








H




waste


=(1


−X




inert




−X




H2O


).


H




CHyOz




−X




H2O




.H




evap


.






Also, it holds that, in use, the computer determines X


uncombusted


on the basis of the following formula:










X
uncombusted

=



(

1




-





X
C


)

·
0.012





M
CHyOz

·

X
inert



1
-

X
inert

-

X

H2O
,
waste




+


(

1




-





X
C


)

·
0.012







(
23
)













In the system, the computer can control the waste incineration process on the basis of one or more of the parameters calculated. Thus, for instance, on the basis of the determined amount of heat released upon the combustion (Q


heat


), the ash-free heating value H


waste,ash-free


) and/or the heating value of the total waste (H


waste


), it is possible to control the amount of air and/or the temperature of the air which is supplied to the incinerator


2


by means of the air supply means


10


,


25


. Also, on the basis of other parameters which have been calculated using the computer


2


, these and/or other settings of the incinerator can be controlled, such as the speed of the conveying means


8


, a metering slide of the entrance


4


, the setting of the valves


18


,


28


, and so forth. Such variants are each understood to fall within the scope of the invention.



Claims
  • 1. A system for determining process parameters relating to thermal combustion processes of matter such as, for instance, waste in an incinerator, comprising sensor means and a computer coupled thereto for determining the parameters, wherein, in use, matter having a combustible part CHyOz is supplied to the incinerator and combusted, thereby forming a flue gas, characterized in that the sensor means are arranged for measuring the fractions XCO2, XO2 and XH2O in the flue gas and that the computer is arranged for determining, on the basis of the measured fractions, the composition (y/z) and/or the heat of combustion (HCHyOz, [J/kg]) of the combustible part CHyOz, with XO2, XH2O, XCO2 respectively representing the fractions of O2, H2O and CO2 in the flue gas.
  • 2. A system according to claim 1, characterized in that, in use, the computer calculates the value of Z on the basis of the formulae: z=2·Xc+12·y-2·XC·XN⁢2·X02, ⁢airXCO⁢2·XN2,air+2·XC·XO⁢2XCO⁢2(11)andXN2=1−XO2−XH2O−XCO2  (5) wherein XO2,air (the oxygen fraction in air supplied to the incinerator), XN2,air (the nitrogen fraction in air supplied to the incinerator), Xc (the uncombusted fraction of carbon) and y are predetermined constant values.
  • 3. A system according to claim 2, characterized in that the predetermined value Xc is between 0.90 and 1.
  • 4. A system according to claim 2, characterized in that, in use, the computer calculates the value of HCHyOz on the basis of the formulae: HCHyOz=408.4+102.4·y-156.8·zMCHyOz·103(15)andMCHyOz=0.012+0.001y+0.016z  (14)
  • 5. A system according to claim 4, characterized in that, in use, the computer determines the ash-free heating value Hwaste,ash-free on the basis of the formulae:Hwaste,ash-free=(1−XH2O,ash-free).HCHyOz−XH2O,ash-free.Hevap  (18) and XH2O,ashfree=MH2OMH2O+1(XH2O·XcXCo2-XH2O,air·Xc·XN2XCO2·XN2,air-12·y)⁢MCHyOz(17)wherein MH2O represents the known molar mass of water and Hevap represents the known evaporative heat of water.
  • 6. A system according to claim 1, characterized in that the system further comprises sensor means for determining the air flow Φtot of the air which, in use, is supplied to the incinerator, the computer being arranged to determine on the basis of the measured fractions XCO2, XO2 and XH2O, the ash-free heating value (Hwaste,ash-free, [J/kg ash-free]) and/or, further on the basis of the measured air flow Φtot, the amount of heat (Qheat, [W]) which is released upon the combustion.
  • 7. A system according to claim 6, characterized in that, in use, the computer determines the amount of Qheat which is released upon the combustion, on the basis of the formulae: Qheat=Hwaste, ⁢ashfree·ΦCHyOz·MCHyOz1-XH2O,ashfree;and(19)ΦCHyOz=XCO2·XN2,airXC·XN2⁢(Φprimary⁢ + ⁢Φsecondary)(9)
  • 8. A system according to claim 6, characterized in that the computer is further arranged for determining, on the basis of the predetermined value of the inert fraction of the waste (Xinert, [kg inert/kg waste]), the following parameters: the waste flow (Φwaste, [kg/s]), the moisture fraction of the waste (XH2O,waste, [kg water/kg waste]), the heating value of the total waste (Hwaste, [J/kg waste]) and/or the fraction of uncombusted (Xuncombusted, [kg C/kg ash]).
  • 9. A system according to claim 8, characterized in that, in use, the computer determines Φwaste on the basis of the following formula: Φwaste=ΦCHyOz·MCHyOz+ΦH2O·MH2O1⁢ - ⁢Xinert(20)
  • 10. A system according to claim 9, characterized in that, in use, the computer calculates XH2O,waste on the basis of the following formula: XH2O=ΦH2O·MH2OΦwaste(21)
  • 11. A system according to claim 10, characterized in that, in use, the computer calculates Hwaste on the basis of the following formula:Hwaste=(1−Xinert−XH2O).HCHyOz−XH2O.Hevap  (22)
  • 12. A system according to claim 10, characterized in that, in use, the computer determines Xuncombusted on the basis of the following formula: Xuncombusted=(1⁢ - ⁢Xc)·0.012MCHy⁢Oz·Xinert1-Xinert-XH2O,waste+(1⁢ - ⁢Xc)·0.012(23)
Priority Claims (2)
Number Date Country Kind
1012239 Jun 1999 NL
1014516 Feb 2000 NL
PCT Information
Filing Document Filing Date Country Kind
PCT/NL00/00377 WO 00
Publishing Document Publishing Date Country Kind
WO00/75569 12/14/2000 WO A
US Referenced Citations (7)
Number Name Date Kind
4101632 Lamberti Jul 1978 A
4758519 Nakao et al. Jul 1988 A
4895082 Mindermann et al. Jan 1990 A
4984524 Mindermann et al. Jan 1991 A
5280756 Labbe Jan 1994 A
5915310 Hura et al. Jun 1999 A
6182584 Gaudio Feb 2001 B1