Field of the Invention
[0001] This invention relates to cogeneration and is more particularly concerned with a
cogeneration process which ensures low NOX content of the evolved gases.
Background of the Invention
[0002] Some combustion processes generate effluent gases having an unacceptable NOX content.
Thus, oxides of nitrogen are one of the principal contaminants emitted by combustion
processes. In every combustion process, the high temperatures at the burner result
in the fixation of some oxides of nitrogen. These compounds are found in stack gases
mainly as nitric oxide (NO) with lesser amounts of nitrogen dioxide (NO₂) and only
traces of other oxides. Since nitric oxide (NO) continues to oxidize to nitrogen dioxide
(NO₂) in the air at ordinary temperatures, there is no way to predict with accuracy
the amounts of each separately in vented gases at a given time. Thus, the total amount
of nitric oxide (NO) plus nitrogen dioxide (NO₂) in a sample is determined and referred
to as "oxides of nitrogen (NOX)".
[0003] Oxides of nitrogen emissions from stack gases, through atmospheric reactions, produce
"smog" that stings eyes and causes acid rains. For these reasons, the content of oxides
of nitrogen present in gases vented to the atmosphere is severely limited by various
state and federal agencies.
[0004] Cogeneration is a process which emits stack gases of undesirable NOX content.
[0005] Cogeneration is the simultaneous production of both useful thermal energy (usually
steam) and electrical energy from one source of fuel. One or more gas turbines followed
by a waste heat boiler using natural gas as fuel for both the turbines and to heat
the exhaust gases from the turbines represent a typical system.
[0006] In recent years, the cogeneration market has expanded rapidly due in part to the
Public Utility Regulatory Policy Act of 1978. PURPA gave financial incentive to cogenerators
that sell excess electrical power and requires that utilities purchase power from
cogenerators. It also allows utilities to own up to 50% of a cogeneration facility
and receive the benefits of this status.
[0007] One problem with this system is the level of NOX emissions generated with the combined
firing cycle. Cogeneration plants using conventional gas turbines and auxiliary fuel
fired heat recovery boilers to produce electricity and steam are being subjected to
stringent NO
X emission standards requiring levels below the 150 ppm range. New Source Performance
Standards (NSPS) strictly limit NOX emission. To meet the regulations for NOX emissions,
several methods of NOX control have been employed. These can be classified as either
equipment modifications or injection methods. Injection methods include injection
of either water or steam into the combustion zone to lower the flame temperature and
retard the formation of NOX, since the amount of NOX formed generally increases with
increasing temperatures, or injection of ammonia to selectively reduce NOX. Water
or steam injection, however, adversely affects the overall fuel efficiency of the
process as energy is absorbed to vaporize the water or heat the steam that otherwise
would go toward heating the turbine gas and be ultimately converted into usable electricity
or steam. A process involving the injection of ammonia into the products of combustion
is shown, for example, in
Welty, U.S 4,164,546. Examples of processes utilizing ammonia injection and a reducing
catalyst are disclosed in
Sakari et al, U.S. 4,106,286; and
Haeflich, U.S. 4,572,110. Selective reduction methods using ammonia injection are expensive
and somewhat difficult to control. Thus, these methods have the inherent problem of
requiring that the ammonia injection be carefully controlled so as not to inject too
much and create a possible emission problem by emitting excess levels of ammonia.
In addition the temperature necessary for the reduction of the oxides of nitrogen
must be carefully controlled to get the required reaction rates.
[0008] Equipment modifications include modifications to the burner or firebox to reduce
the formation of NOX. Although these methods do reduce the level of NOX, each has
its own drawbacks. Combustion equipment modification affects the performance of the
turbines and limits the range of operations. Moreover, cogeneration plants of this
type employed for generating electric power and steam are being subjected to increasingly
stringent NOX emission standards, and a satisfactory emission control system is required
to minimize the undesirable emissions exhausted to the atmosphere. A selective catalytic
reduction system is presently considered by some authorities to be the best available
control technology for the reduction of NOX from the exhaust gas of a cogeneration
plant, and as a consequence is required equipment. Currently available selective catalytic
reduction systems used for the reduction of NOX employ ammonia injection into the
exhaust gas stream for reaction with the NOX in the presence of a catalyst to produce
nitrogen and water vapor. Such systems typically have an efficiency of 80-90 percent
when the exhaust gas stream is at temperature within a temperature range of approximately
600°-700° F. The NOX reduction efficiency of the system will be significantly less
if the temperature is outside the stated temperature range and the catalyst may be
damaged at higher temperatures.
[0009] The turbine exhaust temperature of most gas turbine cogeneration plants, at full
or rated load of the gas turbine engine, is conventionally between approximately 775°F
and 1050°F. Since the exhaust gas temperature is above the optimum temperature range
of the usual selective catalytic reduction system, it is necessary to reduce the temperature
of the exhaust gas stream before it passes through the system. Current practice is
to provide steam superheater and/or steam generating tubes upstream of the system
to withdraw heat from the exhaust gas stream to cool the gas to a preselected desired
nominal temperature before it passes through the system. This imposes various operating
limitations on the cogeneration plant which either seriously limit the operating range
of the gas turbine engine or require an undesirable exhaust gas bypass or other mechanism
for diverting a portion of the exhaust gas stream. Where supplementary firing is provided
to increase steam production, the supplementary firing is conventionally carried out
with an excess of air.
[0010] It is therefore an object of the present invention to provide a cogeneration system
of the type described wherein the level of NOX in the emissions is lowered in an improved
manner.
[0011] It is another object of the invention to provide a cogeneration system wherein NOX
emissions are controlled without adversely affecting the operation of the turbine.
[0012] It is a further object of the invention to provide a cogeneration system embodying
a gas turbine wherein NOX emissions are reduced without adversely affecting the fuel
efficiency of the system.
[0013] It is a still further object of the invention to provide for NOX removal in a cogeneration
system employing a gas turbine which is more economical and more readily controlled
than systems heretofore commonly employed in the cogeneration art.
Brief Summary of the Invention
[0014] In accordance with the invention, a cogeneration system is provided wherein electrical
power is generated by a gas turbine, the gaseous effluent together with sufficient
additional fuel to produce a fuel-rich, fuel-air mixture is either combusted, e.g.
in an afterburner, or is catalytically treated in a reducing atmosphere and is then
fed to a boiler to generate steam. Air is added to the gaseous effluent from the boiler
to form a lean fuel-air mixture, and this mixture is passed over an oxidizing catalyst,
with the resultant gas stream then passing to an economizer or low pressure waste
boiler for substantial recovery of its remaining heat content, and the gas, now meeting
NOX emission standards, is thereafter vented to the atmosphere. In a preferred form
of the invention, at least some of the final effluent, i.e., the effluent from the
economizer or low-pressure waste-heat boiler, is circulated to the combustor supplying
gas to the turbine.
Brief Description of the Drawings
[0015]
Figure 1 is a diagramatic flow sheet of a cogeneration system embodying a gas turbine
and embodying features of the present invention.
Figure 2 is a diagramatic flow sheet of a cogeneration system embodying a gas turbine
showing a novel method of handling the exhaust from the turbine; and
Figure 3 is a similar flow sheet showing recirculation of the gas.
Detailed Description of Preferred Embodiments
[0016] Referring now to Figure 1, (the drawings), the reference numeral 10 designates a
combustor or burner which receives fuel such as gas or naptha and compressed air and
burns the air-fuel mixture to produce a gaseous effluent which passes into a duct
12 which directs it to a gas turbine 14 which is coupled to a generator (not shown),
to produce electrical power. The turbine exhaust gas leaves through a duct 16 into
which are introduced further amounts of fuel, the amount depending upon the fuel-air
ratio in the exhaust gas from the turbine. Since there will be ample air, only fuel
is injected at this point. The amount of fuel added is selected so that there will
be 10 to 25% stoichiometric excess fuel relative to the available oxygen in the exhaust
gas from the gas turbine. The fuel added is ordinarily gas, such as natural gas. Thus,
the exhaust gaseous stream from the turbine is treated, i.e., has fuel added to it,
to produce a fuel-rich, fuel-air mixture containing 10% to 25% excess of fuel over
the oxygen stoichiometrically present. The thus-treated exhaust gas from the turbine
is then passed to an afterburner 18 wherein it is burned at a temperature of about
2000 to 3000°F. A residence time of 0.5 seconds is required to ensure that the desired
reduction of the oxides of nitrogen will occur. A greater residence time can be employed,
e.g., 1 minute or more, but serves no useful purpose. Alternatively, as seen in Figure
2, the afterburner of unit 18 can be replaced by a reducing catalyst treatment. Thus,
the fuel-enriched exhaust gas from the turbine at about 800°F. to about 1050°F. is
passed to a catalytic treatment zone 18, wherein the fuel-rich stream is passed over
a reducing catalyst, e.g., platinum-rhodium in the zero-valent state supported on
a carrier such as alumina, silica or a metal alloy. The making of such catalysts is
well known to persons skilled in the art. Catalyst volumes will vary depending on
the particular catalyst used. Ordinarily, the quantity of catalyst and the flow rate
are such that the space velocity is typically in the range of 30,000 to 50,000 hr.⁻¹
preferably 30,000 to 40,000 hr. ⁻¹.
[0017] As mentioned, Applicant has disclosed in
Mc Gill et al 4,405,587, oxides of nitrogen can be reduced by reaction in a reducing atmosphere
at temperatures in excess of 2000°F, for example 2000° to 3000°F. Combining this observation
with a gas turbine operation to generate electricity, maximum utilization of the turbine
exhaust as useful heat to generate steam can be achieved. Products from the afterburner
or the catalytic treatment zone 18 pass to and through a waste-heat boiler wherein
they are cooled to a temperature of 500 - 600°F. Thus, the heated gaseous stream passes
into a duct 20 and is led to a waste-heat boiler 22 which effectively utilizes the
heated gaseous stream to produce steam and simultaneously to cool the stream. The
gaseous effluent from the catalytic-treatment step, when it is used, which is ordinarily
at a temperature of 1000-1400°F., passes, as mentioned, to and through a waste-heat
boiler wherein the effluent is cooled to a temperature of about 500 - 600°F. The afterburner
18 when used and the waste-heat boiler 22 can, of course, be combined in the form
of a fuel-burning boiler wherein the added fuel and the exhaust gas from the turbine
are combusted to produce steam directly.
[0018] In any case, the boiler 22 discharges a waste effluent gas into a duct 24. Because
of the addition of fuel to the duct 16 and the burning or catalytic treatment of the
turbine exhaust gas in the presence of this fuel with significantly less than the
stoichiometric requirement of oxygen, i.e., under reducing conditions, the exhaust
gas in duct 24 from the boiler 22 contains not only combustion gases, but some unburned
fuel. It is, however, low in NOX and the treatment of the gases flowing through the
system has brought about a reduction of any NOX formed, or a suppression of the formation
of the NOX, without the use of ammonia or like treating system widely used in the
prior art. In order, however, to utilize to a maximum the heat potential of the gas
and any fuel which it may contain, air is added to the stream in conduit 24 and the
resulting gaseous stream is passed to a gas treatment unit 26 wherein the gas stream
is passed over an oxidizing catalyst. The amount of air is added in an amount relative
to the stream in conduit 24 such that the resulting stream will contain oxygen soichiometrically
in excess of the amount needed to burn any fuel which may be present in the stream,
e.g., 10% to 50% excess. Thus products at the boiler discharge temperature, e.g.,
500° - 600°F are mixed with air and passed over an oxidizing catalyst. Either noble
metal catalyst such as platinum or palladium or base metal oxides, such as copper
oxide, chrome oxide, or manganese oxide, or the like, may be used for this purpose.
The noble metal catalysts, e.g., platinum or palladium catalysts, are most suitable
the noble metals deposited in the zero valent state upon a support, such as alumina,
silica, kiesel-guhr, or a metal alloy, and the like. The metal oxide catalysts are
also most suitably the metal oxides supported on supports of this character. The making
of such catalysts is well known to persons skilled in the art. Catalyst volumes will
vary depending on the particular catalyst used. Ordinarily, the quantity of catalyst
and the flow rate are such that the space velocity is typically in the range of 30,000
to 50,000 hr.⁻¹. Data indicate that NOX levels in the parts per billion range can
be realized by the combined reduction-oxidation operations of this invention. The
oxidized gaseous effluent from the unit 26 passes into a conduit 27 which leads an
economizer or a low-pressure, waste-heat boiler, or the like, indicated at 28, and
the heat content of the oxidized gaseous effluent is extracted to the maximum amount
economically feasible. The cooled gas at a temperature of about 300 to 400°F is then
discharged through an outlet conduit 30 into a stack 32 and vented to the atmosphere
with the assurance that the vented effluent will complex with NOX emission standards.
It will have a NOX content of less than 50 ppm.
[0019] In a preferred form of the present invention, as seen in Figure 3, treated gaseous
effluent from conduit 30, i.e., the low NOX effluent following passage of the gas
and the subsequent heat removal in the economizer, is cycled to combustor 10 wherein
the gas stream to be fed to turbine 14 is prepared. Thus, as seen in Figure 3 of the
drawing, when effluent, e.g. flue gas, is to be re-cycled, an appropriate valve (not
shown) controls the recycle rate. At least a portion of the effluent is diverted into
line 36 which conducts the diverted effluent to combustor 10. In turbine operation,
air is added to the combustor for combustion of the fuel and a large excess of air
is also added to keep the flame temperature in the combustor from becoming so high
that the generated gas will damage the blades of the turbine. It has been observed
that the recycled effluent gas acts as a heat sink in the combustor and makes it possible
readily to prevent the turbine from over-heating. Thus, the large excess of air ordinarily
added to control the flame temperature can be eliminated so that there is less oxygen
in the effluent gas and there is an important saving of fuel needed to produce reducing
conditions.
[0020] As mentioned, in view of the presence of cycled effluent in combustor 10, the oxygen
content of the turbine exhaust will be significantly lower, which will correspondingly
lower the fuel requirement for the subsequent reducing step. The quantity of effluent
diverted can vary but, for best results the quantity of recycled effluent, e.g. flue
gas, added to the combustor will be such as is required to produce a turbine exhaust
at a temperature of 800-1000°F. with 1-2% 0₂.
[0021] One aspect of the invention is that the gas turbine 14 furnishes the total of the
combustion-supporting air for the afterburner 18, if one is used, and that care is
taken to maintain reducing conditions during this combustion, or during the catalytic
treatment at 18, by appropriate control of the supply of fuel. Another aspect of the
invention is that heat recovery in a turbine cogeneration system is maximized in a
highly economical manner and that NOX content is kept at a minimum without resort
to elaborate equipment reconstruction, without heat loss by injecting water into the
exhaust gases from the turbine, and without ammonia injection or catalytic reduction
in the presence of ammonia.
[0022] It will, or course, be understood in the foregoing description of the drawing, reference
to a combustor or heater, to turbine, afterburner, boiler, waste-heat boiler, economizer,
gas treatment unit, and the like, can utilize standard equipment well known to persons
skilled in the art. The gas treatment units, for example, can be any containers adapted
for gas passage and containing an appropriate catalyst. The turbine 14, for example,
can be of the type which produces substantially the same quantity of exhaust gas throughout
the range of its operation, as, for example, a single cycle, single shaft gas turbine.
[0023] Minimizing the formation of oxides of nitrogen in cogeneration, in accordance with
the invention, offers several advantages over the current state of the art. This process
does not require that a potentially obnoxious gas, such as ammonia, be injected into
the system; the reaction conditions do not require that a narrowly-controlled temperature
be maintained for the reduction of oxides of nitrogen to occur; the operating conditions
are compatible with conventional cogeneration conditions; and greater NOX reduction
efficiencies can be achieved.
[0024] The following examples will serve more fully to illustrate the features of the invention.
EXAMPLE I
[0025] In a typical operation, utilizing an afterburner, a combustor is fed with natural
gas to produce a combustible mixture which is combusted at a temperature of 2000°F.
to produce a stream of combustion products which are fed to a turbine to generate
electricity. The exhaust stream from the turbine, at a temperature of 800°F. contains
about 14% oxygen. Natural gas at ambient temperature is injected into this exhaust
stream to give the resultant stream a fuel content such that the fuel is 10% in stoichiometric
excess relative to the oxygen present. The resultant stream is then combusted at a
temperature of 3300°F. and since the fuel is in excess, the combustion takes place
in a reducing atmosphere. Heat present in the combustion products is at least partially
converted into steam by heat exchange with water, e.g., in boiler tubes, and the resulting
gaseous stream, which is of course, oxygen depleted, has a temperature of 500°F. To
this oxygen-depleted stream is then added air at ambient temperature in an amount
such that the resultant stream has an oxygen content which is 50% stoichiometrically
in excess relative to any fuel present in the oxygen-depleted stream to which the
air is added. The resultant oxygen-rich stream is then fed through a bed of platinum
black supported on alumina with a space velocity of 50,000 hr.⁻¹. At this point the
gaseous stream being processed has a temperature of 500°F. This temperature increases
across the catalyst bed to about 750°F. Heat is then extracted by appropriate heat
exchange to leave a final stream to be vented having a temperature of about 350°F.
and a NOX content of less than 50ppm.
EXAMPLE 2
[0026] In another typical operation, a combustor is fed with natural gas to produce a combustible
mixture which is combusted at a temperature of 800-1000°F. to produce a stream of
combustion products which are fed to a turbine to generate electricity. The exhaust
stream from the turbine, at a temperature of 800°F. contains about 14% oxygen. Natural
gas at ambient temperature is injected into this exhaust stream to give the resultant
stream a fuel content such that the fuel is 10% in stoichiometric excess relative
to the oxygen present. The resultant stream is then passed over a platinum-rhodium
catalyst (<1% supported on alumina) at a space velocity of 40,000 hr.⁻¹ and, since
the fuel is in excess, the treatment takes place in a reducing atmosphere. This catalytic
treatment causes the temperature of the stream to rise to 1400°F. Heat present in
the combustion products is at least partially converted into steam by heat exchange
with water, e.g., in boiler tubes, and the resulting gaseous stream, which is of course,
oxygen depleted, has a temperature of 500°F. To this oxygen-depleted stream is then
added air at ambient temperature in an amount such that the resultant stream has an
oxygen content which is 25-50% stoichiometrically in excess relative to any fuel present
in the oxygen depleted stream to which the air is added. The resultant oxygen-rich
stream is then fed through a bed of platinum (1<% supported on alumina) with a space
velocity of 50,000 hr.⁻¹. At this point the gaseous stream being processed has a
temperature of 500°F. This temperature increases across the catalyst bed to about
750°F. Heat is then extracted by appropriate heat exchange to leave a final stream
to be vented having a temperature of about 350°F. and a NOX content of less than 50
ppm.
EXAMPLE 3
[0027] In another operation, a combustor is fed with natural gas and combustion air to produce
a combustible mixture which is combusted at a temperature of 1700°F. to produce a
stream of combustion products which are fed to a turbine to generate electricity.
The exhaust stream from the turbine, at a temperature of 800-1000°F. contains about
14% oxygen. Natural gas at ambient temperature is injected into this exhaust stream
to give the resultant stream a fuel content such that the fuel is 10% in stoichiometric
excess relative to the oxygen present. The resultant stream is then combusted at a
temperature of 3300°F. and, since the fuel is in excess, the combustion takes place
in a reducing atmosphere. Heat present in the combustion products is at least partially
converted into steam by heat exchange with water, e.g., in boiler tubes, and the resulting
gaseous stream, which is of course, oxygen depleted, has a temperature of 500°F. To
this oxygen-depleted stream is then added air at ambient temperature in an amount
such that the resultant stream has an oxygen content which is 25-50% stoichiometrically
in excess relative to any fuel present in the oxygen-depleted stream to which the
air is added. The resultant oxygen-rich stream is then fed through a bed of platinum
black (<1% supported on alumina) with a space velocity of 50,000 hr.⁻¹. At this point
the gaseous stream being processed has a temperature of 500°F. This temperature increases
across the catalyst bed to about 750°F. Heat is then extracted by appropriate heat
exchange to leave a final stream to be vented having a temperature of about 350°F.
and a NOX content of less than 50 ppm. In order to regulate combustion in the combustor
preceding the turbine so that the gaseous effluent fed to the turbine is at a temperature
of 1700°F., 60-65% of the final effluent stream is cycled to provide a ratio of 1.75:1.0
of recycled flue gas to combustion gases.
EXAMPLE 4
[0028] In still another operation, a combustor is fed with natural gas to produce a combustible
mixture which is combusted at a temperature of 1700°F. to produce a stream of combustion
products which are fed to a turbine to generate electricity. The exhaust stream from
the turbine, at a temperature of 800°F. contains about 14% oxygen. Natural gas at
ambient temperature is injected into this exhaust stream to give the resultant stream
a fuel content such that the fuel is 10% in stoichiometric excess relative to the
oxygen present. The resultant steam is then passed over platinum-rhodium (<1% supported
on alumina) at a space velocity of 30,000 hr. ⁻¹ and, since the fuel is in excess,
the treatment takes place in a reducing atmosphere. This catalytic treatment causes
the temperature of the stream to rise to 1400°F. Heat present in the combustion products
is at least partially converted into steam by heat exchange with water, e.g., in boiler
tubes, and the resulting gaseous stream, which is of course, oxygen depleted, has
a temperature of 500°F. To this oxygen-depleted stream is then added air at ambient
temperature in an amount such that the resultant stream has an oxygen content which
is 50% stoichiometrically in excess relative to any fuel present in the oxygen-depleted
stream to which the air is added. The resultant oxygen-rich stream is then fed through
a bed of platinum black (<1% supported on alumina) with a space velocity of 50,000
hr.⁻¹. At this point the gaseous stream being processed has a temperature of 500°F.
This temperature increases across the catalyst bed to about 750°F. Heat is then extracted
by appropriate heat exchange to leave a final stream to be vented having a temperature
of about 350°F. and a NOX content of less than 50 ppm. In order to regulate combustion
in the combustor preceding the turbine so that the gaseous effluent fed to the turbine
is at a temperature of 1700°F., 65% of the final effluent stream is cycled to provide
a ratio of 1.75:1.0 of cycled effluent to combustion gases.
[0029] It will be understood that various changes may be made without departing from the
invention as defined in the appended claims and it is intended, therefore, that all
matter contained in the foregoing description and in the drawing shall be interpreted
as illustrative only and not in a limiting sense.
1. A process for low NOX cogeneration to produce electricity and heat which comprises
combusting fuel to produce a gaseous stream of combustion products, passing said gaseous
stream through a turbine to generate electricity, and to produce a gaseous exhaust
stream, adding additional fuel to said exhaust stream, to provide a fuel-rich combustible
gas stream having fuel in excess of the oxygen in said combustible gas stream, combusting
or catalytically treating with a reducing catalyst said fuel-rich combustible gas
stream in a reducing atmosphere to produce a heated oxygen-depleted gaseous stream,
converting at least a portion of the heat in said oxygen-depleted stream into steam,
adding air to said oxygen-depleted stream to produce a stoichiometric excess of oxygen
in the resultant stream relative to fuel present in said resultant stream, passing
said resultant stream over an oxidizing catalyst to produce an oxidized gaseous stream,
removing heat from said oxidized stream, and venting the resultant cooled stream.
2. A process as defined in claim 1, wherein said gaseous exhaust stream is at a temperature
of 775° to 1050°F.
3. A process as defined in claim 1, wherein said fuel is added to said gaseous exhaust
in an amount 10% to 25% stoichiometrically in excess of the oxygen present in the
resultant combustible gas stream.
4. A process as defined in claim 1, wherein said combustible gas stream is combusted
at a temperature of 2000 to 3000°F.
5. A process as defined in claim 4 wherein said combustible gas stream has a residence
time 0.5 seconds during its combustion.
6. A process as defined in claim 1, wherein said fuel-rich stream is combusted.
7. A process as defined in claim 1, wherein said fuel-rich stream is catalytically
treated.
8. A process as defined in claim 7, wherein said fuel-rich gas stream is catalytically
reacted at a temperature of 800 to 1050°F.
9. A process as defined in claim 8 wherein the space velocity of aid fuel-rich gas
stream while being catalytically treated is about 30,000 to 50,000 hr.⁻¹.
10. A process as defined in claim 1, wherein said oxygen-depleted stream is cooled
to a temperature of about 500 - 600°F. during said conversation of the heat to steam.
11. A process as defined in claim 1, wherein the space velocity of said resultant
stream passing over said oxidizing catalyst is about 30,000 to 50,000 hr. ⁻¹.
12. A process as defined in claim 1, wherein said air is added to said oxygen-depleted
stream in an amount to provide a stoichiometric excess of oxygen present in the resultant
stream of 10 to 25%.
13. A process as defined in claim 1, wherein the cooled gas vented to the atmosphere
is at a temperature of about 350 to 500°F.
14. A process as defined in claim 1, wherein the cooled gas vented to the atmosphere
has a NOX content less than 50ppm.
15. A process as defined in claim 1, further including the step of cycling at least
a portion of said oxidized stream to said step of combusting fuel.
16. A process as defined in claim 14, wherein said cycled gas stream is 60 to 65%
of said oxidized stream.
17. A system for low NOX cogeneration to produce electricity and heat which comprises
means for combusting fuel to produce a gaseous stream of combustion products, a turbine
connected to generate electricity, conduit means for passing said gaseous stream through
said turbine to effect generation of electricity, conduit means for passing the gaseous
exhaust stream from said turbine to said combusting means, means for adding additional
fuel to said exhaust stream to provide a combustible gas stream having fuel in excess
of the oxygen in said combustible gas stream, means for catalytically treating with
a reducing catalyst or combusting said combustible gas stream in a reducing atmosphere
to produce a heated oxygen-depleted gaseous stream, means for converting at least
a portion of the heat in the gaseous stream combusted in said combusting means into
steam, means for adding air to said last-named stream to produce a stoichiometric
excess of oxygen in the resultant stream relative to fuel present in said resultant
stream gas passage means containing an oxidizing catalyst, conduit means for passing
said resultant stream into said gas passage means and over said oxidizing catalyst
to produce an oxidized gaseous stream, means for removing heat from said oxidized
stream, conduit means for passing said oxidized gaseous stream from said gas passage
means to said means for removing heat, a vent, and a gas conduit connecting said means
for removing heat to said vent.
18. A system as defined in claim 17, wherein said vent is a stack.
19. A system as defined in claim 17, wherein said converting means is a boiler.
20. A system as defined in claim 17, further including means for cycling at least
a portion of said oxidized stream to said means for combusting fuel.