Caterpillar Patenting Diesel Engines With OCP Fuel Injection
We all knew it was only a matter of time before the
diesel manufacturers started using OCP. I say this bexause Mercury Marine is now selling Optimax out boards burning JP-5 to the US Military. Also E P Bassus is converting Tohatsu OCP to burn a variety of heavy fuels to the UK Military. Orbital has known for many years that diesel would work with OCP injectors. Now it is happening. I look for a variety of 2S and 4S heavy fuel applications, both SIDI and CIDI using Orbital's OCP fuel injection systems.
Similar to Gasoline OCP, except air and EGR gasses are mixed and
compressed to the desirable temperature and pressure prior to
entering the OCP injector to be mixed with diesel.
United States Patent Application 20040112344
Kind Code A1
Wark, Christopher G. ; et al. June 17, 2004
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Temperature control for gas assisted fuel delivery
Abstract
A method and apparatus for atomizing fuel being delivered for
combustion. The method and apparatus includes providing a stream of
pressurized gas, controlling a temperature of the stream of gas to a
desired temperature, and injecting a quantity of fuel into the stream
of gas, wherein the desired temperature is selected to atomize the
fuel to a desired fuel droplet size.
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Inventors: Wark, Christopher G.; (Peoria, IL) ; Choi, Cathy Y.;
(Morton, IL)
Correspondence Name and Address: CATERPILLAR INC.
100 N.E. ADAMS STREET
PATENT DEPT.
PEORIA
IL
616296490
Serial No.: 321157
Series Code: 10
Filed: December 17, 2002
U.S. Current Class: 123/568.15; 123/585
U.S. Class at Publication: 123/568.15; 123/585
Intern'l Class: F02M 025/07
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Claims
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What is claimed is:
1. A method for atomizing fuel being delivered for combustion,
including the steps of: providing a stream of pressurized gas;
controlling a temperature of the stream of gas to a desired
temperature; and injecting a quantity of fuel into the stream of gas;
wherein the desired temperature is selected to atomize the fuel to a
desired fuel droplet size.
2. A method, as set forth in claim 1, wherein providing a stream of
pressurized gas includes the step of providing a stream of
pressurized air.
3. A method, as set forth in claim 1, wherein providing a stream of
pressurized gas includes the step of providing a stream of
pressurized exhaust gas recirculation (EGR) gas.
4. A method, as set forth in claim 1, wherein providing a stream of
pressurized gas includes the step of providing a stream of at least
one of pressurized air and pressurized exhaust gas recirculation
(EGR) gas.
5. A method, as set forth in claim 1, wherein controlling a
temperature of the stream of gas includes the step of controlling a
temperature of the stream of gas to a temperature within a range from
about 100 degrees Celsius to about 500 degrees Celsius.
6. A method, as set forth in claim 1, wherein controlling a
temperature of the stream of gas includes the step of controlling a
temperature of the stream of gas to a temperature within a range from
about 300 degrees Celsius to about 500 degrees Celsius.
7. A method, as set forth in claim 1, wherein the desired temperature
is selected to atomize the fuel to a desired fuel droplet size of
about 10 microns.
8. A method, as set forth in claim 1, wherein the desired temperature
is selected to atomize the fuel to a desired fuel droplet size of
less than 10 microns.
9. A method, as set forth in claim 1, wherein injecting a quantity of
fuel includes the step of injecting a quantity of liquid fuel into
the stream of gas.
10. A method for providing atomized fuel to a combustion chamber,
including the steps of: providing a stream of gas; pressurizing the
gas to a desired pressure; controlling a temperature of the stream of
gas to a desired temperature; and injecting a quantity of fuel into
the stream of gas; wherein the desired pressure and the desired
temperature are selected to provide atomized fuel at less than a
specified fuel droplet size.
11. An apparatus for atomizing fuel being delivered for combustion,
comprising: a source of gas being delivered in a stream; a compressor
located such that the stream of gas passes therethrough and is
pressurized; a temperature control unit located such that the stream
of gas passes therethrough and is controlled to a desired
temperature; a fuel injector for injecting fuel into the stream of
gas after the gas passes through the compressor and the temperature
control unit, wherein the fuel is atomized to a desired fuel droplet
size as a function of the desired temperature; and a combustion
chamber for receiving the atomized fuel for combustion.
12. An apparatus, as set forth in claim 11, wherein the source of gas
is at least one of air and exhaust gas recirculation (EGR) gas.
13. An apparatus, as set forth in claim 11, wherein the desired
temperature is within a range from about 100 to 500 degrees Celsius.
14. An apparatus, as set forth in claim 11, wherein the desired
temperature is within a range from about 300 to 500 degrees Celsius.
15. An apparatus, as set forth in claim 11, wherein the desired fuel
droplet size is about 10 microns.
16. An apparatus, as set forth in claim 11, wherein the desired fuel
droplet size is less than 10 microns.
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Description
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TECHNICAL FIELD
[0001] This invention relates generally to a method and apparatus for
atomizing a liquid fuel and, more particularly, to a method and
apparatus for controlling a size of atomized fuel droplets by
temperature control of a gas for gas assisted fuel delivery.
BACKGROUND
[0002] Atomization of a liquid, e.g., a liquid fuel used for
combustion, is often desired. For example, when introducing a liquid
fuel into a combustion chamber, the most efficient combustion takes
place when the fuel is completely vaporized and preferably when the
fuel has completely and thoroughly mixed with ambient gases also
present in the chamber. The fuel vaporizes more quickly and readily
when the fuel has been atomized to the smallest droplet size
possible.
[0003] Gas assist injectors have long been used to atomize fuel prior
to entry into combustion chambers. For example, in U.S. Pat. No.
4,759,335, Ragg et al. disclose a system which injects fuel directly
into a combustion chamber by the use of compressed gas, i.e.,
compressed air.
[0004] More recently, in U.S. Pat. No. 5,241,938, Takagi et al.
disclose a fuel injector which includes an air assist passage for
atomizing the fuel during injection.
[0005] In U.S. Pat. No. 5,746,189, Kuzuya et al. disclose a gas
assist system in which exhaust gas recirculation (EGR) gas is used
with gas assist injectors. The EGR gas offers the added benefit of
keeping combustion temperature down in the combustion chamber.
[0006] All of the above listed references and others are effective to
atomize fuel to an extent, but may not be sufficient for some
applications, such as when a homogeneous mixture of fuel and air is
desired.
[0007] The present invention is directed to overcoming one or more of
the problems as set forth above.
"SUMMARY OF THE INVENTION
[0008] In one aspect of the present invention a method for atomizing
fuel being delivered for combustion is disclosed. The method
includes the steps of providing a stream of pressurized gas,
controlling a temperature of the stream of gas to a desired
temperature, and injecting a quantity of fuel into the stream of
gas, wherein the desired temperature is selected to atomize the fuel
to a desired fuel droplet size.
[0009] In another aspect of the present invention an apparatus for
atomizing fuel being delivered for combustion is disclosed. The
apparatus includes a source of gas being delivered in a stream, a
compressor located such that the stream of gas passes therethrough
and is pressurized, a temperature control unit located such that the
stream of gas passes therethrough and is controlled to a desired
temperature, a fuel injector for injecting fuel into the stream of
gas after the gas passes through the compressor and the temperature
control unit, wherein the fuel is atomized to a desired fuel droplet
size as a function of the desired temperature, and a combustion
chamber for receiving the atomized fuel for combustion.
BRIEF DESCRIPTION OF THE DRAWINGS
[0010] FIG. 1 is a block diagram illustrating a preferred embodiment
of the present invention;
[0011] FIG. 2 is a block diagram illustrating an alternate
embodiment of the present invention;
[0012] FIG. 3 is a block diagram illustrating yet another alternate
embodiment of the present invention; and
[0013] FIG. 4 is a flow diagram illustrating a preferred method of
the present invention.
DETAILED DESCRIPTION
[0014] Referring to the drawings, a method and apparatus 100 for
atomizing fuel being delivered for combustion is disclosed.
[0015] Referring to FIG. 1 in particular, a block diagram
illustrating a preferred embodiment is shown. A combustion chamber
102 receives fuel and air, combusts the fuel/air mixture, and
exhausts the gases from combustion. The combustion chamber 102 may
be part of an internal combustion engine (not shown), as is well
known in the art.
[0016] A portion of the exhaust gas may be routed through an exhaust
gas recirculation (EGR) system 110. EGR systems are well known in
the art and need not be described further.
[0017] The EGR gas may be sent through a fuel injector 104, in
particular, a gas assist fuel injector 104. Gas assist fuel
injectors are configured to pass a stream of high pressure gas
therethrough. Fuel, in particular liquid fuel such as diesel,
gasoline, and the like, is received by the fuel injector 104, which
causes the fuel to enter the stream of gas. The gas assisted fuel
then atomizes prior to entry into the combustion chamber. It is
noted that the fuel injector 104 may be configured for injection
into an intake port (not shown) or directly into the combustion
chamber 102.
[0018] The EGR gas may pass through a compressor 108 prior to
entering the fuel injector 104. Gas assist injectors typically
require the gas to enter under pressure high enough to overcome the
pressure in the combustion chamber 102. Although the EGR gas may
have enough pressure initially, it may be required under some engine
operating conditions to compress the gas still further.
[0019] In the preferred embodiment, the EGR gas passes through a
temperature control unit 106 prior to entering the fuel injector
104. An elevated temperature of the gas is desired for the present
invention. Preferably, the temperature of the gas as it enters the
fuel injector 104 is within a range from about 100 degrees Celsius
to about 500 degrees Celsius. More particularly, it is preferred
that the temperature of the gas is within a range from about 300
degrees Celsius to about 500 degrees Celsius. Typical temperatures
of gases for gas assist injectors, as used in the cited art
references, range from about 30 degrees Celsius to about 50 degrees
Celsius.
[0020] The temperature control unit 106 may increase the temperature
of the gas to a desired value. However, the temperature control unit
106 may also decrease the temperature of the gas, for example when
EGR gas is used and the temperature already exceeds the desired
value. Although an elevated temperature of the gas is desired to
achieve the desired results, a temperature which exceeds the desired
range, e.g., above 500 degrees Celsius, may cause coking in the
combustion chamber 102, may cause combustion to take place too soon,
and may cause excessive component wear.
[0021] Referring to FIG. 2, a block diagram depicting an alternate
embodiment of the present invention is shown.
[0022] The exhaust gas from the combustion chamber 102 passes
through a turbo-charger 202. In addition, fresh air enters the turbo-
charger 202. It is well known in the art that the exhaust gas passes
through a turbine portion (not shown) of the turbo-charger 202,
which drives a compressor portion (not shown), which in turn
compresses the air entering the turbo-charger 202. The compressed
air is then delivered to an engine as intake air, preferably through
an intake manifold (not shown).
[0023] In the embodiment of FIG. 2, however, a portion of the
compressed air is delivered to the fuel injector 104, for use in gas
assisted injection of the fuel. The compressed air may, however,
first pass through a temperature control unit 106 to achieve a
desired temperature of the air. Although the turbo-charger 202 may
heat the air somewhat during the compression process, it may be
desired to heat the air an additional amount. Alternatively, it may
be desired to cool the air an amount to achieve the desired
temperature prior to entering the fuel injector 104.
[0024] Referring to FIG. 3, a block diagram illustrating another
alternate embodiment of the present invention is shown.
[0025] A source of fresh air is delivered to a compressor 108. The
compressor 108 may be an isolated air compressor used primarily for
purposes of the present invention, or may be a compressor used for
some other purpose as well, such as an air brake compressor on a
large truck.
[0026] The compressed air is delivered to the fuel injector 104 for
gas assist purposes as described above. Preferably, the compressed
air is delivered through a temperature control unit 106 to either
heat or cool the air to the desired temperature.
INDUSTRIAL APPLICABILITY
[0027] Operation of the present invention may best be described with
reference to the flow diagram of FIG. 4, which depicts a preferred
method of the present invention.
[0028] In a first control block 402, a stream of gas is provided.
The stream of gas may be air, EGR gas or some other suitable source
of gas for use in a gas assist injector.
[0029] In a second control block 404, the stream of gas is
pressurized, for example by one of the compressor methods described
above.
[0030] In a third control block, the temperature of the gas is
controlled to within a desired temperature range, for example from
about 300 degrees Celsius to about 500 degrees Celsius. It is noted
that, although compression of the gas is described as taking place
prior to temperature control of the gas, it may be desired to
achieve temperature control prior to compression without deviating
from the scope of the invention.
[0031] In a fourth control block 408, fuel is injected into the
stream of gas as the gas passes through the fuel injector 104.
Preferably, the chosen temperature of the gas results in atomization
of the fuel into droplets having a size of about 10 microns and
less. Without temperature control of the gas, typical fuel droplet
size would range from about 30 to about 100 microns.
[0032] Other aspects can be obtained from a study of the drawings,
the disclosure, and the appended claims. "
Have a nice day, Tom