Not Applicable.
The disclosure relates generally to vehicle engines and more specifically, but not necessarily entirely, to engines that may be operated at high specific output, such as turbo charged or supercharged diesel and gasoline engines.
An electronically controlled fuel blending system that injects compressed natural gas into the air intake of a diesel engine resulting in lower emissions, increased fuel economy, and air fuel ration is disclosed. Air fuel ratios may be monitored and adjusted by a CPU (Central Processing Unit) and may be monitored by a user on a visual display, which outputs the monitored vital engine functions such as: fuel usage, fuel ratio, actual mileage in real time, fuel levels, fuel flow rates, altitude adjustments, GPS position and comparison of fuel consumption. The CPU may also monitor the current cost of fuel per mile per gallon at current speeds and conditions, allowing drivers to adjust driving habits to reduce fuel consumption and emission levels.
The system may use standard 3600 PSI natural gas and is capable of using up to 5000 PSI natural gas levels. These pressure levels may be controlled by a high pressure reducer, which takes the natural gas pressure levels from a high level of 3600-5000 PSI to less than 100 PSI, thereby allowing air to efficiently mix with the natural gas and provide optimal fuel hybrid mixtures.
The system may comprise a pressure reducer with an integrated heating element (12V) to eliminate: (1) icing and freezing problems; (2) formation of condensation; and (3) formation of methane from the reduction in pressure of natural gas.
The system may also comprise an electronically controlled valve, which may comprise a stepper motor actuated valve that has electronically controlled variable valve opening sizes.
The system may also comprise a natural gas nozzle assembly, which may be built as a one piece unit that replaces a short section of an air flexible air intake or may be placed in line with an air intake of an engine.
The system may also comprise a mass air flow sensor that monitors air flow and volume on the fly during use. This sensor may produce a 0-5 analog signal, which is sent to the CPU to adjust the air to gas mixture levels produced by the injection nozzle on the fly during use.
The system may also comprise an air temperature sensor that may work in conjunction with the mass air flow sensor to enable the CPU to accurately measure actual air volume entering the engine and to adjust temperature on the fly to keep efficiency levels as high as possible.
The system may also comprise a pressure sensor that may be installed on the air intake, downstream from a turbo charger. This sensor may be used to help the CPU calculate the optimum air fuel ratio.
The system may also comprise a diesel fuel flow meter that may be used to determine the diesel consumption in real time. The diesel fuel flow meter may send the CPU data that allows the display screen to display the diesel consumption that assists in the cost per mile calculation and the miles per gallon (or kilometers per liter) cost calculation displayed on the screen. That data and information may be transmitted to a computer system allowing fleet management to assist drivers in adjusting driving habits. Such data may be networked wherein a control base and fleet members form a network wherein data is exchanged in order to maximize certain parameters.
The natural gas/diesel injection system, bi-fuel, hybrid, mixing system, fuel enhancement, emission control device, may enhance combustion and fumigation. The system may incorporate a fuel metering system and fuel blending system that improves efficiency and reduces diesel fuel consumption.
The system may also comprise the components of an electronic control unit with a display screen, a regulator, a natural gas injection nozzle assembly, and multiple sensors for monitoring conditions and operation during use of the system.
The system may be microprocessor controlled, wherein current conditions may be displayed to a user on the fly during use such as natural gas and diesel fuel levels, natural gas/diesel ratio being used, current mileage MPG (separate and combined), fuel consumption maybe monitored and adjusted constantly and automatically within the bounds of the system components. The system may optimize natural gas usage, which reduces diesel consumption for the same relative and proportional power output, resulting in lower fuel costs, lower emissions, and increased power.
The system may use multiple sensors to gather input on vital engine conditions such as a mass airflow sensor allowing the system to precisely adjust for optimum air to natural gas ratio, which results in a dramatic reduction in diesel consumption. Exhaust gas temperature, temperature, pressure, natural gas flow meter, diesel flow meter, natural gas pressure sensor, are also used for the optimization method.
The system may be integrated with a vehicle's on-board computer system and may automatically adjust according to current conditions experienced by the vehicle. The driver of the vehicle may also be able to manually override certain system functions if needed.
The natural gas system maybe designed to operate within a range of 3600 PSI to 5000 PSI or higher in order to accommodate the amount of fuel desired, and to provide the vehicle with the fuel needed to travel reasonable distances between fill-ups.
The features and advantages of the disclosure will become apparent from a consideration of the subsequent detailed description presented in connection with the accompanying drawings in which:
For the purposes of promoting an understanding of the principles in accordance with the disclosure, reference will now be made to the embodiments illustrated in the drawings and specific language will be used to describe the same. It will nevertheless be understood that no limitation of the scope of the disclosure is thereby intended. Any alterations and further modifications of the inventive features illustrated herein, and any additional applications of the principles of the disclosure as illustrated herein, which would normally occur to one skilled in the relevant art and having possession of this disclosure, are to be considered within the scope of the disclosure.
Before the digital closed loop natural gas and diesel hybrid fuel blending systems and methods are disclosed and described, it is to be understood that this disclosure is not limited to the particular configurations, process steps, and materials disclosed herein as such configurations, process steps, and materials may vary somewhat. It is also to be understood that the terminology employed herein is used for the purpose of describing particular embodiments only and is not intended to be limiting since the scope of the disclosure will be limited only by the patent claims and equivalents thereof.
It must be noted that, as used in this specification and appended claims, if any, the singular forms “a,” “an,” and “the” include plural referents unless the context clearly dictates otherwise.
In describing and claiming the subject matter of the disclosure, the following terminology will be used in accordance with the definitions set out below.
As used herein, the terms “comprising,” “including,” “containing,” “characterized by,” and grammatical equivalents thereof are inclusive or open-ended terms that do not exclude additional, unrecited elements or method steps.
As used herein, the phrase “consisting of” and grammatical equivalents thereof exclude any element, step, or ingredient not specified in the claim.
As used herein, the phrase “consisting essentially of” and grammatical equivalents thereof limit the scope of a claim to the specified materials or steps and those that do not materially affect the basic and novel characteristic or characteristics of the claimed disclosure.
With reference primarily to
The turbo charger 104 may interface with the engine 102 through an inlet channel 118 that has been configured to facilitate the movement of fluids (gas or liquid) into the engine 102. The inlet channel 118 may comprise a temperature sensor 119 for sensing the temperature of the air in the inlet channel and reporting the resultant data to the computer 110. The inlet channel 118 may comprise a pressure sensor 120 for sensing the pressure of the fluid mixture in the inlet channel 118. The inlet channel 118 may comprise a pressure switch 122 configured to control the pressure of the fluids in the inlet channel 118 so as to allow control of the fluids in the inlet channel 118 as it enters the engine 102.
After the engine 102 has consumed the chemical energy of the fuel air mixture entering the engine 102 by way of the inlet channel 118, exhaust gasses enter an outlet channel 124. The outlet channel 124 may comprise an exhaust temperature sensor 126. The outlet channel 124 channels the exhaust fluids into the turbo charger 104 to actuate the working elements of a turbo charger as is well known in the art.
The system 100 may further comprise natural gas fuel tanks 130. A single natural gas fuel tank may be used or a bank or array of fuel tanks may be used. The tanks 130 may be pressurized in a range from about 2500 psi to about 7000 psi. It will be appreciated that tanks containing pressures outside that range may also be used by the disclosure and it is within the scope of this disclosure to contemplate tanks pressurized to far higher pressures or far lower pressures than provided in the above range. The pressures of the tanks 130 within the system 100 are generally pressurized such that the pressure differential between the operating pressure of the system and the pressure in the tank or tanks causes natural gas to flow from the tanks 130 to the system 100. Accordingly any pressure or means for facilitating flow from tanks into an engine system is within the scope of this disclosure.
A natural gas fuel line 132 may be used to move the natural gas from the tanks 130 into the system 100 and more particularly into a pressure reducer 138. The natural gas fuel line 132 may comprise a natural gas pressure sensor 134 configured to sense the pressure of the natural gas and send data to the computer 110. The natural gas fuel line 132 may further comprise a fuel shut-off valve 136 configured to open and close thereby stopping the flow of natural gas into the pressure reducer 138.
The pressure reducer 138 may be configured to reduce the pressure of the natural gas fluid. The pressure reducer 138 may reduce the pressure of natural gas by providing volume of space for which the natural gas may freely expand thereby reducing its pressure. As heat is transferred or absorbed into the depressurizing fluid of natural gas, a heating element 139 may be employed to control the temperature of the pressure reducer 138. By controlling the temperature of the pressure reducer 138 freezing, condensation of water, and the formation of methane can be controlled. It may be noted that the natural gas may be inserted into the air flow system at a pressure in the range from about 10 psi to about 200 psi, or over a larger or smaller range.
A natural gas flow sensor 140 may be employed in the system 100 to sense the flow of natural gas in to the system 100. A natural gas flow controller 142 may be implemented to control the flow of natural gas in the system and may be controlled by the computer 110 or another control apparatus. The natural gas flow controller 142 may operate by opening and closing a valve that physically restricts the flow of the natural gas.
A natural gas injection assembly 144 may be employed in the system 100 and may comprise a natural gas nozzle 146 that is configured to inject natural gas into the air intake 106 such that the natural gas is mixed with the incoming air thereby creating a more energy rich combustible fluid. The nozzle 146 may be configured to disperse the natural gas in a homogeneous mixture and may produce a venturi effect in order to cause greater mixing of the incoming air and the natural gas.
The sensors as discussed above and the various control mechanisms may be electronically connected to a control unit 148. The control unit 148 may comprise components typical of control units such as a processor for processing data, memory for rapid data storage and data reading, storage for storing data, and circuitry supporting the components. The control unit 148 may also be configured with a visual display for visually displaying the data generated within the system 100. The control unit 148 may further comprise audio alerts. The control unit 148 may be configured to cause the system 100 to operate within a certain set of parameters by causing various control means to control their respective subjects. The control unit 148 may be fully engaged in the system 100 there by controlling all aspects of the operation of the system 100. In an embodiment the control unit 148 may be capable of partial control thereby leaving a portion of the system control to native control elements. The control unit may further comprise a communication device 150, such as a wireless transmitter that is configured to communicate with other systems or a control base thereby forming a network. Any data transmitted to the computer can be transmitted to the control unit 148.
Referring now to
The turbo charger 204 may interface with the engine 202 through an inlet channel 218 that has been configured to facilitate the movement of fluids (gas or liquid) into the engine 202. The inlet channel 218 may comprise a temperature sensor 219 for sensing the temperature of the air in the inlet channel and reporting the resultant data to the computer 210. The inlet channel 218 may comprise a pressure sensor 220 for sensing the pressure of the fluid mixture in the inlet channel 218. The inlet channel 218 may comprise a pressure switch 222 configured to control the pressure of the fluids in the inlet channel 218 so as to allow control of the fluids in the inlet channel 218 as it enters the engine 202.
After the engine 202 has consumed the chemical energy of the fuel air mixture entering the engine 202 by way of the inlet channel 218, exhaust gasses enter an outlet channel 224. The outlet channel 224 may comprise an exhaust temperature sensor 226. The outlet channel 224 channels the exhaust fluids into the turbo charger 204 to actuate the working elements of a turbo charger as is well known in the art.
The system 200 may further comprise natural gas fuel tanks 230. A single natural gas fuel tank may be used or a bank or array of fuel tanks may be used. The tanks 230 may be pressurized in a range from about 2500 psi to about 7000 psi. It will be appreciated that tanks containing pressures outside that range may also be used by the disclosure and it is within the scope of this disclosure to contemplate tanks pressurized to far higher pressures or far lower pressures than provided in the above range. The pressures of the tanks 230 within the system 200 are generally pressurized such that the pressure differential between the operating pressure of the system and the pressure in the tank or tanks causes natural gas to flow from the tanks 230 to the system 200. Accordingly any pressure or means for facilitating flow from tanks into an engine system is within the scope of this disclosure.
A natural gas fuel line 232 may be used to move the natural gas from the tanks 230 into the system 200 and more particularly into a pressure reducer 238. The natural gas fuel line 232 may comprise a natural gas pressure sensor 234 configured to sense the pressure of the natural gas and send data to the computer 210. The natural gas fuel line 232 may further comprise a fuel shut-off valve 236 configured to open and close thereby stopping the flow of natural gas into the pressure reducer 238.
The pressure reducer 238 may be configured to reduce the pressure of the natural gas fluid. The pressure reducer 238 may reduce the pressure of natural gas by providing volume of space for which the natural gas may freely expand thereby reducing its pressure. As heat is transferred or absorbed into the depressurizing fluid of natural gas, a heating element 239 may be employed to control the temperature of the pressure reducer 238. By controlling the temperature of the pressure reducer 238 freezing, condensation of water, and the formation of methane can be controlled. It may be noted that the natural gas may be inserted into the air flow system at a pressure in the range from about 10 psi to about 200 psi, or over a larger or smaller range.
A motorized control valve 241 may be employed to control the flow of natural gas after it has been depressurized. A natural gas flow sensor 240 may be used inline after the motorized control valve 241 in order to monitor the operation of the control valve 241. A diaphragm metering valve 243 may be incorporated to react to changes in the negative pressure created in the air intake 206 as a result of the turbo charger 204. The diaphragm metering valve 243 may be passive and made of a material with a predetermined bias or elasticity to properly control the flow of the natural gas in direct response to the changes in the system 200. For example, the material may be made from silicon or from multiple layers of silicon. In an embodiment, multiple diaphragms may be used in place of a single diaphragm. A natural gas injection assembly 244 may be included to disperse the natural gas into the air flow in the air intake 206.
The sensors as discussed above and the various control mechanisms may be electronically connected to a control unit 248. The control unit 248 may comprise components typical of control units such as a processor for processing data, memory for rapid data storage and data reading, storage for storing data, and circuitry supporting the components. The control unit 248 may also be configured with a visual display for visually displaying the data generated within the system 200. The control unit 248 may further comprise audio alerts. The control unit 248 may be configured to cause the system 200 to operate within a certain set of parameters by causing various control means to control their respective subjects. The control unit 248 may be fully engaged in the system 200 thereby controlling all aspects of the operation of the system 200. In an embodiment the control unit 248 may be capable of partial control thereby leaving a portion of the system control to native control elements. The control unit may further comprise a communication device 250, such as a wireless transmitter that is configured to communicate with other systems or a control base thereby forming a network. Any data transmitted to the computer can be transmitted to the control unit 248.
With reference to
With reference to
With reference primarily to
The turbo charger 504 may interface with the engine 502 through an inlet channel 518 that has been configured to facilitate the movement of fluids (gas or liquid) into the engine 502. The inlet channel 518 may comprise a temperature sensor for sensing the temperature of the air in the inlet channel and reporting the resultant data to the computer 510. The inlet channel 518 may comprise a pressure sensor for sensing the pressure of the fluid mixture in the inlet channel 518. The inlet channel 518 may comprise a pressure switch configured to control the pressure of the fluids in the inlet channel 518 so as to allow control of the fluids in the inlet channel 518 as it enters the engine 502.
After the engine 502 has consumed the chemical energy of the fuel air mixture entering the engine 502 by way of the inlet channel 518, exhaust gasses enter an outlet channel 524. The outlet channel 524 may comprise an exhaust temperature sensor 526. The outlet channel 524 channels the exhaust fluids into the turbo charger 504 to actuate the working elements of a turbo charger as is well known in the art.
The system 500 may further comprise natural gas fuel tanks 530. A single natural gas fuel tank may be used or a bank or array of fuel tanks may be used. The tanks 530 may be pressurized in a range from about 2500 psi to about 7000 psi. It will be appreciated that tanks containing pressures outside that range may also be used by the disclosure and it is within the scope of this disclosure to contemplate tanks pressurized to far higher pressures or far lower pressures than provided in the above range. The pressures of the tanks 530 within the system 500 are generally pressurized such that the pressure differential between the operating pressure of the system and the pressure in the tank or tanks causes natural gas to flow from the tanks 530 to the system 500. Accordingly any pressure or means for facilitating flow from tanks into an engine system is within the scope of this disclosure.
A natural gas fuel line 532 may be used to move the natural gas from the tanks 530 into the system 500 and more particularly into a pressure reducer 538. The natural gas fuel line 532 may comprise a natural gas pressure sensor 534 configured to sense the pressure of the natural gas and send data to the computer 510. The natural gas fuel line 532 may further comprise a fuel shut-off valve configured to open and close thereby stopping the flow of natural gas into the pressure reducer 538.
The pressure reducer 538 may be configured to reduce the pressure of the natural gas fluid. The pressure reducer 538 may reduce the pressure of natural gas by providing volume of space for which the natural gas may freely expand thereby reducing its pressure. As heat is transferred or absorbed into the depressurizing fluid of natural gas, a heating element may be employed to control the temperature of the pressure reducer 538. By controlling the temperature of the pressure reducer 538 freezing, condensation of water, and the formation of methane can be controlled. It may be noted that the natural gas may be inserted into the air flow system at a pressure in the range from about 10 psi to about 200 psi, or over a larger or smaller range. Heat may be applied to other elements of the system 500 to control freezing and other operating conditions of the components. For example, the tanks and the natural gas lines within the system 500 may benefit from thermal control.
A natural gas flow sensor may be employed in the system 500 to sense the flow of natural gas in to the system 500. A natural gas flow controller may be implemented to control the flow of natural gas in the system and may be controlled by the computer 510 or another control apparatus. The natural gas flow controller may operate by opening and closing a valve that physically restricts the flow of the natural gas.
A natural gas injection assembly or array 544 maybe employed in the system 500 and may comprise a natural gas injector 546 or a plurality of natural gas injectors, that are configured to inject natural gas into the air intake 506 such that the natural gas is mixed with the incoming air thereby creating a more energy rich combustible fluid. The injector 546 may be configured to disperse the natural gas in a homogeneous mixture and may produce a venturi effect in order to cause greater mixing of the incoming air and the natural gas. The array 544 of injectors 546 may cause the injectors 546 to operate independently from one another or in concert, as discussed in greater detail below. The introduction of natural gas may be made prior to the turbo charger 504 or after the turbo charger 504.
The sensors as discussed above and the various control mechanisms may be electronically connected to a control unit 548. The control unit 548 may comprise components typical of control units such as a processor for processing data, memory for rapid data storage and data reading, storage for storing data, and circuitry supporting the components. The control unit 548 may also be configured with a visual display for visually displaying the data generated within the system 500 and may communicate with the computers 510 and 511. The control unit 548 may further comprise audio alerts. The control unit 548 may be configured to cause the system 500 to operate within a certain set of parameters by causing various control means to control their respective subjects. The control unit 548 may be fully engaged in the system 500 there by controlling all aspects of the operation of the system 500. In an embodiment the control unit 548 may be capable of partial control thereby leaving a portion of the system control to native control elements. The control unit may further comprise a communication device, such as a wireless transmitter that is configured to communicate with other systems or a control base thereby forming a network. Any data transmitted to the computer can be transmitted to the control unit 548. The system 500 may further include exhaust sensors 555 in order to comply with regulatory systems and requirements.
With reference primarily to
The turbo charger 604 may interface with the engine 602 through an inlet channel 618 that has been configured to facilitate the movement of fluids (gas or liquid) into the engine 602. The inlet channel 618 may comprise a temperature sensor for sensing the temperature of the air in the inlet channel and reporting the resultant data to the computer 610. The inlet channel 618 may comprise a pressure sensor for sensing the pressure of the fluid mixture in the inlet channel 618. The inlet channel 618 may comprise a pressure switch configured to control the pressure of the fluids in the inlet channel 618 so as to allow control of the fluids in the inlet channel 618 as it enters the engine 602.
After the engine 602 has consumed the chemical energy of the fuel air mixture entering the engine 602 by way of the inlet channel 618, exhaust gasses enter an outlet channel 624. The outlet channel 624 may comprise an exhaust temperature sensor 626. The outlet channel 624 channels the exhaust fluids into the turbo charger 604 to actuate the working elements of a turbo charger as is well known in the art.
The system 600 may further comprise natural gas fuel tanks 630. A single natural gas fuel tank may be used or a bank or array of fuel tanks may be used. The tanks 630 may be pressurized in a range from about 2500 psi to about 7000 psi. It will be appreciated that tanks containing pressures outside that range may also be used by the disclosure and it is within the scope of this disclosure to contemplate tanks pressurized to far higher pressures or far lower pressures than provided in the above range. The pressures of the tanks 630 within the system 600 are generally pressurized such that the pressure differential between the operating pressure of the system and the pressure in the tank or tanks causes natural gas to flow from the tanks 630 to the system 600. Accordingly any pressure or means for facilitating flow from tanks into an engine system is within the scope of this disclosure.
A natural gas fuel line 632 may be used to move the natural gas from the tanks 630 into the system 600 and more particularly into a pressure reducer 638. The natural gas fuel line 632 may comprise a natural gas pressure sensor 634 configured to sense the pressure of the natural gas and send data to the computer 610. The natural gas fuel line 632 may further comprise a fuel shut-off valve configured to open and close thereby stopping the flow of natural gas into the pressure reducer 638.
The pressure reducer 638 may be configured to reduce the pressure of the natural gas fluid. The pressure reducer 638 may reduce the pressure of natural gas by providing volume of space for which the natural gas may freely expand thereby reducing its pressure. As heat is transferred or absorbed into the depressurizing fluid of natural gas, a heating element may be employed to control the temperature of the pressure reducer 638. By controlling the temperature of the pressure reducer 638 freezing, condensation of water, and the formation of methane can be controlled. It may be noted that the natural gas may be inserted into the air flow system at a pressure in the range from about 10 psi to about 200 psi, or over a larger or smaller range. Heat may be applied to other elements of the system 600 to control freezing and other operating conditions of the components. For example the tanks and the natural gas lines within the system 600 may benefit from thermal control.
A natural gas flow sensor may be employed in the system 600 to sense the flow of natural gas in to the system 600. A natural gas flow controller may be implemented to control the flow of natural gas in the system and may be controlled by the computer 610 or another control apparatus. The natural gas flow controller may operate by opening and closing a valve that physically restricts the flow of the natural gas.
As seen in the
The sensors as discussed above and the various control mechanisms may be electronically connected to a control unit 648. The control unit 648 may comprise components typical of control units such as a processor for processing data, memory for rapid data storage and data reading, storage for storing data, and circuitry supporting the components. The control unit 648 may also be configured with a visual display for visually displaying the data generated within the system 600 and may communicate with the computers 610 and 611. The control unit 648 may further comprise audio alerts. The control unit 648 may be configured to cause the system 600 to operate within a certain set of parameters by causing various control means to control their respective subjects. The control unit 648 may be fully engaged in the system 600 there by controlling all aspects of the operation of the system 600. In an embodiment the control unit 648 may be capable of partial control thereby leaving a portion of the system control to native control elements. The control unit may further comprise a communication device, such as a wireless transmitter that is configured to communicate with other systems or a control base thereby forming a network. Any data transmitted to the computer can be transmitted to the control unit 648. The system 600 may further include exhaust sensors 655 in order to comply with regulatory systems and requirements.
With reference primarily to
The turbo charger 704 may interface with the engine 702 through an inlet channel 718 that has been configured to facilitate the movement of fluids (gas or liquid) into the engine 702. The inlet channel 718 may comprise a temperature sensor for sensing the temperature of the air in the inlet channel and reporting the resultant data to the computer 710. The inlet channel 718 may comprise a pressure sensor for sensing the pressure of the fluid mixture in the inlet channel 718. The inlet channel 718 may comprise a pressure switch configured to control the pressure of the fluids in the inlet channel 718 so as to allow control of the fluids in the inlet channel 718 as it enters the engine 702.
After the engine 702 has consumed the chemical energy of the fuel air mixture entering the engine 702 by way of the inlet channel 718, exhaust gasses enter an outlet channel 724. The outlet channel 724 may comprise an exhaust temperature sensor 726. The outlet channel 724 channels the exhaust fluids into the turbo charger 704 to actuate the working elements of a turbo charger as is well known in the art.
The system 700 may further comprise natural gas fuel tanks 730. A single natural gas fuel tank may be used or a bank or array of fuel tanks may be used. The tanks 730 may be pressurized in a range from about 2500 psi to about 7000 psi. It will be appreciated that tanks containing pressures outside that range may also be used by the disclosure and it is within the scope of this disclosure to contemplate tanks pressurized to far higher pressures or far lower pressures than provided in the above range. The pressures of the tanks 730 within the system 700 are generally pressurized such that the pressure differential between the operating pressure of the system and the pressure in the tank or tanks causes natural gas to flow from the tanks 730 to the system 700. Accordingly any pressure or means for facilitating flow from tanks into an engine system is within the scope of this disclosure.
A natural gas fuel line 732 may be used to move the natural gas from the tanks 730 into the system 700 and more particularly into a pressure reducer 738. The natural gas fuel line 732 may comprise a natural gas pressure sensor 734 configured to sense the pressure of the natural gas and send data to the computer 710. The natural gas fuel line 732 may further comprise a fuel shut-off valve configured to open and close thereby stopping the flow of natural gas into the pressure reducer 738.
The pressure reducer 738 may be configured to reduce the pressure of the natural gas fluid. The pressure reducer 738 may reduce the pressure of natural gas by providing volume of space for which the natural gas may freely expand thereby reducing its pressure. As heat is transferred or absorbed into the depressurizing fluid of natural gas, a heating element may be employed to control the temperature of the pressure reducer 738. By controlling the temperature of the pressure reducer 738 freezing, condensation of water, and the formation of methane can be controlled. It may be noted that the natural gas may be inserted into the air flow system at a pressure in the range from about 10 psi to about 200 psi, or over a larger or smaller range. Heat may be applied to other elements of the system 700 to control freezing and other operating conditions of the components. For example the tanks and the natural gas lines within the system 700 may benefit from thermal control.
A natural gas flow sensor may be employed in the system 700 to sense the flow of natural gas in to the system 700. A natural gas flow controller may be implemented to control the flow of natural gas in the system and may be controlled by the computer 710 or another control apparatus. The natural gas flow controller may operate by opening and closing a valve that physically restricts the flow of the natural gas.
A natural gas injection assembly or array 744 maybe employed in the system 700 and may comprise a natural gas injector 746 or a plurality of natural gas injectors, that are configured to inject natural gas into the air intake 706 such that the natural gas is mixed with the incoming air thereby creating a more energy rich combustible fluid. The injector 746 may be configured to disperse the natural gas in a homogeneous mixture and may produce a venturi effect in order to cause greater mixing of the incoming air and the natural gas. Shown in the corresponding figure is an array of four injectors. It is within the scope of the disclosure to anticipate any number of injectors and apply those injectors in concert. The array of injectors may be independently controlled so as to overlap one another in duration or may have multiple injectors open and close simultaneously. The array 744 of injectors 746 may cause the injectors 746 to operate independently from one another or in concert, as discussed in greater detail below. The introduction of natural gas may be made prior to the turbo charger 704 or after the turbo charger 704.
The sensors as discussed above and the various control mechanisms may be electronically connected to a control unit 748. The control unit 748 may comprise components typical of control units such as a processor for processing data, memory for rapid data storage and data reading, storage for storing data, and circuitry supporting the components. The control unit 748 may also be configured with a visual display for visually displaying the data generated within the system 700 and may communicate with the computers 710 and 711. The control unit 748 may further comprise audio alerts. The control unit 748 may be configured to cause the system 700 to operate within a certain set of parameters by causing various control means to control their respective subjects. The control unit 748 may be fully engaged in the system 700 there by controlling all aspects of the operation of the system 700. In an embodiment the control unit 748 may be capable of partial control thereby leaving a portion of the system control to native control elements. The control unit may further comprise a communication device, such as a wireless transmitter that is configured to communicate with other systems or a control base thereby forming a network. Any data transmitted to the computer can be transmitted to the control unit 748. The system 700 may further include exhaust sensors 755 in order to comply with regulatory systems and requirements.
With reference primarily to
The turbo charger 804 may interface with the engine 802 through an inlet channel 818 that has been configured to facilitate the movement of fluids (gas or liquid) into the engine 802. The inlet channel 818 may comprise a temperature sensor for sensing the temperature of the air in the inlet channel and reporting the resultant data to the computer 810. The inlet channel 818 may comprise a pressure sensor for sensing the pressure of the fluid mixture in the inlet channel 818. The inlet channel 818 may comprise a pressure switch configured to control the pressure of the fluids in the inlet channel 818 so as to allow control of the fluids in the inlet channel 818 as it enters the engine 802.
After the engine 802 has consumed the chemical energy of the fuel air mixture entering the engine 802 by way of the inlet channel 818, exhaust gasses enter an outlet channel 824. The outlet channel 824 may comprise an exhaust temperature sensor 826. The outlet channel 824 channels the exhaust fluids into the turbo charger 804 to actuate the working elements of a turbo charger as is well known in the art.
The system 800 may further comprise natural gas fuel tanks 830. A single natural gas fuel tank may be used or a bank or array of fuel tanks may be used. The tanks 830 may be pressurized in a range from about 2500 psi to about 8000 psi. It will be appreciated that tanks containing pressures outside that range may also be used by the disclosure and it is within the scope of this disclosure to contemplate tanks pressurized to far higher pressures or far lower pressures than provided in the above range. The pressures of the tanks 830 within the system 800 are generally pressurized such that the pressure differential between the operating pressure of the system and the pressure in the tank or tanks causes natural gas to flow from the tanks 830 to the system 800. Accordingly any pressure or means for facilitating flow from tanks into an engine system is within the scope of this disclosure.
A natural gas fuel line 832 may be used to move the natural gas from the tanks 830 into the system 800 and more particularly into a pressure reducer 838. The natural gas fuel line 832 may comprise a natural gas pressure sensor 834 configured to sense the pressure of the natural gas and send data to the computer 810. The natural gas fuel line 832 may further comprise a fuel shut-off valve configured to open and close thereby stopping the flow of natural gas into the pressure reducer 838.
The pressure reducer 838 may be configured to reduce the pressure of the natural gas fluid. The pressure reducer 838 may reduce the pressure of natural gas by providing volume of space for which the natural gas may freely expand thereby reducing its pressure. As heat is transferred or absorbed into the depressurizing fluid of natural gas, a heating element may be employed to control the temperature of the pressure reducer 838. By controlling the temperature of the pressure reducer 838 freezing, condensation of water, and the formation of methane can be controlled. It may be noted that the natural gas may be inserted into the air flow system at a pressure in the range from about 10 psi to about 200 psi, or over a larger or smaller range. Heat may be applied to other elements of the system 800 to control freezing and other operating conditions of the components. For example the tanks and the natural gas lines within the system 800 may benefit from thermal control.
A natural gas flow sensor may be employed in the system 800 to sense the flow of natural gas in to the system 800. A natural gas flow controller may be implemented to control the flow of natural gas in the system and may be controlled by the computer 810 or another control apparatus. The natural gas flow controller may operate by opening and closing a valve that physically restricts the flow of the natural gas.
A natural gas injection assembly or array 844 maybe employed in the system 800 and may comprise a natural gas injector 846 or a plurality of natural gas injectors, that are configured to inject natural gas into the air intake 806 such that the natural gas is mixed with the incoming air thereby creating a more energy rich combustible fluid. The injector 846 may be configured to disperse the natural gas in a homogeneous mixture and may produce a venturi effect in order to cause greater mixing of the incoming air and the natural gas. Shown in the corresponding figure is an array of four injectors. It is within the scope of the disclosure to anticipate any number of injectors and apply those injectors in concert. The array of injectors may be independently controlled so as to overlap one another in duration or may have multiple injectors open and close simultaneously. The array 844 of injectors 846 may cause the injectors 846 to operate independently from one another or in concert, as discussed in greater detail below. The introduction of natural gas may be made prior to the turbo charger 804 or after the turbo charger 804. Instructions may be derived or executed from map tables representing different operating states or conditions of use. One map table may represent data for use during a no load or light load operating state or condition. Another map table may represent data for heavy or high load operating state or condition, such as a truck that is pulling a full pay load.
The sensors as discussed above and the various control mechanisms may be electronically connected to a control unit 848. The control unit 848 may comprise components typical of control units such as a processor for processing data, memory for rapid data storage and data reading, storage for storing data, and circuitry supporting the components. The control unit 848 may also be configured with a visual display for visually displaying the data generated within the system 800 and may communicate with the computer 810. The control unit 848 may further comprise audio alerts. The control unit 848 may be configured to cause the system 800 to operate within a certain set of parameters by causing various control means to control their respective subjects. The control unit 848 may be fully engaged in the system 800 there by controlling all aspects of the operation of the system 800. In an embodiment the control unit 848 may be capable of partial control thereby leaving a portion of the system control to native control elements. The control unit may further comprise a communication device, such as a wireless transmitter that is configured to communicate with other systems or a control base thereby forming a network. Any data transmitted to the computer can be transmitted to the control unit 848. The system 800 may further include exhaust sensors 855 in order to comply with regulatory systems and requirements.
It is within the scope of the disclosure to offer the components of the system in a kit form that can be fitted to a variety of vehicles.
An embodiment may comprise a plurality of sensors for collecting operational data from the engine, wherein said operational data comprises engine speed, engine load, and mass flow into said engine, and a first controller that processes said operational data to create operational map tables for said engine. The embodiment may further comprise a second controller that instructs said engine to follow said map tables during use of said engine. The embodiment may further comprise a first map table representing a first operating mode and a second map table representing a second operating mode or condition. Additionally the embodiment may have a main fuel injector capable of directly injecting a second gaseous fuel into said combustion chamber, and a pilot fuel injector capable of injecting a pilot fuel into said combustion chamber. The embodiment may further comprise an intake conduit for directing said natural gas fuel into said combustion chamber and an array having a natural gas injector configured to inject natural gas into said intake conduit, wherein the natural gas is introduced into said combustion chamber of said engine with a primary fuel and air.
An embodiment of a system for using natural gas in combination with diesel fuel for combustion in an engine may comprise:
an engine;
a tank of natural gas;
a tank of diesel fuel;
a depressurization chamber; and
an injection assembly for injecting metered natural gas into an air take of the engine.
An embodiment of a method for using natural gas in combination with diesel fuel for combustion in an engine may comprise:
depressurizing natural gas from a pressurized state;
mixing said natural gas with air in an air in take to an engine;
supplying diesel fuel to said engine; and
supplying natural gas to said engine, such that said natural gas and said diesel fuel are mixed in a predetermined ratio thereby optimizing efficiency.
An embodiment of a network for maximizing efficiency of the operation of network members may comprise:
a first data set relating to operational conditions of network members;
a second data set identifying network members;
a third data set comprising optimizational information and parameters;
wherein the first data set, the second data set and the third data set are stored on a server connected to the network.
An embodiment of a method of use may perform the step of sensing and recording operational data from said engine to computer readable memory, wherein said operational data comprises engine speed, engine load, mass flow into said engine. The embodiment may further perform the step of processing with a first computer processor said operational data to create operational map tables for said engine and writing said operational map tables to computer readable memory. Additionally, an embodiment may perform the step of instructing a second computer processor that is in communication with said engine to retrieve from memory said operational map tables for controlling engine operation with the second computer processor based on values retrieved from said operational map tables during use. The embodiment may further include the steps of generating a first instruction from a first map table during a portion of use, and generating a second instruction from a second map table during a portion of use. The method may further include controlling a main fuel injector capable of directly injecting a second gaseous fuel into a combustion chamber and controlling a pilot fuel injector capable of injecting a pilot fuel into said combustion chamber, such that directing said natural gas fuel into said combustion chamber by controlling an array having a natural gas injector configured to inject natural gas in to said intake conduit, wherein the natural gas is introduced into said combustion chamber of said engine with a primary fuel and air.
In the foregoing Detailed Description, various features of the disclosure are grouped together in a single embodiment for the purpose of streamlining the disclosure. This method of disclosure is not to be interpreted as reflecting an intention that the claimed disclosure requires more features than are expressly recited in each claim. Rather, inventive aspects lie in less than all features of a single foregoing disclosed embodiment.
It is to be understood that the above-described arrangements are only illustrative of the application of the principles of the disclosure. Numerous modifications and alternative arrangements may be devised by those skilled in the art without departing from the spirit and scope of the disclosure and the appended claims are intended to cover such modifications and arrangements. Thus, while the disclosure has been shown in the drawings and described above with particularity and detail, it will be apparent to those of ordinary skill in the art that numerous modifications, including, but not limited to, variations in size, materials, shape, form, function and manner of operation, assembly and use may be made without departing from the principles and concepts set forth herein.
This application claims the benefit of U.S. Provisional Application No. 61/265,279, filed Nov. 30, 2009, which is hereby incorporated by reference herein in its entirety, including but not limited to those portions that specifically appear hereinafter, the incorporation by reference being made with the following exception: In the event that any portion of the above-referenced provisional application is inconsistent with this application, this application supercedes said above-referenced provisional application.
Number | Date | Country | |
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61265279 | Nov 2009 | US |