Patent Application
20190186350
This application is directed towards an externally powered turbocharging system for an internal combustion engine.
Air compressors such as superchargers or turbochargers can be used to increase the amount of air within the cylinders of an internal combustion engine. This increase in air allows a greater amount of fuel to be burned, increasing the power output of the engine. Turbochargers are powered by the exhaust gases of an engine and typically includes a turbine and a compressor, which can be coupled via a common shaft. The rotation of the turbine causes the compressor to rotate, which compresses air entering the internal combustion engine. Superchargers include a compressor which is gear driven or belt driven by the internal combustion engine. The compressor can then compress air entering the internal combustion engine.
While turbochargers and superchargers can each significantly increase the power output of an internal combustion engine, each device has inherent drawbacks. Turbochargers use exhaust pressure from the internal combustion engine to spin the turbine wheels. The physical characteristics of the turbine wheel and housing impact the responsiveness and maximum power output of the turbocharger system. Selecting physical characteristics of a turbocharger system generally determining tradeoffs between responsiveness and power output, with higher power turbocharging systems being less responsive. Supercharger systems, being belt or gear driven by the internal combustion engine, can have improved responsiveness relative to turbocharger systems, potentially with reduced maximum output due to parasitic loss on the engine introduced by supercharger drive system. Additionally, even turbocharger systems can cause some degree of initial power loss to an engine due to increased back pressure during the exhaust cycle of the engine.
Air compression systems that seek to avoid the drawbacks of superchargers and turbochargers are known in the art, with some systems attempting to provide a supercharging or turbocharging system that is powered independently of the primary internal combustion engine to which the air compression system is connected. Such independently powered compression systems have not found wide-spread utilization in the auto industry, as existing independent air compressor systems are too large and/or heavy to enable practical integration into existing internal combustion engine designs or may not provide a sufficient performance and/or efficient advantage to warrant the additional weight or cost of integration.
Described herein is an air compression system that can provide compressed air to an internal combustion engine while being powered separately from such engine. Rather than deriving power from the internal combustion engine, the system derives power from an external power source including but not limited to a gas turbine, gas generator, internal combustion engine, electric motor, compressed air motor, hydraulic motor, steam generator, etc. or any combination thereof. Additionally, the air compression system can be configured to both move and remove large volumes of a fluid from a specific, or multiple points within an attached internal combustion engine, improving engine efficiency by both pressurizing the intake tract and by assisting in the removal of exhaust gasses from the internal combustion engine. The system can be configured to apply a vacuum to the exhaust system of the internal combustion engine reducing or eliminating exhaust back pressure and preventing the buildup of exhaust manifold pressure. For example, diesel engines that are fitted with particulate filters and other emissions control components may experience reduced performance or efficiency due to the increased exhaust system backpressure caused by those systems. Such concerns may be overcome by the use of the exhaust vacuum system described herein. Additionally, the system designed herein may have particular applicability to high performance engine designers that wish to be able have a boost profile that is independent of the state of the internal combustion engine to which an associated turbocharger or supercharger is attached.
In one embodiment, the system includes a device having a compressor affixed to the intake tract of an internal combustion engine. The device can be configured to deliver a pre-determined quantity of air to the intake manifold of the internal combustion engine in order to increase the power output or efficiency of the internal combustion engine. Additionally, the device can have a secondary turbine that is configured as a vacuum compressor. The vacuum compressed can be affixed to the exhaust manifold of the engine and can create a vacuum to assist in the removal of any desired quantity of exhaust from the internal combustion engine. The exhaust vacuum can reduce exhaust back pressure on the engine, resulting in an increase in power output and/or efficiency of the internal combustion engine. The device may utilize any combination and any number of compressors and turbines of any design with either a fixed or variable geometry housing, adjustable nozzles to change or optimize flow characteristics, and or adjustable blade pitch in order to accomplish any task the device could be utilized. This device may be used in any application that requires both the delivery and removal of large quantities of a fluid to a specific point including but not limited to internal combustion engines of any design.
So that the manner which the above recited features of the present embodiments can be understood in detail, a more particular description of the embodiments, briefly summarized above, may be had by reference to embodiments, some of which are illustrated in the appended drawings. The appended drawings illustrate only typical embodiments, are not to be considered limiting as to all embodiments, and in which:
For the purposes of explanation, numerous specific details are set forth to provide a thorough understanding of the various embodiments described below. However, it will be apparent to a skilled practitioner in the art that the embodiments may be practiced without some of these specific details. In other instances, well-known structures and devices are shown in block diagram form to avoid obscuring the underlying principles, and to provide a more thorough understanding of embodiments. Although some of the following embodiments are described with reference to a graphics processor, the techniques and teachings described herein may be applied to various types of circuits or semiconductor devices, including general purpose processing devices or graphic processing devices. Reference herein to “one embodiment” or “an embodiment” indicate that a particular feature, structure, or characteristic described in connection or association with the embodiment can be included in at least one of such embodiments. However, the appearances of the phrase “in one embodiment” in various places in the specification do not necessarily all refer to the same embodiment.
In the following description and claims, the terms “coupled” and “connected,” along with their derivatives, may be used. It should be understood that these terms are not intended as synonyms for each other. “Coupled” is used to indicate that two or more elements, which may or may not be in direct physical or electrical contact with each other, co-operate or interact with each other. “Connected” is used to indicate the establishment of communication between two or more elements that are coupled with each other.
The turbocharger includes a turbine 106a that spins a shaft 120a connected to multiple compressors (compressor 101, compressor 102). Turbine 106a is spun by a pressurized fluid including a combusting fuel/air mixture 119 that is output from the combustor 103. A fuel supply 104a provides the combustor 103 with fuel. The fuel type may be the same or different as the fuel supply 104b used for the internal combustion engine 107. The supplied fuel can be any of a variety of fuels suitable for use within a gas turbine, including but not limited to Jet A, Jet A-1, Jet B, diesel, petrol, natural gas, kerosene, E85, biodiesel, biogas, or a mixture thereof.
The common shaft 120 is connected to multiple compressors (compressor 101, compressor 102, vacuum compressor 107) for creating boost pressure (e.g., turning ambient air 109a into compressed air 115) as well as scavenging exhaust gases from the exhaust of the internal combustion engine (exhaust vacuum 111). The turbocharger can utilize engine vacuum on a compressor section to start the combustion process in a combustor 103. For example, during startup, the compressor 101 can act as a turbine to spin shaft 120a, causing compressor 102 to compress ambient air 109b into compressed air 118, which flows into the combustor 103.
Once combustion has begun in the combustion chamber, gasses pass through turbine 106a, which can accelerate shaft 120a to which compressor 102 and compressor 101 are connected. Once accelerated, the compressor 101 supplies the intake manifold 116 with pressurized air. In one embodiment, combustor exhaust 121, having spun turbine 106a, can be routed to turbine 106b, which is connected to a vacuum compressor 107 via a second shaft 120b. Vacuum compressor 107 can actively scavenge exhaust from the exhaust manifold 112, reducing back pressure on the engine by creating an exhaust vacuum 111. The internal combustion engine exhaust air 110 can then be output via a conventional exhaust pipe channel.
In one embodiment, combustor exhaust 121 can be variably routed through turbine 106b or through a separate exhaust outlet. In one embodiment, instead of routing the combustor exhaust 121 through turbine 106b, turbine 106b can be excluded and shaft 120b can connect turbine 106a to vacuum compressor 107, such that a single common shaft 120 connects compressor 101, compressor 102, turbine 106a, and vacuum compressor 107. Combustor exhaust 121 can then be output via a separate exhaust path.
In one embodiment, compressed air output from compressor housing 201 can flow through an intercooler of heat exchanger 215 to reduce the temperature of the compressed air before the compressed air is supplied to the intake manifold 216 of the internal combustion engine 217. Exhaust gasses from the internal combustion engine 217 can flow into an exhaust manifold 212, which during operation is in a vacuum state due to operation of a vacuum compressor within housing 207. In one embodiment the internal combustion engine 217 provides an oil feed 214 and oil return 213 system by which engine oil of the internal combustion engine 217 is used to cool and lubricate the turbo system.
The illustrated configurations are representative of specific embodiments, and multiple configurations of turbines and compressors can be used.
As shown in
Pressure to control the pressure-controlled actuator can be provided via a feed line 432 that is tapped into the output section of the compressor housing 422. Output from turbine housing 426 can feed into a second turbine housing 427 to spin a second turbine, which is connected to a second compressor in a second compressor housing 421. The second compressor housing 421 can compress air that is drawn into an ambient air inlet 439a of the second compressor housing, which includes a compressor that provides compressed air via a compressed air outlet 441. The compressed air outlet 441 can connect to a heat exchanger or intercooler to cool the compressed air before the air is provided to an internal combustion engine Exhaust from the combustor can be output via a turbine exhaust outlet 440 that may be separate from the exhaust of an associated internal combustion engine. Exhaust scavenging can be enabled for the prototypical example via the addition of a vacuum compressor wheel to the shaft connecting the compressor impellers of the second turbine housing 427 and second compressor housing 421.
Those skilled in the art will appreciate from the foregoing description that the broad techniques of the embodiments can be implemented in a variety of forms. Various types of combustors can be utilized including can, annular and can annular combustors. The combustor may be positioned between the compressor and turbine or at a remote location. Additionally, the turbines and compressors described herein can axial flow, radial flow, centrifugal, or any combination thereof. In various embodiments, different types of fuels can be utilized including, but not limited to gasoline, propane, diesel oil, kerosene, hydrogen, Jet A, Jet A-1, Jet B, natural gas, E85, biodiesel, biogas, or a mixture thereof.
Described herein, in various embodiments, is a turbocharging system comprising a compressor having an air inlet and a compressed air outlet, the compressed air outlet to couple with the intake manifold of the internal combustion engine, a first turbine coupled to the compressor, the compressor driven without using power from the internal combustion engine; and a vacuum compressor coupled directly or indirectly to the first turbine. The first turbine can drive a common drive shaft that includes the compressor and the vacuum compressor or output of the first compressor can drive a second compressor that is coupled with the vacuum compressor. The vacuum compressor can be used to scavenge exhaust from the internal combustion engine.
Furthermore, the concepts described herein can be applied to various types of internal combustion engines, including those that can be used in automobiles, aircraft, boats, and other types of applications. Thus, in addition to the turbocharging system described herein, an engine apparatus is also provided, where the engine apparatus comprises an internal combustion engine having an intake manifold and an exhaust manifold, a compressor having an air inlet and a compressed air outlet, the compressed air outlet to couple with the intake manifold of the internal combustion engine, a first turbine coupled to the compressor, the compressor driven without using power from the internal combustion engine, and a vacuum compressor driven via the first turbine, the vacuum compressor to scavenge exhaust from the exhaust manifold of the internal combustion engine. Other details can be similar to the turbocharger system described herein.
The engine apparatus can be employed within vehicles of various types. One embodiment provides for a vehicle powered by an internal combustion engine having an intake manifold and an exhaust manifold, the vehicle comprising a compressor having an air inlet and a compressed air outlet, the compressed air outlet to couple with the intake manifold of the internal combustion engine, a first turbine coupled to the compressor, the compressor driven without using power from the internal combustion engine, and a vacuum compressor driven via the first turbine, the vacuum compressor to scavenge exhaust from the exhaust manifold of the internal combustion engine. The vacuum compressor can be directly or indirectly driven by the first turbine.
Therefore, while the embodiments have been described in connection with particular examples thereof, the true scope of the embodiments should not be so limited since other modifications will become apparent to the skilled practitioner upon a study of the drawings, specification, and following claims.
This application claims priority to U.S. Provisional Application No. 62/608,187 to John Manley McDonald, filed Dec. 20, 2017, which is hereby incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| 62608187 | Dec 2017 | US |
