The invention relates to an apparatus for supply of combustion air to a combustion engine via an exhaust inlet to a turbocharger.
In engines in which it is a condition that the turbocharger provides increased power at low rotational speeds, we use a turbocharger with a pressure limiting valve, also known as a “waste gate valve”. This turbocharger is larger than actually required for the motor. The turbocharger is dimensioned with an overcapacity and will reach the desired charge pressure already at low rotational speeds. When the engine reaches the upper rotational speeds, the turbocharger provides too much air, and the overpressure becomes too high. The waste gate valve has an air hose which runs from the inlet manifold down to a diaphragm actuator which acts on the valve. When the charge pressure exceeds a predefined value the pressure against the diaphragm becomes so high that it opens the waste gate valve via a bar. The exhaust gas is then led past the turbo charger and out to the exhaust system, thus the pressure increase ceases. As soon as the admission regulator is reduced, the amount of exhaust against the turbine wheel in the turbo charger is reduced, and the air pressure in the inlet manifold is reduced. The waste gate valve will shut, and all the exhaust gas will again pass through the turbo charger.
It is important for a motor with a turbocharger to have an unobstructed air supply and as few obstacles as possible in the exhaust system. The turbo charger decelerates the exhaust gases and works to some degree as a silencer. The turbo charger and its connections to the exhaust system and the air inlet requires particularly good maintenance and inspection. In addition to lubricating the bearings in the turbo charger the oil has an important role to cool the bearing housing. The heat from the turbine housing propagates into the bearings and the lubricating oil. The oil is so strongly heated when the engine runs at high load that all turbo charged engines must be provided with an oil radiator. The engine should moreover have a lubricating oil which is adapted to motors with turbo chargers.
A turbo charger increases the engine power in that more air is added to the combustion, so as for more fuel to be injected and combusted per work cycle. Suction engines without a turbo charger may use a high proportion up to 10% of their produced energy to suck in air. One of the problems for a diesel engine may be just to have a sufficiently high air supply in the upper rotational speed range. If, in addition, the engine condition is generally poor due to wear in the injection system and a considerable ignition delay, this will often incur sooting. Sooting may often be seen in conjunction with a too high fuel to air ration and exceeds the upper flash point limit for parts of the injected fuel mixture at so-called rich combustion, and one may have incomplete combustion of the fuel. Such an incomplete combustion may also incur an increased carbon monoxide content in the exhaust and is thus poisonous. The invention seeks amongst other things to reduce such sooting.
The turbo charger is driven by the exhaust gases which run out of the engine at high pressure and high temperature. It thus utilizes energy which would otherwise get lost. The turbine runs an air pump which blows air into the air inlet suction (actually air inlet blow) manifold. The capacity of an adapted turbo charger is slightly higher than what is actually required for obtaining a clean combustion with the same fuel injection capacity as a corresponding suction engine. In the upper rotation speed range when the exhaust gases gradually run the exhaust turbine around with great force and speed, more air is pumped into the motor than what it consumes. Sooting in the engine oil damages the oil, which further leads to increased wear and thus reduces the lifetime of the motor. The earlier onset of wear also reduces the engine power. Soot release to the outlet air is highly undesirable, particularly in places where diesel engines must run more or less continually, due to environmental considerations and health regulations, and require frequent cleaning. It is a problem on some petroleum platforms that diesel engines for electricity generators soot to a degree which incur a health problem to the crew. Presently, extensive cleaning of exhaust manifolds are required for keeping the level of sooting sufficiently low. This problem is more heavily expressed when the diesel engine become worn.
The turbo charger does not provide a benefit to all engines. The motor must work at a sufficiently high rotational speed in order to utilize the turbo charger. In excavators and other production machinery running at rather low working rpm, it is anyhow relevant to use magnets at the air inlet.
An actual diesel engine for running an electrical generator may have a 24 liter piston displacement or more and may benefit from using a turbo charger on the arched inlet channel according to the present invention. The actual turbo delivers a large amount of air, about 16 m3/minute at about 1200 rpm for the motor. The diesel motor runs generally an electrical generator which further runs hydraulic systems, thrusters and similarly power demanding equipment on a marine drilling platform, a petroleum production platform, an FPSO vessel, or a similar petroleum installation. The turbo charger according to the invention may also be used on land based plants.
The invention is a turbo charger (3) driven by exhaust gas from a combustion engine (1) via an exhaust inlet (35) to the turbo charger (3). The turbo charger (3) has an axial inlet (31) for combustion air generally at atmospheric pressure, from an outlet (34) at a bent pipe portion (37) with an inlet (36) from an inlet channel (4) from an air inlet (5). The inlet channel (4) has at least one arched wall (41) of non-magnetic material, with an inner surface (43) and an outer surface (45) relative to the inlet channel (4), wherein along the arched wall (41) is arranged a series of at least three magnets (6) having sequentially opposite magnetisation directions directed mainly orthogonal to said wall (41), and with a pole surface (61) of each magnet (6) generally in level with said wall (41), with a mutual separation between said magnets at least as long as a half of a first width of said inlet channel's cross-section.
An advantage of the invention is that the magnets are arranged along the radially inner part of the air flow in the inlet channel where it is expected that the air will pass with high speed and even air flow. It appears to the applicant that the motor's combustion properties are improved compared to when they are arranged along the opposite, outer wall of the air inlet channel. This allows reducing the rotation speed somewhat without losing power, or the fuel consumption is reduced, while sooting is reduced. The magnets are arranged along the outside surface of the wall of the channel so as for not to extend into the air flow which would reduce the area of the flow cross section. An additional advantage of the invention is that the magnets are arranged with a separation along the channel which allows the magnet's fields to extend into the channel cross section and not being “shorted” over to the adjacent neighbour magnet's oppositely directed magnetic field.
A turbo charger with magnets on an arched wall on the inlet channel to a large diesel engine may thus result in reduced sooting and thus provide reduced maintenance costs, improved health conditions, and slightly reduced noise level and/or improved engine power.
The invention is illustrated in the attached drawings, wherein
The invention described here is a turbo charger (3) driven by exhaust gas from a combustion engine (1) via an exhaust outlet (35) to the turbo charger (3). Such a turbo charger is illustrated in
The inlet channel's (4) cross-section may be round, weakly elliptic or rectangular, and is often rectangular for large motors, please see
Magnets along an arched surface in the air inlet to the turbo provides reduced sooting from the diesel engine. One possible explanation to the reduced sooting may be that the flow pattern of the inflowing air is slightly changed so as to achieve a slightly improved mixing of air and fuel, but this patent application does not seek any fluid mechanical explanation. The invention results in a small change in the effect curve of the engine, which may also provide a slightly modified way of running and a changed vibration pattern relative to the way it was before the magnets were mounted on the inlet channel. This leads to a slight allowable reduction in the motor's rotational speed while maintaining the torque, alternatively utilising the same rotational speed with a slightly increased power.
According to a preferred embodiment of the invention each magnet (6) is arranged on the wall's outer surface (45), and with a pole surface (61) of each magnet (6) generally being flush with the wall's (41) inward facing surface (43) without breaking through this. In this way the inward facing surface (43) may be kept slick and turbulence, which would otherwise have been formed, will be avoided, and the magnet's inward directed face will also not prevent the air flow. Each magnet (6) may be arranged in a capsule (62) arranged on the wall's (41) outward facing surface (45). In
The turbo charger (3) according to the invention is preferably arranged for inlet of mainly atmospheric combustion air. In this way possible waste of energy for membrane filtration or use of separately stored pressurised air.
According to a preferred embodiment of the invention the arched wall (41) constitutes the shorter, inner path of the inlet channel (4). This is illustrated in both
The arched wall (41) turns with an angle of between 20 degrees and 90 degrees. According to a preferred embodiment it does not turn as much as 90 degrees, but turns with an angle of between 26 degrees and 60 degrees.
There should be a certain separation between the magnets so as for them not to end up to close and thus to a partial degree mutually annul their effect. An internal separation between the magnets should at least be as wide as a half of a first width of the inlet channel as counted at right angles on the wall (41) such as shown in the cross-section in
Number | Date | Country | Kind |
---|---|---|---|
20091230 | Mar 2009 | NO | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/NO2010/000110 | 3/23/2010 | WO | 00 | 11/2/2011 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2010/110672 | 9/30/2010 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
5140816 | Scicluna | Aug 1992 | A |
5500121 | Thornton et al. | Mar 1996 | A |
6021764 | Koyama | Feb 2000 | A |
6178954 | Kim | Jan 2001 | B1 |
7028679 | Hillman et al. | Apr 2006 | B2 |
20070051347 | Thalberg | Mar 2007 | A1 |
20090007878 | Korenjak et al. | Jan 2009 | A1 |
Number | Date | Country |
---|---|---|
2281351 | Mar 1995 | GB |
1019920006633 | Apr 1992 | KR |
9923382 | May 1999 | WO |
2005026521 | Mar 2005 | WO |
Entry |
---|
International Search Report, dated Jun. 16, 2010, from corresponding PCT application. |
Chinese Search Report from corresponding CN application. |
Number | Date | Country | |
---|---|---|---|
20120039704 A1 | Feb 2012 | US |