The present invention relates to the art of heat transfer; more particularly, to air-cooled charge air coolers; and most particularly to air-cooled charge air coolers for cooling air from a turbocharger before it enters an engine.
In order to maximize performance, diesel engines use turbochargers to compress the combustion air, thus increasing its density, and increasing the amount of oxygen available for combustion in the engine. During the course of compression, the temperature of the charge air is increased. Charge air coolers cool the charge air to further increase its density before the charge air enters the engine.
As environmental concerns have emerged, governments have placed limits on emissions from diesel engines. These limits have become more and more restrictive. In order to meet these emissions regulations, diesel engine designers have increased charge air pressures and temperatures.
A common air-cooled charge air cooler is made from aluminum, either tube and header designs or bar and plate designs. These heat exchangers have maximum temperature and pressure limits resulting from design considerations including the maximum allowable stress of aluminum at operating temperatures. The tensile strength of aluminum begins to decrease considerably above about 300° F. This means that the product must use heavier parts in order to contain the charge air pressure without failure.
Bar and plate designs tend to be more robust than tube and header designs. Even so, the inlet manifold and the inlet ends of the charge air passages are subject to the maximum charge air temperature. Some engine designs result in specifications of charge air temperatures of 500° F. or higher with operating pressures of 50 psig or higher. However, it is true that the metal temperature will be somewhat lower than the charge air inlet temperature due to heat transfer between the manifold and the ambient surrounding the charge air cooler. This temperature, which may be 50 to 75° F. lower than the inlet temperature, is still high enough to require the use of low allowable stresses for design of the charge air cooler.
What is needed is a means of lowering the charge air cooler metal temperature significantly more than 50 to 75° F. so that much higher stresses can be used for design purposes.
It is a primary object of the invention to lower the charge air cooler metal temperature significantly more than 50 to 75° F. so that much higher stresses can be used for design purposes.
Briefly described, a heat insulator for an intake manifold of an air-cooled charge air cooler has an enclosure of a material that is able to retain its essential mechanical characteristics in an elevated temperature equal to the temperature of input air to the air-cooled charge air cooler, the enclosure being contained within a housing and having a contact area with said housing that is small in relation to the outside area of the enclosure. The enclosure has an opening for admitting the input air and an interface plate of the same material positioned to pass air through the open end of the enclosure directly to a plurality of hollow air passages in a heat exchanger. The enclosure is not sealed such that there is essentially no pressure differential between the outside and inside of the enclosure.
The present invention will now be described, by way of example, with reference to the accompanying drawings, in which:
Referring to
In operation the high temperature, high pressure charge air enters the intake hose connector 18, distributed to the heat exchanger tubes 28 in the intake manifold 12, cooled in the heat exchanger 14, collected in the outlet manifold 16 and exits the air cooled charge-air cooler 10 through the hose connector 20.
With the present invention the hose connector 18, and the housing 42 are kept at least 250 to 350° F. below the approximately 500° F. inlet charge air, well within the normal design range for aluminum bar and plate heat exchangers.
With reference now to
The housing insert 44 is not air tight, but inhibits the flow of air from inside the housing insert 44 to the cooler aluminum walls of the housing 42 on the intake manifold 12 so that heat from air touching the inside of the housing 42 is passed through the wall of the housing 42 to the outside ambient air. The hot air which transfers from the housing insert 44 to the aluminum housing 42 is cooled by the walls of the housing 42, and the volume of air passing across the inside walls of the aluminum housing 42 does not produce enough heat mass that can't be sufficiently cooled by the heat conduction through the walls of the housing 42, and thus the temperature of the housing 42 is kept significantly less than the charge air temperature entering the hose connector 18.
Also, the housing insert 44, though subject to direct contact with the incoming charge air, is submerged within the high-pressure charge air, so there is no pressure containment required of the housing insert 44 and consequently the tension characteristics that are required of the housing 42 and the hose connector 18 due to the high pressure inlet charge air are not required of the housing insert 44 and the liner 46. As a consequence, the housing insert 44 and liner 46 can be significantly thinner than the housing 42 and the hose connector 18.
Another concern obviated by the present invention is the joint between the internal passages of the intake manifold and the sheets between the header bars and face bars. First, the housing insert 44 shields the plane of the header bars from the incoming high temperature charge air. Second, the housing insert 44 uses the slots 64 to propel the charge air past this plane into the interior of the internal passages. This reduces the abrupt temperature change at this location due to the high temperature charge air in the internal passages of the intake manifold 12 and the relatively cold cooling air temperature on the outside of the charge air cooler 10.
While the invention has been described by reference to various specific embodiments, it should be understood that numerous changes may be made within the spirit and scope of the inventive concepts described. Accordingly, it is intended that the invention not be limited to the described embodiments, but will have full scope defined by the language of the following claims.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/US06/08842 | 3/13/2006 | WO | 00 | 10/27/2009 |
Number | Date | Country | |
---|---|---|---|
60661641 | Mar 2005 | US |