The present embodiments relate to apparatus that can adjust a heat transfer surface area during chilling or freezing processes.
Known freezing systems that are used in, for example, in transit refrigeration (ITR) include mechanical compression refrigeration driven by diesel fuel motors, bunkers filled with CO2 dry ice, or CO2 liquid that is vaporized through heat exchangers mounted inside a refrigerated space and then discharged to an exterior of the space. The air inside the refrigerated space is cooled by forced or natural convection over the surface of the heat exchanger for the mechanical compression refrigeration system, the dry ice bunker or the liquid CO2 heat exchanger. The air temperature inside the refrigerated space will usually be either 0° F. (−18° C.) for a frozen food product, or 34° F. (1° C.) for a chilled product.
Precise temperature control of the air in the space using a mechanical compression refrigeration system is difficult, due to a low temperature difference between the refrigerant temperature and the desired air temperature and thus, a limited heat transfer rate. In addition, for refrigeration systems installed in trailers, the trailer doors are frequently opened for deliveries providing frequent rapid increases in trailer heat load. Precise temperature control of the air in the space is difficult for dry ice bunker systems because the heat exchanger surface always remains at minus 109° F. (−78° C.), and once that temperature is reached the heat transfer cannot be reduced. Therefore, air temperature will drop below the desired set point. Failure to maintain proper temperature control in the space may cause the temperature to be reduced to a rate below that which is acceptable for the product to be transported, and thereby damage the product.
In order to compensate for the anticipated increase in heat load, air temperature within the space will frequently be reduced to a temperature that is lower than desirable for the product being transported. This makes food products especially susceptible to damage, and will therefore likely result in the system efficiency being lowered in order to obtain the proper temperature control for the space.
Known systems also have a cold surface at the heat exchanger which tends to become covered in frost that has been condensed from air external to the refrigerated space being permitted to come into the space (such as when trailer doors are opened to access the product), thereby causing variation in heat transfer rate and potential loss of temperature control for the space. It is desirable to eliminate the frost build up on the heat exchanger surface and provide for a more uniform and consistent temperature of the product and the refrigeration space.
For a more complete understanding of the present inventive embodiment disclosures, reference may be had to the following drawing figures taken in conjunction with the description of the embodiments, of which:
Referring to
The heat exchanger 10 has a portion thereof insulated to prevent heat transfer to the air flow 26 being directed to the heat exchanger. An insulation layer 28 or member is mounted to the interior surface 18 of the sidewall 12 and covers a select portion of said interior surface. The insulation layer 28 may be constructed of high density foam or polystyrene, or be vacuum insulated. The insulation layer 28 is fixed to the interior surface 18 of the sidewall 12 or may be formed integral therewith.
As shown by way of example only with respect to
A moveable insulated shield 30 or member is disposed for rotational movement along the exterior surface 16 of the sidewall 12. The shield 30 has an arcuate shape in order to operate as described below. Referring also to
As shown in
The degree of cooling in the container 22 by the heat exchanger 10 can be controlled by rotation of the shield 30 along the exterior surface 16 of the sidewall 12 to thereby vary the exposed exterior surface area. The shield 30 is mounted to the sidewall 12 so that when the shield is moved or rotated it hugs or glides along the exterior surface 16 of the sidewall. The shield 30 can be manufactured from a material similar to that which is used to manufacture the insulation layer 28. If the shield 30 is manufactured from stainless steel or aluminum, such could have a core of high density foam or polystyrene; or even a vacuum insulated core.
The shield 30 is also provided with at least one knife edge 32. When the shield 30 is moved in, for example, the counter-clockwise direction as shown in
As shown in
Referring still to
Referring to
The moveable shield 30 is provided at an end thereof with a gear flange 54 or collar having at least a portion thereof provided with a plurality of teeth 56. The teeth 56 extend substantially along an edge of the gear flange 54, and certainly at least to an extent necessary to move the shield 30 into the necessary position with respect to the insulation layer 28 in order to provide the desired amount of heat transfer. The servo motor 48 has a shaft 58 extending therefrom which has at an end thereof a gear 60 with a plurality of teeth 62 sized and shaped for being in registration and coacting with teeth 56 of the gear flange 54. With this construction, the servo motor 48 drives the shaft 58 and in turn the gear 60; the teeth 62 coacting with the teeth 56 of the gear flange 54 to rotate the moveable shield 30 into the necessary position with respect to the sidewall 12. The coaction of the insulation layer 28 and the shield 30 adjusts the heat transfer effect that can be provided at the sidewall 12.
The apparatus 10 can be filled or charged with cryogen in different phases. An end portion 51 of the sidewall 12 can be provided with a door 50 or flap through which the dry ice 20 can be introduced into the space 14. A chute 52, charging funnel or hopper is mount to the end portion 51 in registration with the door 50 so that the dry ice 20 in the form of pellets can be introduced into the space 14 for providing the heat transfer effect.
Alternatively, the cryogen introduced into the apparatus 10 can be provided as liquid cryogen introduced through an inlet pipe 40 or fill pipe which may extend substantially across the space 14 as shown in
As shown in
It will be understood that the embodiments described herein are merely exemplary, and that one skilled in the art may make variations and modifications without departing from the spirit and scope of the invention. All such variations and modifications are intended to be included within the scope of the invention as described and claimed herein. Further, all embodiments disclosed are not necessarily in the alternative, as various embodiments of the invention may be combined to provide the desired result.
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| Number | Date | Country | |
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| 20130152618 A1 | Jun 2013 | US |