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[0001] The present invention relates to a heat control device and more particularly to a heat control device feasible for, e.g., an artificial satellite or a spacecraft.
[0002] As for a spacecraft expected to navigate a vacuum environment, heat radiation from outside surfaces is the only heat radiating means available. The amount of heat radiation dictates the temperature inside the spacecraft. A thermal louver has customarily been used for maintaining temperature inside the spacecraft adequate. The thermal louver adjusts the amount of heat radiation to the outside in accordance with temperature. Specifically, the louver includes a bimetal or similar actuator for driving blades. The blades are movable to increase or decrease the effective area and therefore the temperature of heat radiation surfaces, i.e., increase the amount of heat radiation at a high temperature or reduces it at a low temperature.
[0003] However, the above thermal louver is a mechanical device including movable portions and therefore bulky and heavy. Moreover, the louver lacks in reliability due to the movable portions. In addition, the blades cannot be opened and closed more than a preselected number of times due to their limited life.
[0004] Technologies relating to the present invention are also disclosed in, e.g., Japanese Patent Laid-Open Publication Nos, 63-207799, 1-212699 and
[0005] It is therefore an object of the present invention to provide a reliable heat control device operable over a long period of time even in a severe environment and easy to produce.
[0006] It is another object of the present invention to provide a reliable, small size and light weight heat control device including no movable portions.
[0007] In a heat control device of the present invention, a variable-phase substance exhibiting a property of an insulator or a property of metal in a high temperature phase or a low temperature phase, respectively, and radiating a great amount of heat or a small amount of heat in the low temperature phase or the high temperature phase, respectively, controls the temperature of a desired object.
[0008] The above and other objects, features and advantages of the present invention will become more apparent from the following detailed description taken with the accompanying drawings in which:
[0009]
[0010]
[0011]
[0012]
[0013]
[0014] To better understand the present invention, brief reference will be made to a conventional thermal louver, shown in
[0015] A heat control device in accordance with the present invention is characterized in that it uses a heat radiation characteristic particular to a substance itself in place of a mechanical principle. As for a spacecraft expected to navigate a vacuum environment, heat radiation from outside surfaces is the only heat radiating means available. The amount of heat radiation dictates the temperature inside the spacecraft.
[0016] The heat control device of the present invention is implemented by a variable-phase substance (La
[0017]
[0018]
[0019] In the heat control device of the present invention, the variable-phase substance should only be arranged on heat radiation surfaces in the farm of a film and is therefore space-saving and light weight. Moreover, the device is highly reliable because it needs no movable portions. When the device is mounted in a position getting the sunlight, a silicon plate transparent for thermal infrared rays, but opaque for the sunlight, may be positioned in front of the variable-phase substance in order to minimize the sunlight absorption of the device.
[0020] For the variable-phase substance, use may be made of an oxide of Mn-containing perovskite represented by A
[0021] Referring to
[0022] Specifically, the object
[0023] In operation, when the temperature of the surface
[0024] The substance
[0025] The illustrative embodiment is practicable only if the variable-phase substance is implemented by, e.g., an oxide of Mn-containing perovskite represented by A
[0026] A second embodiment of the heat control device in accordance with the present invention will be described with reference to
[0027] As shown in
[0028] If desired, the silicon plate
[0029] In summary, it will be seen that the present invention provides a small size, light weight heat control device using an optical property particular to a substance itself in place of a mechanical principle applied to a conventional thermal louver. In addition, the device of the present invention is highly reliable and long life because it needs no movable portions which would bring about wear, fatigue and other problems.
[0030] Various modifications will become possible for those skilled in the art after receiving the teachings of the present disclosure without departing from the scope thereof.