1. Field of the Invention
The present disclosure relates to thermal management systems, and more particularly to heat switch radiators for variable heat rejection thermal management systems.
2. Description of Related Art
Space vehicles commonly employ thermal management systems to control the temperature of vehicle components, such as electronics. Such systems typically include heat sinks operative to reject heat to the external environment. The temperature of such heat sinks can change as the vehicle operating environment changes, such as when the vehicle passes into or out of direct sunlight. This can alter the heat transfer rate as such heat sinks can more readily reject heat when cold than when warm. Some space vehicle thermal management systems therefore include a supplemental heat rejection device, such as a sublimator, evaporator, variable conductance heat pipe, or pumped coolant loop with a regenerative heat exchanger for managing change in the vehicle operating environment.
Such conventional methods and systems have generally been considered satisfactory for their intended purposes. However, there is still a need in the art for thermal management systems that provide variable heat rejection rates for operation in both cold and warm environments. The present disclosure provides a solution for these needs.
A heat switch radiator includes a heat sink, a coolant tube, and an actuator. The coolant tube is movable with respect to the heat sink. The actuator couples the heat sink to the coolant tube for moving the coolant tube between first and second positions. Heat flow from the coolant tube to the heat sink is greater in the second position than the first position for enhanced heat transfer from the coolant tube in warm operating environments.
In certain embodiments, heat flow between the coolant tube and heat sink can be at an angle with respect to the direction of coolant tube movement. The angle can be orthogonal with respect to the direction of coolant tube movement. Heat flow from the coolant tube to the heat sink can be about twelve times greater when the coolant tube is in the second position than when the coolant tube is in the first position. The actuator can be a passive thermal actuator for changing the rate of heat transfer by moving the coolant tube from the first position to the second position. The rate of heat transfer can vary over a predetermined temperature range.
In accordance with certain embodiments, the heat sink can have laterally offset teeth that define a channel between the teeth. The coolant tube can have longitudinally spaced teeth disposed within the heat sink channel and facing the heat sink teeth. The coolant tube teeth can be adjacent to the heat sink teeth when the coolant tube is in the second position. Thermal gaskets can connect to the facing surfaces of the heat sink teeth for transferring heat from the coolant tube to the heat sink. A graphite velvet material flocked to the underlying tooth can form the thermal gaskets. The coolant tube teeth, thermal gaskets, and heat sink teeth can form a thermal circuit for transferring heat from the coolant tube to the heat sink in the second position.
It is contemplated that the coolant tube can have a guide support. An enclosure with an inner surface can enclose the coolant tube and heat sink. A tube guide can connect to an inner surface of the enclosure and be slidably received in the guide support for supporting the coolant tube. A material having low thermal conductivity can form the enclosure for providing a high resistance heat transfer path between the coolant tube and the heat sink. The actuator can couple between the enclosure and coolant tube for displacing the coolant tube along a movement axis between the first position and second position.
These and other features of the systems and methods of the subject disclosure will become more readily apparent to those skilled in the art from the following detailed description of the preferred embodiments taken in conjunction with the drawings.
So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, preferred embodiments thereof will be described in detail herein below with reference to certain figures, wherein:
Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of the heat switch radiator assembly in accordance with the disclosure is shown in
Heat switch radiator 100 includes a heat switch 120 and a radiator 110. Heat switch 120 includes a coolant tube 130 with a plurality of coolant tube teeth 130A and 130B configured for transferring heat from coolant traversing coolant tube 130 to radiator 110. Radiator 110 includes a plurality of corresponding radiator teeth 110A and 110B configured for receiving heat from coolant tube teeth 130A and 130B and rejecting the heat to the external environment.
Heat switch radiator 100 also includes an enclosure 150 and a tube guide 140. Enclosure 150 connects to radiator 110 and houses a portion of coolant tube 130, coolant tube teeth 130A and 130B, and radiator teeth 110A and 110B. Tube guide 140 connects to an inner surface 152 of enclosure 150 and defines a guide portion 142 extending along its longitudinal length. Coolant tube 130 defines a slotted portion 136 corresponding to guide portion 142 for slidably seating guide portion 142. Slidably seating guide portion 142 in slotted portion 136 allows for movement of coolant tube 130 along a movement axis M that is parallel with guide portion 142 for displacement of coolant tube 130 between a first position, e.g. the ‘off position’, (shown in
In order to facilitate smooth movement (e.g. without binding coolant tube 130), it is contemplated that tube guide 140 be constructed from a material that does not bind with the material from which coolant tube 130 is constructed. This will allow smooth movement of coolant tube 130 in relation to tube guide 140. Tube guide 140 may be constructed from a low friction plastic material, or a graphite-loaded or self-lubricating plastic having similar advantages. Those skilled in the art will know other suitable materials.
Heat switch 120 additionally includes an actuator 160 operatively associated with coolant tube 130 for moving coolant tube 130 between the first and second positions. Actuator 160 includes a fixed portion 162 and a movable portion 164. Fixed portion 162 abuts a stop 154 formed on an outer surface 155 of enclosure 150. Movable portion 164 extends through guides 156 formed on outer surface 155 of enclosure 150 and abuts an elbow 134 defined by coolant tube 130. Actuator 160 is configured to change in length in response to temperature through operation of a thermally expandable body 166 (shown in
When at or below the first predetermined temperature, actuator 160 assumes its first length. When exposed to temperatures above the first predetermined temperature, actuator 160 lengthens by displacing movable portion 164 in the aft direction relative to fixed portion 162, assuming its second length. Assuming its second length applies an aft-directed force on elbow 134 that drives coolant tube 130 in the aft direction along movement axis M as oriented in
A resilient member 170 extends between elbow 134 and a bracket 180. Bracket 180 is fixed with respect to fixed portion 162 of actuator 160. As actuator 160 drives coolant tube 130 in the aft direction, elbow 134 compresses resilient member 170. This causes resilient member 170 to apply an opposite, forward directed force on elbow 134 that is a function of the compression experienced by resilient member 170. Movement of coolant tube 130 ceases once the forward-directed force resulting from compression of resilient member 170 reaches the same magnitude as the aft-directed force imposed by actuator 160 on elbow 134 or when actuator 160 reaches its second predetermined temperature (and second length).
From its second length, upon exposure to temperature below the second predetermined temperature, actuator 160 reduces the aft-directed force applied to elbow 134. As aft-directed force applied by actuator 160 on elbow 134 drops, the forward-directed force applied by resilient member 170 drives coolant tube 130 forward along movement axis M, thereby displacing movable portion 164 toward fixed portion 162 of actuator 160 and reducing the length of actuator 160. Forward-directed movement of coolant tube 130 ceases once the forward-directed force reaches the same magnitude as the aft force imposed by actuator 160 on elbow 134 or when actuator 160 reaches its first predetermined temperature (and first length).
With reference to
Radiator body 112 is fabricated from a material having suitable heat transfer for an intended application, such as aluminum, and can be fabricated via an extrusion process or any other suitable process. First comb 114 and second comb 118 can be formed from an extrusion by milling gaps to form longitudinally adjacent teeth. Those skilled in the art will readily appreciate that any other suitable techniques can be used for fabricating body 112, first comb 114, rail 116, and second comb 118.
With reference to
With reference to
On its upper portion and aft end, coolant tube body 132 defines elbow 134. On its lower portion, coolant tube body 132 defines a first longitudinally extending comb 131 and a second longitudinally extending comb 133. First comb 131 includes a longitudinally extending row of teeth 130A, only a single tooth 130A identified in
Elbow 134 has a first engagement surface 137 on its aft face and a second engagement surface 135 on its forward face. First engagement surface 137 is configured for seating a first end 174 of resilient member 170 (shown in
With reference to
Enclosure 150 defines a forward aperture 158, an aft aperture 151, and longitudinally extending chamber 153. Forward aperture 158 and aft aperture 151 are configured to slidably receive forward and aft end portions of coolant tube 130. It is contemplated that forward and aft bellows structures (omitted for clarity purposes) seat between enclosure 150 and opposite respective ends of coolant tube 130 for allowing coolant tube 130 to sealably move within chamber 153 along movement axis M with respect to enclosure 150. In certain embodiments, enclosure 150 enables maintenance of a sealed environment for impounding particulate within chamber 153 that may shed from thermal gaskets 190 within enclosure 150.
On its aft end enclosure body 152 defines stop 154 and guides 156. Stop 154 extends orthogonally with respect to movement axis M and provides a surface configured to seat fixed portion 162 of actuator 160 (shown in
With reference to
In embodiments, heat switch radiators described herein have thermal conductances that are about eight to fifteen times higher when coolant tube 130 is in the second position than when coolant tube 130 is in the first position. It is further contemplated that embodiments of heat switch radiator 100 can exhibit its full range of throw over a temperature change of 5 to 20 degrees Fahrenheit (3 to 11 degrees Celsius). In certain embodiments, two or more actuators 160 couple to coolant tube 130 for moving coolant tube 130 from the first position to the second position.
With reference to
With reference to
With reference to
With reference to
The methods and systems of the present disclosure, as described above and shown in the drawings, provide for thermal management systems with superior properties including high turn-down ratio heat transfer for operation in both cold and warm environments. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the spirit and scope of the subject disclosure.
This invention was made with government support under Contract No. NNL13AB40P-CLIN001 awarded by the National Aeronautics and Space Administration. The government has certain rights in the invention.
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