Satellite transmitter system
A satellite transmitter module for accepting input signals and emitting output signals for uplink transmission. The module includes a transmitter unit that includes i) transmitter circuitry, ii) at least one input port, iii) and at least one output port. At least one heat sink coupled to the transmitter unit includes a plurality of heat sink fins, wherein at least two of the plurality of heat sink fins are of different heights. A fan is capable of generating air flow parallel with the plurality of heat sink fins. The module further includes an outer enclosure that i) encloses the transmitter unit and the plurality of heat sink fins and ii) is impermeable to the air flow generated by the fan. The outer enclosure includes an enclosure cross section shape that is substantially similar to the at least one heat sink cross section shape defined by the height of each of the plurality of the heat sink fins.
1. An apparatus comprising:
a transmitter unit comprising a transmitter circuitry;
at least one heat sink coupled to the transmitter unit, the heat sink including a plurality of heat sink fins, wherein (i) at least two of the heat sink fins are of different fin heights, (ii) the heat sink is positioned in a close proximity to the transmitter circuitry and (iii) the fin heights of the heat sink fins are a function of the close proximity to the transmitter circuitry and amounts of heat from the transmitter circuitry;
a fan configured to generate an air flow substantially parallel with spaces between the heat sink fins; and
an outer enclosure (i) enclosing the transmitter unit and the heat sink fins therein, (ii) being impermeable to the air flow generated by the fan, and (iii) including a cross section shape substantially similar to a contour of the heat sink fins.
2. The apparatus of claim 1 , wherein the cross section shape of the outer enclosure is substantially similar to a fan cross section shape defined by rotating blades of the fan.
3. The apparatus of claim 1 , wherein the transmitter circuitry is situated along a central axis of the transmitter unit and in substantially a same direction as the air flow from the fan.
4. The apparatus of claim 3 , wherein the height of one of the heat sink fins situated on the central axis of the transmitter unit is higher than the height of others of the heat sink fins when a number of the heat sink fins is odd.
5. The apparatus claim 3 , wherein the heights of two of the heat sink fins situated closest to the central axis of the transmitter unit are higher than the heights of others of the heat sink fins when a number of the heat sink fins is even.
6. The apparatus of claim 1 , wherein (i) the transmitter unit is coupled to another heat sink, and (ii) the another heat sink including another plurality of heat sink fins.
7. The apparatus of claim 1 , wherein the heat sink fins are parallel to every other of the heat sink fins.
8. The apparatus of claim 1 , wherein the cross section shape of the outer enclosure is a rounded shape.
9. The apparatus of claim 1 , wherein the cross section shape of the enclosure is a polygonal shape.
10. The apparatus of claim 1 , wherein the cross section shape of the outer enclosure is a circular shape or an elliptical shape.
11. The apparatus of claim 1 , wherein the heat sink fins includes pin fins.
12. The apparatus of claim 1 , wherein the transmitter circuitry includes a frequency converter unit configured to modify an input frequency of an input signal to an output frequency suitable to use in satellite communication.
13. The apparatus of claim 1 , wherein the transmitter circuitry includes an amplifier unit configured to amplify an input power level of an input signal to an output power level suitable to use in satellite communication.
14. The apparatus of claim 1 , wherein the transmitter circuitry further includes a receiver unit configured to convert an input satellite signal into an output data signal to be demodulated.
15. An apparatus comprising:
a transmitter comprising a transmitter circuitry configured to transmit a satellite communications signal;
at least one heat sink thermally coupled to the transmitter, the heat sink including a plurality of heat sink fins, wherein (i) at least two of the heat sink fins comprise heights as a function of a distance between the heat sink fins and the transmitter, and (ii) the heat sink is positioned in a close proximity to the transmitter;
a fan, disposed at a distal end of the transmitter, and configured to generate an air flow substantially parallel with spaces between the heat sink fins; and
an outer enclosure enclosing the transmitter and the heat sink fins therein.
16. The apparatus of claim 15 , wherein a cross section shape of the outer enclosure is substantially similar to a contour of the heat sink fins.
17. The apparatus of claim 16 , wherein the cross section shape of the outer enclosure is substantially similar to a fan cross section shape defined by rotating blades of the fan.
18. A method for reducing thermal energy in a transmitter comprising the steps of:
connecting two sets of a plurality of heat sink fins to the transmitter, wherein (i) each of the heat sink fins includes a corresponding height, (ii) the heights of a first set of the heat sink fins are determined as a function of distance between the heat sink fins and the transmitter and (iii) the heights of a second set of heat sink fins are not determined as a function of distance between the heat sink fins and the transmitter;
generating an air flow substantially parallel with spaces between the heat sink fins via a fan; and
enclosing the heat sink fins and the transmitter in a housing.
19. The method of claim 18 , wherein (i) a first set of the heat sink fins have heights that are determined as a function of distance between the each of the heat sink fins and the transmitter and (ii) a second set of the heat sink fins have heights that are not determined as a function of distance between the each of the heat sink fins and the transmitter.
20. The method of claim 18 , wherein the housing comprises at least one cross section shape among (i) circular, (ii) elliptical, (iii) rounded-corner, and (iv) polygonal.