Power routing module with switching matrix for solar cell arrays - Patent Application 20070122997

Abstract

What is needed is a means to increase automation in the manufacturing of solar cell arrays while preserving the ability to customize the solar cell arrays. A power routing module having a switching matrix for electrically interconnecting a plurality of solar cells in an array, the switching matrix configured to dynamically route power among a plurality of current paths connected between the power routing module and the plurality of solar cells, at least one of the solar cells having at least one trimmed corner forming a corner region, an area of ​​the substrate within the corner region remaining exposed when the solar cell is attached to the substrate, and a power routing module having a switching matrix attached to the substrate in the area of ​​the substrate within the corner region remaining exposed.

Description

[Technical Field]

[0001] FIELD OF THE DISCLOSURE The present disclosure relates generally to solar cell panels, and more particularly to a power routing module having a switching matrix for a solar cell array. [Background technology]

[0002] The assembly of a typical spaceflight solar cell panel involves the construction of long strings of solar cells. These strings are variable in length and can be very long, for example, up to 20 cells or more. Assembling such long, variable, and fragile components is difficult, which has hindered automation of assembly.

[0003] Existing solutions use solar cells assembled into CIC (cell, interconnect, and cover glass) units. The CIC has metal foil interconnects connected to the front of the cells that extend parallel from one side of the CIC. The CICs are placed close to each other and connected to the bottom of adjacent cells by interconnects. Using these interconnects, the CICs are assembled into linear strings. These linear strings are constructed by hand and laid out to form large solar cell arrays consisting of many strings of variable length.

[0004] Additionally, to protect cells from reverse bias when they are partially shaded, bypass diodes are used, typically connecting between the back contacts of two adjacent cells in a solar cell array.

[0005] When used within a satellite, solar cell arrays are typically packaged as panels. The dimensions of the panels are determined by the needs of the satellite, including the power required and the size and shape constraints required for loading and storing the satellite within the launch vehicle. Furthermore, when the panels are deployed, portions of the panels often need to be used for mechanical equipment, and the solar cell array must avoid these areas. In practice, panels are generally rectangular, but their dimensions and aspect ratios vary widely. The layout of the CICs and strings that fill this space must be highly customized to maximize power generation, resulting in a highly manual manufacturing process.

[0006] Therefore, what is needed is a means to increase automation in the manufacturing of solar cell arrays while preserving the ability to customize the solar cell arrays. Summary of the Invention

[0007] The apparatus and methods of the present disclosure may be implemented in a variety of ways, including but not limited to the examples listed below. 1. A power routing module having a switching matrix for electrically interconnecting a plurality of solar cells in an array, the switching matrix configured to dynamically route power among a plurality of current paths connected between the power routing module and the plurality of solar cells, at least one of the solar cells having at least one trimmed corner forming a corner region, an area of ​​the substrate within the corner region remaining exposed when the solar cell is attached to the substrate, and the power routing module having the switching matrix attached to the substrate in the area of ​​the substrate within the corner region remaining exposed. 2. The switching matrix is ​​configured to dynamically route power among a plurality of current paths connected between the power routing module and one or more bypass diodes. 3. The switching matrix is ​​configured to dynamically route power among multiple current paths connected between the power routing module and one or more power or embedded lines. 4. The switching matrix is ​​configured to dynamically route power in response to control signals. 5. The control signal is a wireless control signal from a remote source. 6. A switching matrix is ​​a space division circuit switch in which power in selected input paths is connected to selected output paths. 7. A switching matrix consists of one or more connection blocks, each of which connects a selected input path to a selected output path according to a control signal. 8. Switching matrices may be addressed individually or in groups. 9. Each connection block in the switching matrix is ​​uniquely addressed. 10. Selected input and output paths within each connection block are uniquely addressed.

[0008] Reference is now made to the drawings, wherein like reference numerals represent corresponding parts throughout the various views. [Brief explanation of the drawings]

[0009] [Figure 1] 1 shows a conventional structure of a solar cell panel. [Figure 2] 1 shows a conventional structure of a solar cell panel. [Figure 3] 1A and 1B show an improved structure of a solar cell panel according to one embodiment. [Figure 4] 1A and 1B show alternative structures of a solar cell panel according to one embodiment. [Figure 5] 4A and 4B show the front surface of an exemplary solar cell that may be used in the improved solar cell panels of FIGS. 3A and 3B and 4A and 4B. [Figure 6] 6 illustrates the backside of the exemplary solar cell of FIG. 5. [Figure 7] 1 illustrates cells arranged in a two-dimensional (2D) grid-like array, according to one embodiment. [Figure 8] 10 shows an embodiment of an array in which one or more bypass diodes are added to the exposed areas of the substrate in the corner regions. [Figure 9] 1 shows an embodiment in which the bypass diode is applied to the backside of the cell, with the interconnect or contact for the bypass diode extending into the corner region between the front and back contacts. [Figure 10] 10 shows a front view of the embodiment of FIG. 9, in which the interconnects or contacts for the bypass diodes extend into the corner regions between the front and back contacts. [Figure 11] FIG. 11 shows the cells of FIGS. 9 and 10 arranged in a 2D grid array and applied to a substrate, with bypass diodes applied to the backside of the cells and contacts for the bypass diodes extending into the corner regions of the cells. [Figure 12] 1 illustrates vertical series connections between cells of an array according to one embodiment. [Figure 13] 1 illustrates horizontal series connections between cells of an array according to one embodiment. [Figure 14] 1 is a schematic side view of one embodiment in which a substrate is underneath and a power routing module is on top, the substrate being an assembly of flexible sheets. [Figure 15] 1 is a schematic side view of one embodiment with a substrate underneath and a power routing module on top, the power routing module attached to a flexible sheet with adhesive. FIG. [Figure 16] FIG. 2 is a top view of a corner region of a solar cell in an array. [Figure 17] 1 shows the structure of a power routing module for series connection of solar cells. [Figure 18] 10 shows a variation of a power routing module attached to solar cells in an array. [Figure 19]1 shows an array of cells laid out corresponding to the direction of current flow determined by a power routing module. [Figure 20] 1 illustrates one embodiment of a power routing module that is fabricated to include a switching matrix. [Figure 21] 1 is a schematic side view of one embodiment with a substrate underneath and a power routing module with a switching matrix on top, the power routing module attached to a flexible sheet with adhesive. FIG. [Figure 22] 10 shows modifications made to the conductors in the corner regions to manipulate the switching matrix. [Figure 23] 1 illustrates one embodiment of a switching matrix for use with a power routing module. [Figure 24] 1 illustrates a method for manufacturing a solar cell, a solar cell panel, and / or a satellite, according to one embodiment. [Figure 25] 1 illustrates the resulting satellite having solar cell panels made of solar cells, according to one embodiment. [Figure 26] 1 illustrates a solar cell panel in functional block diagram form, according to one embodiment. DETAILED DESCRIPTION OF THE INVENTION

[0010] In the following description, reference is made to the accompanying drawings that form a part hereof. These drawings are shown for the purpose of illustrating specific embodiments in which the present disclosure may be practiced. It is to be understood that other embodiments may be utilized and structural changes may be made without departing from the scope of the present disclosure.

[0011] overview An emerging approach to the design of solar cell arrays, for example for spaceflight power applications, is based on electrical connections between the solar cells in the array.

[0012] These new approaches rearrange the components of a solar cell and the arrangement of solar cells within an array. Instead of connecting solar cells into long linear strings and then assembling them on a substrate, solar cells are individually attached to the substrate so that the corner regions of adjacent cells are aligned on the substrate, thereby exposing an area of ​​the substrate. Electrical connections between cells are made by corner conductors formed on or within the substrate in these corner regions. As a result, this approach presents a solar cell array design based on individual cells.

[0013] Thus, a single laydown process and layout can be used to manufacture the solar cell array. Current flow between the solar cells is supported by conductors embedded within the substrate. These electrical connections define the specific characteristics of the solar cell array, such as its dimensions, stayout areas, and circuit terminations. This approach simplifies manufacturing, enables automation, and reduces cost and delivery time.

[0014] 1 and 2 show a conventional structure of a solar cell panel 10, including a substrate 12, a plurality of solar cells 14 arranged in an array, and electrical connectors 16 between the solar cells 14. A half-sized solar cell 14 is shown in FIG. 1, and a full-sized solar cell 14 is shown in FIG. 2. Space solar cells 14 are fabricated from a circular germanium (Ge) substrate starting material. These are later processed into a quasi-rectangular shape for more dense integration into the solar cell panel 10. This wafer is often diced into one or two solar cells 14, which are referred to herein as half-sized or full-sized solar cells 14. Electrical connectors 16, which electrically connect the solar cells 14, are made along the long, parallel edges between the solar cells 14. These series connections are completed without being attached to a substrate, because strings of connected solar cells 14 can be constructed to any length, including any number of solar cells 14. Once completed, the strings of solar cells 14 are attached and mounted to the substrate 12.

[0015] 2, wires 18 are attached to the ends of the strings of solar cells 14 to either electrically connect the strings to other strings or to terminate the wires into a circuit where the current in the array of solar cells 14 is cut off. String-to-string and circuit termination connections are typically made on the substrate 12, typically using wires 18. However, some solar cell panels 10 use printed circuit board (PCB) type equipment with conductors inlaid therein.

[0016] Adjacent strings of connected solar cells 14 can run parallel or anti-parallel. In addition, strings of connected solar cells 14 can be aligned or misaligned. There are many competing influences on the layout of the solar cells 14. As a result, there are regions where the solar cells 14 are parallel or anti-parallel, aligned or misaligned.

[0017] Figures 3A-3B show an improved structure of solar cell panel 10a according to one embodiment, with Figure 3B being an enlarged view of the detail within the dashed circle in Figure 3A. In Figures 5-13, various components of solar cell panel 10a are shown and described in more detail.

[0018] The solar cell panel 10a includes a substrate 12 for the solar cells 14, having one or more corner conductors 20 thereon. In one embodiment, the substrate 12 is a multi-layer substrate 12 consisting of one or more Kapton® (polyimide) layers separating one or more patterned metal layers. The substrate 12 may be attached to a larger, rigid substrate 10a, similar to conventional assembly. Alternatively, the substrate 12 can be attached to a lighter, thinner frame or panel 10a for mounting or deployment.

[0019] A plurality of solar cells 14 are mounted on substrate 12 in a two-dimensional (2D) grid in array 22. In this example, array 22 consists of 96 solar cells 14 arranged in 4 columns and 24 rows, although it is recognized that any number of solar cells 14 may be used in different embodiments.

[0020] At least one of the solar cells 14 has at least one trimmed corner 24, as indicated by the dashed circle, that defines a corner region 26. The solar cells 14 are attached to the substrate 12 such that the corner regions 26 of adjacent solar cells 14 are aligned, thereby exposing an area 28 of the substrate 12. The exposed area 28 of the substrate 12 includes one or more corner conductors 20, and one or more electrical connections are made between the solar cell 14 and the corner conductors 20 within the corner region 26 created by the trimmed corners 24 of the solar cell 14.

[0021] In this example, corner conductors 20 are conductive paths attached to, printed on, embedded within, or deposited on substrate 12 before and / or after solar cells 14 are attached to substrate 12 to facilitate connection between adjacent solar cells 14. The connection between solar cells 14 and corner conductors 20 is made after solar cells 14 are attached to substrate 12.

[0022] In one embodiment, four adjacent solar cells 14 are aligned on substrate 12, with four trimmed corners 24, one from each solar cell 14, coming together at corner regions 26. The solar cells 14 are then individually attached to substrate 12, with the solar cells 14 resting on corner conductors 20 and electrical connections being made between the solar cells 14 and the corner conductors 20.

[0023] The solar cells 14 can be attached to the substrate 12 as a CIC (cell, interconnect, cover glass) unit. Alternatively, uncoated solar cells 14 can be assembled on the substrate 12, followed by the attachment of interconnects to the solar cells 14, followed by the application of a cover glass for a single solar cell 14, a cover glass for a multi-cell solar cell 14, a polymer cover sheet for a multi-cell solar cell 14, or a spray-on encapsulant. This assembly protects the solar cells 14 from damage that could limit their performance.

[0024] 4A and 4B show an alternative structure of solar cell panel 10a, according to one embodiment, with FIG. 4B being an enlarged view of the detail within the dashed circle in FIG. 4A. In this example, only a few corner conductors 20 are printed on or embedded in substrate 12. Alternatively, most of the corner conductors 20 may be contained within a power routing module (PRM) 30 that is attached to substrate 12, as described in more detail below in connection with FIGS. 14-23.

[0025] 5 shows a front view of an exemplary solar cell 14 that can be used in the improved solar cell panel 10a of FIGS. 3A and 3B and 4A and 4B. The solar cell 14, which is a CIC unit, is a half-size solar cell 14. (Full-size solar cells 14 can also be used.)

[0026] As indicated by the dashed circle, the solar cell 14 is fabricated with at least one trimmed corner that defines a corner region 26, whereby the corner region 26 created by the trimmed corner 24 includes at least one contact 32, 34 that makes an electrical connection with the solar cell 14. In the example shown in FIG. 5, the solar cell 14 has two trimmed corners 24, each with a front contact 32 on the front side of the solar cell 14 and a back contact 34 on the back side of the solar cell 14, with the contacts 32 and 34 extending into the corner region 26. (A full-sized solar cell 14 has four trimmed corners 24, each with one front contact 32 and one back contact 34.)

[0027] The trimmed corners 24 encourage the use of circular wafers as the starting material for the solar cells 14. In a conventional panel 10, these trimmed corners 24 result in unused space on the panel 10 after the solar cells 14 are attached to the substrate 12. However, the new approach described in this disclosure utilizes this unused space. Specifically, the metal foil interconnects, including the corner conductors 20, front contacts 32, and back contacts 34, are moved to the corner regions 26. In contrast, existing CICs have interconnects attached to the front of the solar cells 14 and are connected to the back (where splicing occurs) during string fabrication.

[0028] Current generated by the solar cells 14 is collected on the front surface of the solar cells 14 by a grid 36 of thin metal fingers 38 and wider metal bus bars 40 connected to either front contact 32. Adding metal to the grid 36 balances the reduction in light entering the solar cells 14 and thus their power output, while the additional metal reduces resistance. The bus bars 40 are low-resistance conductors that carry high currents and provide redundancy in case a front contact 32 is severed. Optimization typically requires short bus bars 40 that extend directly between the front contacts 32. Having the front contacts 32 within the trimmed corners 24 results in the bus bars 40 being spaced away from the perimeter of the solar cells 14. This is accomplished while simultaneously minimizing the length of the bus bars 40 and minimizing light shading. This also results in shorter fingers 38. This reduces parasitic resistance within the grid 36 because the shorter fingers 38 reduce the total amount of current carried. This creates a design preference to move the front contact 32 and mating busbar 40 to allow for shorter thin fingers 38.

[0029] Figure 6 shows the backside of the exemplary solar cell of Figure 5. The backside of the solar cell 14 has a backside layer 42 that connects to both backside contacts 34.

[0030] 7 illustrates solar cells 14 arranged in a 2D grid in an array 22, according to one embodiment. The array 22 includes a plurality of solar cells 14 attached to a substrate 12 such that corner regions 26 of adjacent solar cells 14 are aligned, thereby exposing an area 28 of the substrate 12. Electrical connections (not shown) between the solar cells 14 are made in the exposed area 28 of the substrate 12 using front and back contacts 32, 34 of the solar cells 14 and corner conductors 20 (not shown) formed on or within the exposed area 28 of the substrate 12.

[0031] During assembly, the solar cells 14 are individually attached to the substrate 12. This assembly can occur directly on a support surface, which can be either rigid or flexible, i.e., the substrate 12. Alternatively, the solar cells 14 may be assembled into a 2D grid-like array 22 on a temporary support surface and then transferred to the final support surface, i.e., the substrate 12.

[0032] 8 shows an embodiment of an array 22 in which one or more bypass diodes 44 have been added to exposed areas 28 in corner regions 26 of substrate 12 for use in one or more electrical connections. The bypass diodes 44 protect the solar cells 14 if they are unable to generate current, which may be due to being partially shaded, causing the solar cells 14 to become reverse biased. In one embodiment, the bypass diodes 44 are attached to the corner regions 26 of the substrate 12 separately from the solar cells 14.

[0033] FIG. 9 shows an embodiment in which a bypass diode 44 is attached to the back surface of the solar cell 14, with an interconnect or contact 46 for the bypass diode 44 connected to the back surface 42 and extending into the corner region 26 between the front contact 32 and the back contact 34.

[0034] FIG. 10 shows a front view of the embodiment of FIG. 9 in which an interconnect or contact 46 for a bypass diode 44 (not shown) extends into the corner region 26 between the front contact 32 and the back contact 34.

[0035] FIG. 11 shows the solar cells 14 of FIGS. 9 and 10 arranged in a 2D grid array 22 and attached to the substrate 12, with bypass diodes 44 (not shown) attached to the backside of the solar cells 14 and contacts 46 for the bypass diodes 44 extending into the corner regions 26 of the solar cells 14.

[0036] One advantage of this approach is that the layouts shown in Figures 7, 8, and 11 are generalized layouts. Specifically, these layouts can be repeated across any customer-desired size of panel 10a. This greatly simplifies the assembly, modification, testing, and inspection processes.

[0037] Following the placement of the solar cell 14 and bypass diode 44, there is another step in which customization occurs. In the corner regions 26 of the solar cell 14, the front contact 32 and the back contact 34 must be connected. This can be done in a number of combinations to route the current in the desired path.

[0038] After the solar cells 14 are attached to the substrate 12, connections are made between the solar cells 14 and the corner conductors 20. A front contact 32 and a back contact 34 of the solar cells 14 are located in each corner region 26 for attachment to the corner conductors 20. The interconnects for the front contact 32 and back contact 34 of each solar cell 14 can be welded, soldered, or otherwise bonded to the corner conductors 20 to provide a conductive path 20, 32, 34 that routes current externally to the solar cell 14.

[0039] The corner conductors 20 allow for any customization of electrical connections. Adjacent solar cells 14 can be electrically connected to pass current up and down or side to side, depending on the specific design needs. Current can also be routed around stayout areas, if desired. The length and width of the solar cell array 22 can be configured as desired. The width of the array 22 can also vary along its length.

[0040] In one embodiment, the electrical connections are series connections that determine the amount of current flow through the solar cells 14. This can be achieved by the connection schemes shown in Figures 12 and 13. Figure 12 shows vertical series connections 48 between the solar cells 14 in the array 22, and Figure 13 shows horizontal series connections 50 between the solar cells 14 in the array 22. In both Figures 12 and 13, these series connections 48, 50 are electrical connections between the front and back contacts 32, 34 of the solar cells 14 and the bypass diodes 44, and these series connections are made using corner conductors 20 formed on or in the exposed areas 28 of the substrate 12. Unlike a large string assembly without being attached to a substrate, the amount of current (power) flowing through the solar cells 14, indicated by arrow 52, ​​is determined by these series connections 48, 50.

[0041] The corner conductors 20 between the solar cells 14 can take a variety of forms. The corner conductors 20 can be completed using electrical wires with electrical connections made at both ends, which can be by soldering, welding, conductive adhesive, or other processes. In addition to electrical wires, metal foil connectors similar to interconnects can also be applied. Metal conductor paths or traces (not shown) can also be incorporated into the substrate 12.

[0042] In summary, this new approach attaches solar cells 14 individually to a substrate 12 so that the corner regions 26 of two, three, or four adjacent solar cells 14 are aligned on the substrate 12. The solar cells 14 can be laid out so that the trimmed corners 24 are aligned and the corner regions 26 are adjacent, thereby exposing areas 28 of the substrate 12. Electrical connections between the solar cells 14 are made within these corner regions 26 between the front and back contacts 32 of the solar cells 14, the bypass diodes 44 on or within the exposed areas 28 of the substrate 12, and the corner conductors 20. These conductive paths are used to create strings of solar cells 14 in series connections 48, 50 that comprise the circuit.

[0043] Power Routing Module While the use of electrical connections between solar cells 14 in corner regions 26 facilitates automation, there is still a need for a variety of corner conductors 20 that can achieve different configurations to allow for the customization required by customers. However, this may require a large number of corner conductors 20 in corner regions 26, resulting in corner conductors 20 being densely packed together, creating electrostatic discharge (ESD) concerns.

[0044] On the other hand, to maximize power generation from an array of solar cells 14, it is desirable to have as small a corner area 26 as possible. To reduce labor and component costs during assembly, it is desirable to have larger solar cells 14. However, the designs described herein change this assessment, and there is little cost penalty as a result of having smaller solar cells 14. Smaller solar cells 14 are advantageous for filling up the area on the wafer, as well as the panel 10a. Smaller solar cells 14 lead to better utilization of materials and labor. However, smaller solar cells 14 also lead to smaller trimmed corners 24 and corner areas 26, which creates connection strategy challenges.

[0045] This disclosure describes a PRM 30 that customizes the corner conductors 20 used in the corner region 26. The PRM 30 is attached to the substrate 12 within the corner region 26. Rather than forming all of the corner conductors 20 on the substrate 12, most of the corner conductors 20 are contained within the PRM 30. Different versions of the PRM 30 with different conductor 20 layouts (e.g., 2D or 3D) can be selected to create a desired connection layout for the array 22.

[0046] 14 is a schematic side view of one embodiment of a substrate 12 at the bottom and a PRM 30 at the top, where the substrate 12 is an assembly of flexible sheets. The substrate 12 includes a polyimide base layer 54 with a copper (Cu) layer 56a on top and a Cu layer 56b below, where the Cu layers 56a and 56b form a multi-layer conductor. The Cu layer 56a is patterned as corner conductors 20, and the Cu layer 56b is patterned to form buried conductors within the substrate 12, including, for example, V+, V-, and bridging lines. The substrate 12 can be provided with a conductive polyimide backsheet 58, which is useful in space environments for reducing charge buildup.

[0047] Shown on the right is the solar cell 14 attached to the substrate 12 with adhesive 60. Metal foil interconnects 62 attached to the solar cell 14 and corner conductors 20 can also be seen.

[0048] The substrate 12 also includes an insulating layer separating at least one of the multilayer conductors 56 a, 56 b from at least another of the multilayer conductors 56 a, 56 b. In one embodiment, there is a top polyimide overlay layer 64 a and a bottom polyimide overlay layer 64 b. Polyimide has a high breakdown strength greater than that of air or vacuum, and the polyimide overlay layers 64 a, 64 b are useful for preventing ESD, which is a concern in the space environment.

[0049] The PRM 30 is located on top of the substrate 12 to provide electrical interconnection between the solar cells 14 in the array 22. The PRM 30 comprises an insulating layer including a polyimide base layer 66 and a conductive layer including a single Cu layer 68 deposited thereon. The Cu layer 68, including one or more corner conductors 20, is used to provide electrical interconnection between the solar cells 14, and the polyimide base layer 66 is used to electrically insulate the corner conductors 20 of the Cu layer 68.

[0050] The base layer 66 of the PRM is shown as being polyimide, but can be selected from a wide variety of insulators appropriate for the environment, including other suitable polymers and ceramics such as glass or alumina. An advantage of glass or other transparent insulators is that they can be used in conjunction with a laser welding process, in which a laser beam is transmitted through the insulator and the energy of the laser beam is absorbed by the conductive traces 68 on the PRM 30.

[0051] The top surface (the surface facing the sun) of the PRM 30 can have a highly reflective coating, such as Al foil bonded to polyimide, which will reflect solar energy, reduce heating of the solar array 22, and reduce the operating temperature of the solar cells 14, resulting in increased power production.

[0052] PRM 30 may include bypass diodes 44 to protect solar cells 14 from reverse bias, and bypass diodes 44 may be connected to one or more corner conductors 20 of PRM 30 by interconnects 62. PRM 30 may also include adhesive 70 for attaching PRM 30 to substrate 12 and electrical joints 72 for connecting one or more of PRM 30 corner conductors 20 to one or more of the corner conductors 20 of substrate 12, such as for connecting Cu layer 66 to Cu layer 56a.

[0053] 15 is a schematic side view of the embodiment of FIG. 14 in which PRM 30 is attached to substrate 12 using adhesive 70. PRM 30 is attached to substrate 12 in areas 28 that would remain exposed in corner regions 26 of substrate 12 when solar cell 14 is attached to substrate 12. In this embodiment, electrical connection is made by electrical joints 72 sandwiched between one or more corner conductors 20 of PRM 30 and one or more corner conductors 20 of substrate 12 (e.g., between Cu layers 56a and 66). Electrical joints 72 could be achieved by directly connecting layer 68 to Cu layer 56a, by solder, or via the laser welding process described above, or via an ultrasonic welding process.

[0054] 16 shows a top view of a corner region 26 of a solar cell 14 in an array 22, including the front and back contacts 32 and 34, and without a PRM 30 attached. Only a few corner conductors 20 are shown in this view. The area 28 left exposed in the corner region 26 of the substrate 12 also includes electrical pads 74 that provide contact between the PRM 30 and a conductive path within the substrate 12, such as a V+ or V− line, a buried line, or other conductive path buried or inlaid within the substrate 12 (e.g., within Cu layer 56b). This is a common design for all corner regions 26, regardless of application or RPM 30.

[0055] FIG. 17 shows one embodiment in which the PRM 30 electrically interconnects the solar cells 14 by making series connections 48 between them. It should be noted that FIG. 17 shows the structure from the sun's perspective, as seen through the polyimide base layer 64 (not shown), as does FIG. 18. Corner conductor 20a connects to the back contact 34 of the top-left solar cell 14 (not shown), corner conductor 20b connects to the front contact 32 of the bottom-left solar cell 14 (not shown), and corner conductor 20c connects to the back contact 34 of the bottom-left solar cell 14 (not shown) through bypass diode 44a. Corner conductor 20d connects to the back contact 34 of the bottom-right solar cell 14 (not shown), corner conductor 20e connects to the front contact 32 of the top-right solar cell 14 (not shown), and corner conductor 20f connects to the back contact 34 of the top-right solar cell 14 (not shown) through bypass diode 44b.

[0056] It should be noted that minor modifications can rotate the PRM 30 to change the functionality of the connections between the solar cells 14. For example, the PRM 30 of Figure 17 could be rotated to provide a left-right series connection 50.

[0057] 18 shows another embodiment in which PRM 30 electrically interconnects solar cells 14 with one or more power lines within substrate 12. In this embodiment, corner conductor 20a terminates the back contact 34 of the top-left solar cell 14 (not shown) at a pad 74 for a buried V+ line (not shown), corner conductor 20b terminates the front contact 32 of the bottom-left solar cell 14 (not shown) at a pad 74 for a buried V- (common) line (not shown), and corner conductor 20c connects to the back contact 34 of the bottom-left solar cell 14 (not shown) through bypass diode 44a. Both corner conductors 20a, 20b are dual-redundantly connected to V+ and V- line pads 74, although more or fewer connections can be made as desired. As in Figure 17, corner conductor 20d is connected to the back contact 34 of the lower right solar cell 14 (not shown), corner conductor 20e is connected to the front contact 32 of the upper right solar cell 14 (not shown), and corner conductor 20f is connected to the back contact 34 of the upper right solar cell 14 (not shown) through bypass diode 44b.

[0058] Other configurations of PRM 30 and its connections to substrate 12 can be found in the previously cross-referenced U.S. patent application Ser. No. xx / xxx, xxx, entitled "POWER ROUTING MODULE FOR A SOLAR ARRAY," filed Sep. 14, 2016, by Eric Rehder, Attorney Docket No. 16-0440-US-NP (G&C 147.217-US-U1), and U.S. Provisional Patent Application Ser. No. 62 / 394,649, entitled "POWER ROUTING MODULE FOR A SOLAR ARRAY," filed Sep. 14, 2016, by Eric Rehder, Attorney Docket No. 16-0440-US-PSP (G&C 147.217-US-P1).

[0059] 19 shows the layout of an array 22 consisting of 4 rows and 8 columns of solar cells 14 labeled as cell 1 (14) through cell 32 (14), where the numbering of the solar cells 14 corresponds to the direction of current flow as determined by the PRMs 30 electrically interconnecting the solar cells 14 within a column of the solar cells 14. Additionally, the PRMs 30 for the third / fourth, fifth / sixth, and seventh / eighth columns of the first column cooperate with the PRMs 30 for the first / second, and fifth / sixth columns of the second column to terminate the circuits between the solar cells 14. The fourth or bottom column PRM 30 bridges the current between the columns.

[0060] Other layouts of array 22 using PRM 30 are also found in the previously cross-referenced U.S. patent application Ser. No. xx / xxx, xxx, filed Sep. 14, 2016, by Eric Rehder, entitled "POWER ROUTING MODULE FOR A SOLAR ARRAY," Attorney Docket No. 16-0440-US-NP (G&C 147.217-US-U1), and U.S. Provisional Patent Application Ser. No. 62 / 394,649, filed Sep. 14, 2016, by Eric Rehder, entitled "POWER ROUTING MODULE FOR A SOLAR ARRAY," Attorney Docket No. 16-0440-US-PSP (G&C 147.217-US-P1).

[0061] Power routing module with switching matrix Although it is possible to fabricate a solar cell array 22 with corner conductors 20 fixed on the substrate 12, the implementation of a static PRM 30 as described above offers significant flexibility and ease of design and manufacturing. Instead of using the static PRM 30 described above with fixed connections between different corner conductors 20, this disclosure describes how a PRM 30 with a switching matrix can make these connections. By placing the switching matrix in the PRM 30, the amount of space for the switching matrix can be maximized.

[0062] In particular, this disclosure describes a PRM 30 with a switching matrix for dynamically selecting different conductor 20 layouts for different current paths. The use of a PRM 30 with a switching matrix overcomes imperfections in a solar cell array 22.

[0063] Currently, due to considerable concern about failures that could result in power loss, space-based solar cell arrays 22 are designed to produce more power than necessary. During operation in space, the solar cell array 22 is exposed to solar radiation and other factors that could result in the loss of one or more solar cells 14 due to degradation or damage.

[0064] During operation, especially in orbit, reliability of the solar cell array 22 is problematic when using the static PRM 30 described above. For example, a failure of one solar cell 14 could rob an entire circuit, which may contain 50 solar cells 14. Thus, the circuit acts like a failure multiplier, and the failure of a single solar cell 14 appears as the failure of many solar cells 14. In another example, depending on the distribution, 10 faulty solar cells 14 could eliminate 10 circuits containing 500 solar cells 14. With conventional manufacturing, these 10 solar cells 14 would prevent the power production of another 490 non-faulty solar cells 14. The present disclosure is based on restoring such power.

[0065] Currently, there is no way to control power or route and / or re-route power due to failure or degradation of a cell 14. Instead, redundancy is built into the solar cell array 22 to ensure that sufficient power is available to the vehicle or equipment in light of such failure or degradation. However, this leads to extensive over-design of the solar cell array 22 to ensure operation, where the solar cell array 22 is built with additional solar cells 14 to account for the possibility of loss.

[0066] The solution proposed herein eliminates the need to overdesign the solar cell array 22. By including a switching matrix in the PRM 30, connections can be changed during operation. If a solar cell 14 fails, it can simply be skipped, allowing all other solar cells 14 in the circuit to be used without penalty. This greatly improves the reliability of power production, especially in environments that put solar cells 14 at risk.

[0067] In one embodiment, a method and system for switchably routing power in a solar cell array 22 includes an addressable switching matrix having multiple paths connected between a PRM 30 and multiple solar cells 14, the addressable switching matrix configured to route current (power) flow in response to a control signal. The connections made by the switching matrix may be changed during operation of the solar cell array 22. The series, stayout, and termination configurations of each cell-to-cell connection may be changed as needed. Optionally, the control signal may be a wireless control signal from a remote source, eliminating the need for external wiring in the panel 10a.

[0068] The switching matrix can be implemented with electronic switches or mechanical relays, although mechanical relays tend to be cumbersome and consume more power than electronic switches. In either example, the switching matrix can be powered by the vehicle's power system, or alternatively, directly from the solar cells 14 in the panel 10a. Important criteria are the ability to connect to multiple input and output paths, very low power consumption, and the ability to function in a space environment.

[0069] 20 shows an example of a PRM 30 having a switching matrix 76 for electrically interconnecting multiple solar cells 14 in an array 22, the switching matrix 76 configured to dynamically route power among multiple current paths connected between the PRM 30 and the multiple solar cells 14 via pads 74, one or more bypass diodes 44, one or more power or buried lines via pads 74, as shown by solid lines. Control signals are provided to pads 78 of the switching matrix 76, which may include multiple conductors.

[0070] In one example, the switching matrix 76 is an electronic switching matrix 76 comprising space division circuit switches within which power in selected input paths is connected to selected output paths, however, the switching matrix 76 may also be implemented by electromechanical or electronic means.

[0071] The switching matrix 76 consists of a crossbar switch containing NxN crosspoints, where N is the number of input paths and the number of output paths. A control signal at each crosspoint, which is a gate, connects a selected input path to a selected output path.

[0072] The switching matrix 76 may consist of multi-stage switches, which reduces the number of crosspoints and therefore the complexity of the switches 76. Again, a control signal at each stage connects a selected input path to a selected output path.

[0073] Figure 21 is a schematic side view similar to the embodiment of Figure 15, showing PRM 30 including a switching matrix 76. In this example, switching matrix 76 is mounted on top of polyimide layer 66 and electrically connected to one or more of the corner conductors 20 of PRM 30.

[0074] PRM 30 with switching matrix 76 is attached to substrate 12 in area 28 of substrate 12 in corner region 26 that will remain exposed when solar cells 14 are attached to substrate 12. As shown in FIG. 22, there are slight modifications to conductors 20 in corner region 26 compared to the previous figure. For example, pad 78 is used for one or more control signals and one or more conductors that operate switching matrix 76. Also, pads 80 for V+ and V- line connections are slightly relocated.

[0075] FIG. 23 shows a single connection block 82 within the switching matrix 76, which connects a selected left input path to a selected right output path.

[0076] The switching matrix 76 may consist of one or more connection blocks 82, each of which connects a selected input path to a selected output path in accordance with a control signal. The control signal at each connection block 82 connects the selected input path to a selected output path.

[0077] In this example, for a single connection block 82, there are 16 input paths on the left, labeled Connection 1, that can be connected to 16 output paths on the right. The paths are each labeled: Cell 1 front (32), Cell 1 back (34), Cell 2 front (32), Cell 2 back (34), Cell 3 front (32), Cell 3 back (34), Cell 4 front (32), Cell 4 back (34), Diode 1N (n-face) (44), Diode 1P (p-face) (44), Diode 2N (n-face) (44), Diode 2P (p-face) (44), V+1, V+2, V−, and Unused. These assignments correspond to the connected pads 74 in FIG. 20. In the connection block 82 labeled Connection 1, the input path Cell 1 back contact 34 is connected to the output path Cell 2 front contact 32, which is the standard series configuration for current flow between solar cells 14.

[0078] The table below describes six connections made using the switching matrix 76 of the PRM 30 in a standard series configuration for current flow between four solar cells 14 aligned in the corner regions 26 of the substrate 12. TIFF0007784976000001.tif80170

[0079] In another example, the table below describes eight connections made using the switching matrix 76 of the PRM 30 in a standard series configuration for current flow between four solar cells 14 aligned in a corner region 26, with some of the solar cells 14 terminating in V+ and V- lines buried within the substrate 12 (e.g., layer 56b). TIFF0007784976000002.tif105170

[0080] In one example, a combination of static corner conductors 20, static PRMs 30, and PRMs 30 with a switching matrix 76 may be used in the solar cell array 22, with the PRMs 30 with the switching matrix 76 distributed in some manner throughout the solar cell array 22. In another example, only PRMs 30 with the switching matrix 76 may be used in the solar cell array 22. While FIG. 20 shows a switching matrix 76 that completely controls the current routing, in many situations it will be sufficient to implement a smaller, simpler switch 76 with fewer components.

[0081] The solar cell array 22 could have multiple switching matrices 76. To control multiple switching matrices 76, each switching matrix 76 would require an identifier and instructions to identify its switching configuration. Multiple switching matrices 76 could have the same switch configuration and switch together, thus sharing an identifier. In either case, it is necessary to uniquely address the switching matrix 76, each connection block 82 containing the switching matrix 76, and selected input and output paths within each connection block 82.

[0082] In one example, a 16-bit address is used to uniquely address a PRM 30 with a switching matrix 76. The 16-bit address can identify 65,536 distinct addresses in unsigned notation, with integer values ​​from 0 to 65,535.

[0083] In one example, the 16-bit value is also used to uniquely address the input and output path selections within the connection pads 78 of the switching matrix 76 when there are 16 possible input paths and 16 possible output paths in the switching matrix 76. When eight connection blocks are used, as described in the previous table, a total of 128 bits (16 x 8) are required to address all of the input and output path selections.

[0084] In one example, the switching matrix 76 also requires two additional lines for power and return. If addressed as individual lines, the switching matrix 76 would require 16+128+2 lines or 146 lines. (Alternatively, power could be drawn directly from the solar array 22.)

[0085] Obviously, running 146 lines in parallel would be cumbersome. However, these lines carry very little current or power and therefore can be very narrow. The resolution of the flex circuit is in the 2 mil range, which means that 144 lines, each 2 mil wide, with 144 spaces between them, would be roughly 1 / 2 inch all over pad 78. This is cumbersome, although not impossible.

[0086] Preferably, information would be transmitted in a serial pattern of bits. Using a device such as a shift register, the serial data would be conveyed on the data lines and a clock. Thus, the 144 data lines could be reduced to two lines, simplifying layout and increasing reliability.

[0087] An alternative addressing possibility is to use radio electromagnetic or optical control signals broadcast from a remote source such as the satellite itself or a ground station via the satellite, which would reduce complexity even further.

[0088] manufacturing Each embodiment of the present disclosure may be described in relation to a method 84 for manufacturing a solar cell 14, a solar cell panel 10a, and / or a satellite, including steps 86-98 shown in FIG. 24, and the resulting satellite 100 having a solar cell panel 10a made of solar cells 14 is shown in FIG. 25.

[0089] 23 , during the pre-production phase, an example method 84 may include specification and design 86 of the solar cell 14, solar cell panel 10a, and / or satellite 100, and sourcing 88 of these materials. During the production phase, component and subassembly manufacturing 90 of the solar cell 14, solar cell panel 10a, and / or satellite 100, and system integration 92 occurs, including manufacturing of the solar cell 14, solar cell panel 10a, and / or satellite 100. The solar cell 14, solar cell panel 10a, and / or satellite 100 may then undergo certification and delivery 94 for placement in service 96. The solar cell 14, solar cell panel 10a, and / or satellite 100 may be scheduled for servicing and maintenance 98 (including modification, reconfiguration, refurbishment, etc.) prior to launch.

[0090] Each step of method 84 may be performed or implemented by a system integrator, a third party, and / or an operator (e.g., a customer). For purposes of this specification, a system integrator may include, but is not limited to, any number of solar cell, solar cell panel, satellite, or spacecraft manufacturers and primary system subcontractors; a third party may include, but is not limited to, any number of vendors, subcontractors, and suppliers; and an operator may be a satellite communications company, military organization, service organization, etc.

[0091] 25, a satellite 100 produced by the example method 84 may include a system 102, a body 104, a solar cell panel 10a made up of solar cells 14, and one or more antennas 106. Examples of systems 102 included in the satellite 100 include, but are not limited to, one or more of a propulsion system 108, an electrical system 110, a communication system 112, and a power system 114. Any number of other systems 102 may also be included.

[0092] 26 illustrates in functional block diagram form a solar cell panel 10a according to one embodiment. The solar cell panel 10a comprises a solar cell array 22 consisting of one or more solar cells 14 individually mounted on a substrate 12. Each solar cell 14 absorbs light 116 from a light source 118 and generates an electrical output 120 in response.

[0093] At least one solar cell 14 has at least one trimmed corner 24 defining a corner region 26 whereby an area 28 of the substrate 12 remains exposed when the solar cell 14 is attached to the substrate 12. When multiple solar cells 14 are attached to the substrate 12, the corner regions 26 of adjacent solar cells 14 are aligned, whereby the area 28 of the substrate 12 is exposed.

[0094] The area 28 of the substrate 12 that remains exposed includes one or more corner conductors 20 attached to, printed on, or embedded in the substrate 12, and one or more electrical connections between the solar cells 14 and the corner conductors 20 are made in the corner regions 26. The corner regions 26 may also include one or more bypass diodes 44.

[0095] The corner region 26 includes at least one contact, such as a front contact 32 on the front surface of the solar cell 14 and / or a back contact 34 on the back surface of the solar cell 14 .

[0096] Interconnectors 62 are used to make electrical connections between the solar cells 14 and the corner conductors 20 .

[0097] A power routing module 30 having a switching matrix 76 is mounted on the exposed area 28 of the substrate 12 for dynamically selecting different conductor layouts for different current paths of electrically interconnected solar cells 14 in the array 22.

[0098] Additionally, the present disclosure includes embodiments according to the following clauses: Clause 1. An apparatus for a solar cell array comprising: a power routing module having a switching matrix for electrically interconnecting a plurality of solar cells in the array, the switching matrix configured to dynamically route power between a plurality of current paths connected between the power routing module and the plurality of solar cells, at least one of the solar cells having at least one trimmed corner forming a corner region, an area of ​​the substrate within the corner region remaining exposed when the solar cell is attached to the substrate, and the power routing module having the switching matrix attached to the substrate in the area of ​​the substrate within the corner region that remains exposed. Clause 2. The apparatus of clause 1, wherein the switching matrix is ​​configured to dynamically route power among a plurality of current paths connected between the power routing module and one or more bypass diodes. Clause 3. The apparatus of clause 1 or 2, wherein the switching matrix is ​​configured to dynamically route power among multiple current paths connected between the power routing module and one or more V+, V-, or buried lines. Clause 4. The apparatus of any one of clauses 1 to 3, wherein the switching matrix is ​​configured to dynamically route power in response to one or more control signals. Clause 5. The apparatus of clause 4, wherein the control signal is a wireless control signal from a remote source. Clause 6. The apparatus of any one of clauses 1 to 5, wherein the switching matrix is ​​a space division circuit switch in which current in selected input paths is connected to selected output paths. Clause 7. The apparatus of clause 6, wherein the switching matrix comprises one or more connection blocks, each connecting a selected input path to a selected output path in accordance with a control signal. Clause 8. Apparatus according to any one of clauses 1 to 7, wherein the switching matrix is ​​uniquely addressed. Clause 9. The apparatus of clause 8, wherein each connection block in the switching matrix (76) is uniquely addressed. Clause 10. The apparatus of clause 9, wherein selected input and output paths within each connection block are uniquely addressed. Clause 11. A method comprising: fabricating a power routing module having a switching matrix for electrically interconnecting a plurality of solar cells in an array, the switching matrix configured to dynamically route power between a plurality of current paths connected between the power routing module and the plurality of solar cells, at least one of the solar cells having at least one trimmed corner forming a corner region, an area of ​​the substrate within the corner region remaining exposed when the solar cell is attached to the substrate, and the power routing module having the switching matrix attached to the substrate in the area of ​​the substrate within the corner region that remains exposed. Clause 12. The method of clause 11, wherein the switching matrix is ​​configured to dynamically route power among a plurality of current paths connected between the power routing module and one or more bypass diodes. Clause 13. The method of clause 11 or 12, wherein the switching matrix is ​​configured to dynamically route power among a plurality of current paths connected between the power routing module and one or more power or embedded lines. Clause 14. The method of any one of clauses 11 to 13, wherein the switching matrix is ​​configured to dynamically route power in response to a control signal. Clause 15. The method of clause 14, wherein the control signal is a wireless control signal from a remote source. Clause 16. The method of any one of clauses 11 to 15, wherein the switching matrix is ​​a space division circuit switch in which power in selected input paths is connected to selected output paths. Clause 17. The method of clause 16, wherein the switching matrix comprises one or more connection blocks, each connecting a selected input path to a selected output path in accordance with a control signal. Clause 18. A method according to any one of clauses 11 to 17, wherein the switching matrix is ​​uniquely addressed. Clause 19. The method of clause 18, wherein each connection block in the switching matrix is ​​uniquely addressed. Clause 20. The method of clause 19, wherein selected input and output paths within each connection block are uniquely addressed. Clause 21. A solar cell panel comprising a solar cell array comprising at least one power routing module having a switching matrix for electrically interconnecting a plurality of solar cells in the array, the switching matrix configured to dynamically route power among a plurality of current paths connected between the power routing module and the plurality of solar cells, at least one of the solar cells having at least one trimmed corner forming a corner region, an area of ​​the substrate within the corner region remaining exposed when the solar cell is attached to the substrate, and the power routing module having the switching matrix attached to the substrate in the area of ​​the substrate within the corner region that remains exposed. Clause 22. The solar cell panel of clause 21, wherein the switching matrix is ​​configured to dynamically route power among a plurality of current paths connected between the power routing module and one or more bypass diodes. Clause 23. The solar cell panel of clause 21 or 22, wherein the switching matrix is ​​configured to dynamically route power among a plurality of current paths connected between the power routing module and one or more power or embedded lines. Clause 24. The solar cell panel of any one of clauses 21 to 23, wherein the switching matrix is ​​configured to dynamically route power in response to a control signal. Clause 25. The solar cell panel of clause 24, wherein the control signal is a wireless control signal from a remote source. Clause 26. A solar cell panel as described in any one of clauses 21 to 25, wherein the switching matrix is ​​a space division circuit switch in which power in selected input paths is connected to selected output paths. Clause 27. The solar cell panel of clause 26, wherein the switching matrix comprises one or more connection blocks, each of which connects a selected input path to a selected output path in accordance with a control signal. Clause 28. A solar cell panel according to any one of clauses 21 to 27, wherein the switching matrix is ​​uniquely addressed. Clause 29. The solar cell panel of clause 28, wherein each connection block in the switching matrix is ​​uniquely addressed. Clause 30. The solar cell panel of clause 29, wherein selected input and output paths within each connection block are uniquely addressed.

[0099] The description of the above embodiments has been presented for purposes of illustration and description and is not intended to be exhaustive or to be limited to the disclosed embodiments. Many alternatives, modifications, and variations may be used in place of the specific elements described above.

Claims

1. a plurality of solar cells (14); A substrate (12); a power routing module (30) having a switching matrix (76) for electrically interconnecting the plurality of solar cells (14) in the array, the switching matrix (76) configured to dynamically route power among a plurality of current paths connected between the power routing module (30) and the plurality of solar cells (14); At least one of the solar cells (14) has at least one trimmed corner (24) that forms a corner region (26); an area (28) of the substrate (12) within the corner region (26) that remains exposed when the solar cell (14) is attached to the substrate (12); the plurality of current paths are provided on or within the substrate (12); The power routing module (30) having the switching matrix (76) is attached to the substrate (12) in the area (28) of the substrate within the corner region (26) that remains exposed, and is electrically connected to the plurality of current paths by electrically connecting electrical contacts provided on the solar cells (14) with electrical contacts provided on the substrate (12).

2. 2. The apparatus of claim 1, wherein the switching matrix (76) is configured to dynamically route power among the plurality of current paths connected between the power routing module (30) having one or more bypass diodes (44) and the plurality of solar cells (14).

3. 3. The apparatus of claim 1, wherein the switching matrix (76) is configured to dynamically route power among the plurality of current paths connected between the power routing module (30) and one or more V+, V-, or buried wires.

4. 4. The apparatus of claim 1, wherein the switching matrix (76) is configured to dynamically route power in response to one or more control signals.

5. The apparatus of claim 4 , wherein the control signal is a wireless control signal from a remote source.

6. 6. The apparatus of claim 1, wherein the switching matrix (76) is a space division circuit switch in which current in selected input paths is connected to selected output paths.

7. 7. The apparatus of claim 6, wherein the switching matrix (76) comprises one or more connection blocks, each connecting the selected input path to the selected output path in accordance with a control signal.

8. 8. Apparatus according to any one of claims 1 to 7, wherein the switching matrix (76) is uniquely addressed.

9. 8. The apparatus of claim 7, wherein each of the connection blocks in the switching matrix (76) is uniquely addressed.

10. 10. The apparatus of claim 9, wherein selected input and output paths within each of the connection blocks are uniquely addressed.

11. Fabricating a power routing module (30) having a switching matrix (76) for electrically interconnecting a plurality of solar cells (14) in an array. the switching matrix (76) configured to dynamically route power among a plurality of current paths connected between the power routing module (30) and the plurality of solar cells (14); At least one of the solar cells (14) has at least one trimmed corner (24) that forms a corner region (26); an area of ​​the substrate (12) in the corner region (26) that remains exposed when the solar cell (14) is attached to the substrate (12); the plurality of current paths are provided on or within the substrate (12); The power routing module (30) having the switching matrix (76) is attached to the substrate (12) in the area (28) of the substrate within the corner region (26) that remains exposed, and is electrically connected to the plurality of current paths by electrically connecting electrical contacts provided on the solar cells (14) with electrical contacts provided on the substrate (12).

12. 12. The method of claim 11, wherein the switching matrix (76) is configured to dynamically route power among the plurality of current paths connected between the power routing module (30) having one or more bypass diodes (44) and the solar cells (14).

13. 13. The method of claim 11 or 12, wherein the switching matrix (76) is configured to dynamically route power among the plurality of current paths connected between the power routing module (30) and one or more power or embedded lines.

14. 14. The method of any one of claims 11 to 13, wherein the switching matrix (76) is configured to dynamically route power in response to a control signal.

15. The method of claim 14 , wherein the control signal is a wireless control signal from a remote source.

16. 16. The method of any one of claims 11 to 15, wherein the switching matrix (76) is a space division circuit switch in which power in selected input paths is connected to selected output paths.

17. 17. The method of claim 16, wherein the switching matrix (76) comprises one or more connection blocks, each of which connects the selected input path to the selected output path according to a control signal.

18. 18. The method of any one of claims 11 to 17, wherein the switching matrix (76) is uniquely addressed.

19. 18. The method of claim 17, wherein each of the connection blocks in the switching matrix is ​​uniquely addressed.

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