Embodiments described herein relate to photovoltaic energy sources.
Electrical output of a photovoltaic (PV) panel may vary due to transient obstructions, such as clouds and dust storms. The obstructions are temporarily positioned between the sun and the PV panel, which may reduce electrical generation and accordingly electrical output of the PV panel. Alternatively, obstructions may include a characteristic that increases the electrical output. For instance, bright white clouds may reflect some radiation in addition to that illumination provided by the sun, which may increase the electrical output. The obstructions may be difficult to predict and may result in inconsistent and unreliable electrical output from the PV panel. The inconsistency of the electrical output contributes to an inability of an electrical grid to sufficiently rely on the PV panel.
In general, electrical grids can accommodate some inconsistency in electrical generation and variations in electrical loading. This inconsistency in electrical generation and these variations in electrical loading are usually slow and can be predictable. For example, a very hot day may be predicted. The very hot day may have associated with it a high electrical load, which can be accommodated for in energy markets. Similarly, a particular utility plant may have a scheduled maintenance period, which may result in lowered energy supply. Again, the scheduled maintenance period can be accommodated for in energy markets. For example, the scheduled maintenance and/or the high electrical load may be accommodated for by bringing another plant online, operating at a higher production rate, or purchasing electricity from another source. However, the output of the PV panel, because of transient obstructions, may vary quickly and unpredictably. Thus, the electrical grid cannot accommodate for such output variations of PV panels.
The subject matter claimed herein is not limited to embodiments that solve any disadvantages or that operate only in environments such as those described above. Rather, this background is only provided to illustrate one example technology area where some embodiments described herein may be practiced.
An example embodiment includes a solar photovoltaic (PV) panel. The PV panel may be configured as a modular electrical source. The PV panel may include an electrical PV output, a storage and retrieval subsystem, and one or more PV cells. The electrical PV output is configured to be electrically coupled to a distribution system such that electricity produced by the PV panel is supplied to the distribution system. The storage and retrieval subsystem includes a dedicated energy storage device. The storage and retrieval subsystem is electrically coupled to the PV output and configured to provide per-panel energy storage to the PV panel. The PV cells are electrically coupled to the PV output and electrically coupled to the dedicated energy storage device. The PV cells are configured to photovoltaically generate an electrical potential in response to exposure to incident illumination. During periods in which incident illumination is available to the PV cells, the PV cells supply a first portion of the electrical potential to the PV output and a second portion of the electrical potential to the dedicated energy storage device. The storage and retrieval subsystem is configured to intermediately supply energy stored thereon to the PV output during periods in which incident illumination is partially unavailable or unavailable to the PV cells.
The object and advantages of the embodiments will be realized and achieved at least by the elements, features, and combinations particularly pointed out in the claims.
It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory and are not restrictive of the invention, as claimed.
Example embodiments will be described and explained with additional specificity and detail through the use of the accompanying drawings in which:
all according to at least one embodiment described herein.
The PV panel 100 of
In general, the electrical output of the PV panel 100 is reduced for a period of time while the transient obstruction 110 is positioned between the insolation 108 and the PV panel 100 or a portion thereof.
In the plot 200 of
The first period 212 exists from a time equal to 0 on the plot 200 to a first time 210 and from a second time 213 onward. During the first period 212 the electrical output of the PV panel 100 may be the nominal designed electrical output of the PV panel 100. At the first time 210, the transient obstruction 110 begins to obscure the insolation 108. The transient obstruction 110 may make the insolation 108 unavailable or partially unavailable. The second period 214 may include times from the first time 210 to a second time 213. The second time 213 corresponds to a time at which the transient obstruction 110 is no longer positioned between the insolation 108 and the PV panel 100. During the second period 214, the insolation line 206 and the electrical output line 208 begin to drop, representing a reduction from nominal insolation 108 and a corresponding reduction in electrical output of the PV panel 100. The electrical output and the nominal insolation 108 of the PV panel 100 may continue to be reduced during the second period 214. During the second period 214, the transient obstruction 110 may begin to move away from the PV panel 100, which may increase the insolation 108 and electrical output of the PV panel 100.
At the second time 213, the transient obstruction 110 is no longer positioned between the PV panel 100 and the insolation 108. Accordingly, the insolation 108 may increase and the electrical output of the PV panel 100 may also increase. The first period 212 may last from the second time 213 until another transient obstruction 110 is positioned between the PV panel 100 and the insolation 108.
The plot 200 of
From
Accordingly, some embodiments described in this disclosure include a solar PV panel that is configured as a modular electrical source. The PV panel includes a PV output, a dedicated energy storage device, and one or more PV cells. The PV output is configured to be electrically coupled to an electrical distribution system and to supply electricity to the electrical distribution system. The dedicated energy storage device is electrically coupled to the PV output. The PV cells are electrically coupled to the PV output and electrically coupled to the dedicated energy storage device. The PV cells are configured to photovoltaically generate an electric potential in response to exposure to incident illumination during periods in which incident illumination is available to the photovoltaic cells and to supply a first portion of the electrical potential to the electrical output and a second portion of the electrical potential to the dedicated energy storage device. The dedicated energy storage device is configured to intermediately supply energy stored thereon to the PV output during periods in which incident illumination is unavailable or partially unavailable to the PV cells.
In some embodiments, the dedicated energy storage device includes a flywheel assembly. The flywheel assembly may further include rolling element bearings, passive magnetic bearings, an active magnetic rotor with position control, or some combination thereof. In some embodiments, the dedicated energy storage device may include an electrochemical storage device (e.g., a battery) or a pneumatic storage system. Additionally, in some embodiments, the dedicated energy storage device may include some combination of the flywheel, the electrochemical battery, and the pneumatic storage system.
Although
In addition, the energy storage device may be configured to store energy from the distribution system. Thus, the energy storage device may provide load-following to the distribution system, which may increase stability of the distribution system.
Some additional details of this and other embodiments are discussed with reference to the appended figures. In the appended figures, like numbers correspond to like structures unless described otherwise.
The PV panel 400 thus stores a portion of the energy produced while the insolation 108 is available. In addition, the PV panel 400 may also store energy during periods of high production in the distribution system 120 and/or during period of higher than nominal electrical output of the PV panel 400. The storage subsystem 410 is further configured to retrieve the stored energy and make the stored energy available to the PV panel 400. For example, in response to unavailability or partial unavailability of the insolation 108 or when called upon by an external communication, the storage subsystem 410 may retrieve stored energy. The energy made available by the storage subsystem 410 may be adequate to maintain the nominal electrical output of the PV panel 400 despite some variations in the insolation 108.
The storage subsystem 410 may be characterized by a holdup time. The holdup time may indicate a particular duration in which the storage subsystem 410 provides the nominal electrical output of the PV panel 400 when the insolation 108 is completely unavailable. For instance, the PV panel 400 may include a nominal electrical output 110 Watts and the storage subsystem 410 may include a holdup time may be about 15 minutes. The holdup time indicates the storage subsystem 410 can maintain the nominal electrical output 110 Watts of the PV panel 110 for 15 minutes in the absence of insolation 108.
The holdup time is determined by the size and capacity of the storage subsystem 410. In some implementations, the holdup time may be about 10 minutes. In other implementations, the holdup time may be between about three hours and about five hours, for example. In embodiments in which the holdup time is between about three hours and about five hours, the storage subsystem 410 may provide some percentage of (e.g., 85%) of the nominal electrical output of the PV panel 400 for this period, which may enable some flexibility in the PV panel 400 and the storage subsystem 410 for variations due to transient obstructions 110 during this period.
In addition, the storage subsystem 410 may be configured to store and provide more than the nominal electrical output. Some embodiments of the storage subsystem 410 may provide between about 105% and about 300% of the nominal electrical output of the PV panel 400. For example, the PV panel 400 may include a nominal electrical output 110 Watts. The storage subsystem 410 may provide an electrical output of between about 115 and about 330 Watts. The electrical output of 330 Watts may be used in distribution grid stabilization. For instance, to make up for failures or reductions in production capacities in the distribution system 120.
The storage subsystem 410 provides per-panel energy storage. As used in this disclosure, “per-panel” indicates that the storage subsystem 410 is affiliated with the PV panel 400 and is not affiliated with other PV panels that may be included in a panel array that includes the PV panel 400. For instance, the storage subsystem 410 receives electricity produced by the PV cells 104 of the PV panel 400 and the storage subsystem 410 supplies energy stored thereon to the PV output 106 of the PV panel 400.
Moreover, “per-panel” may indicate control of the electrical output and input (e.g., in load-following applications) on a per-panel basis. For example, instead of a global or centralized control of an array that includes one or more of the PV panels 400, the storage subsystem 410 includes functionality that is dedicated to the control of the electrical output and input of the PV panel 400.
Generally, provision of per-panel energy storage enables distribution of energy storage in a panel array. The distribution of the energy storage enables efficient, rapid, and controllable response to the transient obstructions 110. The response to the transient obstructions 110 may smooth variability in the distribution system 120. For example, an operator of the distribution system 120 may control a ramp rate of the storage device 422 (e.g., the percent of nameplate or nameplate capacity/minute). The ramp rate may be controlled on a per-panel basis.
A panel array that includes a number of the PV panels 100 of
In contrast, panel arrays with the PV panels 400 that use the per-panel storage may accommodate for the transient obstructions 110. The per-panel storage enables rapid mitigation of electricity production reductions on a per-PV panel 400 basis. Moreover, the individual PV panels 400 that are affected by the transient obstructions 110 individually make up for any reductions in local electricity production. In addition, inclusion of the storage device 422 may reduce cooling costs when compared to centralized energy storage systems and may eliminate a threat of a single point of failure.
In some embodiments, the storage subsystem 410 is an on-panel storage subsystem. As used in this disclosure, “on-panel” indicates that the storage subsystem 410 is physically connected or physically incorporated in the PV panel 400. For instance, the storage subsystem 410 may be welded or fastened to a frame of the PV panel. In other embodiments, the storage subsystem may not be on-panel but may still provide per-panel energy storage.
The storage subsystem 410 is sized such that the nominal output can be maintained for a particular duration. The particular duration is either greater than a period of unavailability or partial unavailability of the insolation 108 and/or greater than a period involved in the initiation of another mitigation measure. The storage subsystem 410 thus reduces disturbances to operation of the distribution system 120 to which the PV panel 400 provides electricity. In some embodiments, the particular duration may be about 10 minutes. Some additional details of the particular duration are discussed elsewhere herein.
In the embodiment of
The PV output 106 may be electrically coupled to the distribution system 120. The PV panel 400 may supply some portion of the electricity produced by the PV cells 104 to the distribution system 120 via the PV output 106. For example, during periods in which the insolation 108 is available, a nominal output of the PV panel 400, produced by the PV cells 104 may be supplied to the distribution system 120. In addition, during periods in which the insolation 108 is available, some portion of the energy produced by the PV cells 104 may be provided to the storage subsystem 410 and stored therein.
The storage subsystem 410 may be electrically coupled to the interconnected PV device string 102. For example, in the depicted embodiment, the storage subsystem 410 is electrically coupled in parallel to the PV output 106. The storage subsystem 410 is configured to receive some portion of the electricity produced by the PV cells 104 while the insolation 108 is available and store the electricity. In some embodiments, the storage subsystem 410 may not store the electricity as electrical potential. For instance, the storage subsystem 410 may include a dedicated energy storage device (storage device) 422. The storage device 422 may include any system or device that is capable of storage of energy and retrieval of the stored energy to PV panel 400.
An example of the storage device 422 is a flywheel. Rotation of the flywheel may be imposed due to electricity produced by the PV cells 104. The rotation stores the electricity produced by the PV cells 104 as kinetic energy. Another example of the storage device 422 is an electrochemical battery. The electrochemical battery may be charged by the electricity produced by the PV cells 104. Another example of the storage device 422 may include a compressed gas system. The compressed gas system may use the electricity produced by the PV cells 104 to impose a pressure on a gas. The pressure stores the electricity produced by the PV cells 104 as pneumatic potential energy.
In addition, the storage subsystem 410 is configured to supply stored energy in the form of electricity to the electrical distribution system 120 via the PV output 106. For example, the PV storage subsystem 410 may supply electricity to the distribution system 120 while the insolation 108 is unavailable or partially unavailable. For instance,
The amount of electricity supplied to the distribution system 120 may be related to the effect on the PV panel 400 of the unavailability or partial unavailability of the insolation 108. For example, the storage subsystem 410 may supply electricity to the distribution system 120 such that the nominal electrical output of the PV panel 400 is constant or substantially constant. During periods in which the storage subsystem 410 is supplying electricity to the distribution system 120, the constant or substantially constant nominal electrical output of the PV panel 400 may include a first portion that results from electrical production of the PV cells 104 and a second portion that is supplied from the storage subsystem 410. Additionally, in some circumstances, the storage subsystem 410 may supply all of the nominal electrical output of the PV panel 400.
In some embodiments, the storage subsystem 410 may supply electricity to the distribution system 120 outside of periods of unavailability or partial unavailability of the insolation 108. For example, during peak loads of the distribution system 120, the storage subsystem 410 may supply electricity to the distribution system 120. Additionally or alternatively, the storage subsystem 410 may supply electricity to the distribution system 120 in response to an equipment failure or any other circumstance in which additional electrical output may be beneficial.
An example of the PV panel 400 may include a nominal maximum DC output power of 110 Watts at a nominal output voltage of 69.4 Volts and a nominal output current of 1.59 Amperes. In addition, in
Embodiments depicted in
The plot 500 may be separated into four time periods 520, 522, 524, and 526. A first time period 520 is from time equal to 0 on the plot 500 until a first time 528. The first time 528 represents an onset of insolation reduction.
The first time period 520 is representative of circumstances in which the insolation 108 is available and the storage device 422 of the storage subsystem 410 is substantially full or has reached a limit determined by a customer. During the first time period 520, the electrical output of the PV panel 400 is substantially constant. The electrical output is supplied by electricity produced by the PV cells 104 (of
A second time period 522 is from the first time 528 until a second time 530. The second time 530 represents cessation of the insolation reduction. During the second time period 522, the insolation 108 may be considered unavailable or partially unavailable. In some embodiments, the insolation 108 is considered unavailable or partially unavailable when the nominal electrical output of the PV panel 400 supplied by the PV cells 104 is decreased by more than about 10%. Similarly, the insolation 108 may be considered available so long as about 90% the nominal electrical output of the PV panel 400 is supplied by the PV cells 104.
During the second time period 522, the energy output of the storage subsystem 410 increases relative to a reduction in the insolation 108 such that the electrical output of the PV panel 400 is substantially constant.
A third time period 524 is from the second time 530 until a third time 532. The third time 532 represents a time in which electricity produced by the PV cells 104 is supplied to the storage subsystem 410. During the third time period 524, some amount of energy may be supplied by the storage subsystem 410. However, the electrical output of the PV panel 400 is supplied by the electricity produced by the PV cells 104.
A fourth time period 526 is from the third time 532 until a fourth time 534. The fourth time 534 represents a time in which the storage device 422 of the storage subsystem 410 is full. During the fourth time period 526, the electrical output of the PV panel 400 is supplied by electricity produced by the PV cells 104. In addition, electricity produced by the PV cells 104 is being stored in the storage subsystem 410. In the plot 500, the portion of storage subsystem output line 512 below the horizontal axis 504 represents charging or energy storage.
On the plot 500, the electrical output line 510 is substantially constant. In some embodiments, during the second time period 522, the electrical output line 510 may be somewhat lower. In these and other embodiments, the electrical output line 510 may be a step function beginning at the first time 528 and ending at the second time 530. For example, the electrical output line 510 may be constant during the first time period 520, the third time period 524, and the fourth time period 526. During the second time period 522, the electrical output line 510 may be about 80% of the value during the first time period 520, the third time period 524, and the fourth time period 526.
In
The insolation 108 may impinge on a surface 604 of the PV panel 400. The insolation 108 may result in production of electricity that is communicated via a connection 606 to PV panel output connection cables 612. The PV panel output connection cables 612 connect to a series connection 614. The series connection 614 may be an example of the PV output 106 discussed above. The series connection 614 may electrically connect to another PV assembly and/or to a distribution system (e.g., the distribution system 120 discussed above). The series connection 614 may be positioned in a cable run enclosure 616.
In some embodiments, multiple (e.g., 1000) PV assemblies 600 are installed in series. The cable run enclosure 616 may be constructed below the multiple PV assemblies 600. A cable that connects the PV assemblies 600 may be positioned above the cable run enclosure 616. Each of the PV assemblies 600 may be connected to the cable at the series connection 614.
The PV panel output connection cables 612 connect to storage device connections 618 via panel/storage device connections 620. When the insolation 108 is available, a first portion of the electricity produced by PV cells 104 (not shown) in the PV panel 400 is supplied to the series connection 614. A second portion of the electricity produced by the PV cells 104 is supplied to the storage device 422 via the panel/storage device connections 620 and the storage device connections 618. In response to the insolation 108 being unavailable or partially unavailable, energy stored in the storage device 422 may be supplied to the series connection 614 via the storage device connections 618 and the panel/storage device connections 620.
As depicted in
For example, the storage subsystem 410 manages supply of the electricity produced by the PV device string 102 to the energy storage device 422. In addition, the storage subsystem 410 manages the energy retrieval from the storage device 422 and its supply to the distribution system 120. In some embodiments, the storage subsystem 410 may further manage energy provided by the distribution system 120 to the storage device 422.
The storage subsystem 410 of
The controller 708 may also communicate signals to one or more of the communication unit 714, the MPPT 702, the inverter 704, the energy storage device 422, or some combination thereof. For example, the controller 708 may receive a signal indicative of a reduction in electricity output from the PV device string 102, and the controller 708 may then communicate a control signal that commands the inverter to pull energy from the storage device 422.
In the depicted embodiment, the controller 708 may include one or more processors 710 and memory 712. The processor 710 may include any suitable special-purpose or general-purpose computer, computing entity, or processing device including various computer hardware or software modules and may be configured to execute instructions stored on any applicable computer-readable storage media. For example, the processor 710 may include a microprocessor, a microcontroller, a digital signal processor (DSP), an application-specific integrated circuit (ASIC), a field-programmable gate array (FPGA), or any other digital or analog circuitry configured to interpret and/or to execute program instructions and/or to process data.
Although illustrated as a single processor in
The memory 712 may include computer-readable storage media for carrying or having computer-executable instructions or data structures stored thereon. Such computer-readable storage media may include any available media that may be accessed by a general-purpose or special-purpose computer, such as the processor 710. By way of example, and not limitation, such computer-readable storage media may include tangible or non-transitory computer-readable storage media including RAM, ROM, EEPROM, CD-ROM or other optical disk storage, magnetic disk storage or other magnetic storage devices, flash memory devices (e.g., solid state memory devices), or any other storage medium which may be used to carry or store desired program code in the form of computer-executable instructions or data structures and that may be accessed by a general-purpose or special-purpose computer. Combinations of the above may also be included within the scope of computer-readable storage media. Computer-executable instructions may include, for example, instructions and data configured to cause the processor 710 to perform a certain operation or group of operations.
In the embodiment depicted in
The communication unit 714 may include one or more pieces of hardware configured to receive and send communications. In some embodiments, the communication unit 714 may include one or more of an antenna, a wired port, and modulation/demodulation hardware, among other communication hardware devices. In particular, the communication unit 714 may be configured to receive a communication from outside the PV panel 400 and to present the communication to the processor 710 or to send a communication from the processor 710 to another device or network.
In some embodiments, the communication unit 714 may be configured to communicate status signals pertaining to operations of the PV panel 400. For example, the communication unit 714 may be configured to input/output signals informing a grid manager of an operational status (e.g., state of the charge) of the PV panel 400. Additionally, new programs or changes to instructions may be communicated to the controller 708 via the communication unit 714.
In embodiments including the controller 708 and the communication unit 714, a program may be preset to the controller 708. Control communications may be received by the communication unit 714, which may modify or overwrite the preset program.
In some embodiments, the storage subsystem 410 may include the communication unit 714 but omit the controller 708. In these and other embodiments, the storage subsystem 410 may receive control communications that are directly communicated to one or more of the energy storage device 422, the MPPT device 702, and the inverter 704.
The MPPT device 702 may be electrically coupled to the PV device string 102, the controller 708, and the inverter 704. The MPPT device 702 may be configured to perform MPPT techniques. For example, the MPPT device 702 may be configured to determine an optimal current-voltage (IV) point. The IV point may change due to environmental conditions such as temperature, insolation, and the like.
The inverter 704 may receive a signal from the controller 708 and in response draw energy from the storage device 422. The inverter 704 may convert energy drawn from the storage device 422 and the PV device string 102 from direct current (DC) to alternating current (AC). The inverter 704 may then communicate the electricity converted to AC to the PV output 106.
The inverter 704 may be a bi-directional inverter. In embodiments in which the inverter 704 is bi-directional, electricity may be drawn from the distribution system 120. For example, in circumstances in which the energy production in the distribution system 120 exceeds a load in the distribution system 120, electricity may be drawn from the distribution system 120 and stored in the storage device 422. The electricity may be drawn from the distribution system 120. The electricity is then converted from AC to DC and supplied to the storage device 422.
For example, in some embodiments, the storage device 422 may be set to only charge or store about 50% to about 60% of a designed-for capacity. During periods in which energy generation on the grid is high (more than load), excess electricity is stored on the storage device 422. Storage of the excess electricity is referred to as “load following.”
In some embodiments, the storage subsystem 410 of
Furthermore, the inverter 704 may controllably alter its AC output parameters, including voltage, current, frequency, phase, harmonic content, or any combination thereof. Such alterations may be in response to commands generated off-panel and received by communications unit 714, or in response to algorithms executed by the processor 710, or a combination thereof.
In the embodiment of
In the embodiment depicted in
In the embodiment depicted in
An isolation diode 806 may be incorporated within the storage subsystem 410 and its battery management electronics. Upon the electrical output at the PV output 106 being about equal to or less than the charge of the battery 802, the battery 802 begins to supply electrical energy to the PV output 106. The amount of electrical energy supplied to the PV output 106 may be related to a difference between electrical output and the charge of the battery 802. The battery 802 continues to supply electrical energy to the PV output 106 until insolation 108 is available and the electrical output of the PV panel 400 rises above the charge of the battery 802 or the battery 802 is fully discharged.
In some embodiments, a predetermined portion of electrical energy produced by the PV device string 102 may be used to recharge the battery 802 while continuing to supply energy to the PV output 106.
In contrast with the embodiment of
In a non-depicted embodiment, the storage device 422 may include a flywheel assembly with its integral operational control electronics in close analogy to the embodiment of
The flywheel assembly 900 may be configured with a larger energy storage range and larger energy retrieval range than battery 802 of
The flywheel assembly 900 may include a flywheel rotor 902 that is positioned within an evacuated enclosure 904. In some embodiments, the flywheel rotor 902 may be comprised of a carbon fiber matrix composite material. The carbon fiber may include any suitable material such as M30 product from Toray Carbon Fibers America, Inc. The carbon fiber matrix may be a polymeric form of dicyclopentadiene (DCPD) polymerized according to metathesis reactions, for instance. In other embodiments, the flywheel rotor 902 may be comprised of another material or another polymeric form.
In the embodiment of
Two circular arrays of magnets (magnet arrays) 910A and 910B are imbedded in the flywheel rotor 902. The arrays of magnets 910A and 910B may be disposed in the flywheel rotor 902 during the fabrication of the flywheel rotor 902. The arrays of magnets 910A and 910B rotate with the flywheel rotor 902 and project magnetic fields across the enclosure 904 to interact, respectively, with electromagnetic coil assemblies 912A and 912B. The magnet arrays 910A and 910B may include N42 grade rare earth magnets. One or more individual magnets of magnet arrays 910A and 910B may include a nickel-plated cube. The magnets may include an edge length of about 0.5 inches.
The magnet arrays 910A and 910B are distributed on a top face and a bottom face of flywheel rotor 902. Array centerline radii 916 and 918 may be at about 1.75 inches and about 2.35 inches from a central rotational axis 914 of flywheel rotor 902. The magnets of the magnet arrays 910A and 910B are angularly displaced from its adjacent neighbors by approximately 20 degrees. In the depicted embodiment, the magnet arrays 910A and 910B include eighteen magnets. The flywheel rotor 902 may include fifty-two magnets total. In other embodiments the magnet arrays 910A and 910B may include fewer than eighteen or more than eighteen magnets. Additionally, the magnet arrays 910A and 910B may be positioned at different centerline radii 916 and 918. Other embodiments may include other types or dispositions of magnets and other operative configurations such as an arrangement of magnet polarities in a Halbach configuration as well as magnets of other geometries, and other rare earth magnet grades.
The electromagnetic coil assemblies 912A and 912B may include multiple coils. For example, in an example embodiment, the electromagnetic coil assemblies 912A and 912B may include twelve coils with fifteen turns of #22 insulated copper magnet wire. Each of the coils includes an approximate major diameter of about 1.0 inch. The twelve coils are disposed in a circular pattern and fixed to an outside surface of the enclosure 904, with each of the coils being centered at a radius of about 2.0 inches from a radial center of the enclosure 904. The coils may be positioned on the enclosure 904 at regularly spaced angular positions separated by about 20 degrees around the enclosure 904.
To store energy within the flywheel assembly 900, the electromagnetic coil assemblies 912A and 912B are electrically connected to drive electronics (not depicted) that supply the electromagnetic coil assemblies 912A and 912B with electrical energy. Forces arise from the interaction of electromagnetic fields created by the electromagnetic coil assemblies 912A and 912B with permanent magnetic fields provided by the magnet arrays 910A and 910B. The forces cause the flywheel rotor 902 to increase a rotation rate, thereby effecting the conversion of electrical energy supplied to the electromagnetic coil assemblies 912A and 912B. Increasing the rotation rate increases rotational kinetic energy of the flywheel rotor 902.
To recover electrical energy from the flywheel assembly 900, induced current is driven by the relative motion of electromagnetic coil assemblies 912A and 912B to the magnetic fields from rotating magnet arrays 910A and 910B. The electromagnetic coil assemblies 912A and 912B to a PV output (e.g., the PV output 106) after being transformed and/or rectified according to whether panel output is required as AC or DC power. Rotational kinetic energy is thereby transformed to electrical energy in accordance with principles of electric generators.
The inner diameter 908 of flywheel rotor 902 is mechanically fixed to a shaft 920. The shaft 920 may include a diameter of about 0.500 inch and may be comprised of stainless steel. The flywheel rotor 902 is wound onto the shaft 920 so that in operation, the two components rotate together as an integrated assembly. The shaft 920 may be constructed from stainless steel alloy 316 or similar alloys having a relative magnetic permeability of less than about 100. The shaft 920 may be comprised of other materials having similar magnetic and mechanical properties. Examples of such shaft materials may include titanium, silicon carbide, and cermet compositions. Additionally, in some embodiments, rather than winding the flywheel rotor 902 material directly on the shaft 920. For example, an interface component (not depicted) may be installed between the flywheel rotor 902 and the shaft 920 to provide advantageous mechanical properties, such as enhanced compliance and/or energy dissipation (damping).
In the embodiment of
The repulsive magnets 932A, 932B, 934A, and 934B are oriented so that the radial interaction is repulsive. In addition, radial equilibrium positions occur when the repulsive magnets 932A and 932B are radially and axially centered within the repulsive magnets 934A and 934B, respectively. The repulsive magnets 932A and 932B are fixed to the shaft 920. The repulsive magnets 934A and 934B are fixed to enclosure 904. For example, one or more of the repulsive magnets 932A, 932B, 934A, and 934B may be fixed using J-B Weld® product #8265-S or a similar, suitable adhesive.
In some embodiments, one or more of the repulsive magnets 932A, 932B, 934A, and 934B are comprised of rare earth grade 42. Additionally, in some embodiments, the repulsive magnets 932A and 932B may have inside diameters of about 0.500 inch, outer diameters of about 1.0 inch, and thicknesses (heights) of about 0.5 inches. The repulsive magnets 934A and 934B may have inside diameters of about 0.750 inches, outer diameters of about 1.5 inches, and thicknesses (heights) of about 0.250 inches.
In some embodiments, the passive radial magnetic bearings may include a different structure or orientation. For example, a Halbach magnet array, radially magnetized rings, or rings assembled using magnets shaped as segments of a desired assembled ring may be implemented in the flywheel assembly 900 of
Wear elements 926A, 926B, 928A, 928B, 930A, and 930B fix the axial position of the flywheel rotor 902 and the shaft 920. For example, mechanical interaction of wear elements 926A, 928A, and 930A fix a first end of the shaft 920 and mechanical interaction of wear elements 926B, 928B, and 930B fix a second, opposite end of the shaft 920. Together, the wear elements 926A, 928A, 930A, 926B, 928B, and 930B act as axial or thrust bearings that constrain the axial position of the flywheel rotor 902 and the shaft 920.
The wear elements 926A, 926B, 928A, 928B, 930A, and 930B are manufactured from a wear resistant material. For example, the wear resistant material includes about 95% by volume diamond dust and about 5% metallic binder. Upon treatment with heat and pressure, the metallic binder consolidates the diamond dust into a hard, wear-resistant material that may subsequently be formed and polished to desired shape.
In some embodiments, the wear elements 926A and 926B are plane-parallel discs. The wear elements 926A and 926B may have a diameter of about 0.49 inches and a thickness of about 2.00 millimeters. Opposed faces of the wear elements 926A and 926B may be polished to an average roughness of less than 0.10 microns. One of the wear elements 926A and 926B may be mechanically fixed to each end of shaft 920 prior to rotation. For example, the wear elements 926A and 926B may be brazed to its corresponding position on shaft 920 using a titanium-activated braze. Prior to final assembly, the exposed surfaces of the wear elements 926A and 926B may be coated with a vacuum-compatible solid lubricant (e.g., Molykote® Z powder).
The wear elements 928A and 928B are spheres. The wear elements 928A and 928B may be comprised of Element Six type CTM302 PCD material. In some embodiments, the wear elements 928A and 928B may have radii of about 3.0 millimeters and an average surface roughness less than 0.10 microns. The wear elements 928A and 928B may be coated with a vacuum-compatible solid lubricant prior to assembly. The wear elements 928A and 928B run in or spin briefly in their locating depressions in the wear elements 930A and 930B prior to assembly.
The wear elements 930A and 930B are discs. The wear elements 930A and 930B may be comprised of Element Six type CTM302 PCD material. In some embodiments, the wear elements 930A and 930B may have a diameter of about 0.625 inches and a thickness of about 2 millimeters. One face of each of the wear elements 930A and 930B may be planar and polished to an average surface roughness of less than 0.10 microns. An opposite face of each of the wear elements 930A and 930B is similarly planar and polished to an average surface roughness of less than 0.10 microns.
A spherical depression is defined in the wear elements 930A and 930B. In some embodiments, the depth of the depression may be about 2.00 millimeters and the radius of the depression may be not less than about 3.00 millimeters. Each depression is centered on the face in which it is formed and may have an average surface roughness of less than about 0.10 microns.
The wear elements 930A and 930B are attached to their respective locations on the inner surface of enclosure 904 by adhesive bonding. For example, the wear elements 930A and 930B may be adhered to the enclosure 904 using J-B Weld® #8265-S adhesive or a similar product. Prior to assembly, each spherical depression may be coated with a vacuum-compatible solid lubricant. The wear elements 930A and 930B may be subjected to a brief run-in.
In some embodiments, the axial location and thrust bearing functionality of the flywheel assembly 900 may be obtained with other wear-resistant materials such as silicon carbide, tungsten carbide, synthetic diamond, other appropriate materials, or some combination thereof. As well, some embodiments include providing the axial location and thrust bearing functionality through use of other types of bearings, such as conical (tapered) roller bearings and thrust bearings comprised of planar surfaces separated by rolling elements.
Moreover, some embodiments use of interface or attachment materials that provide compliance and/or energy damping. The interface or attachment materials may be advantageous for a specific design with respect to rotor dynamics, stability, vibration control, or wear lifer. For example, wear elements 930A and 930B may be fixed to enclosure 904 using pads of compliant material placed between the wear elements and the enclosure surface. The pads of compliant material may provide compliance and/or energy dissipation. An example of using a compliant material is interposition of a layer of silicon rubber having a thickness of about 1/16 inches and a Durometer hardness of 50 A between each of the wear elements 930A and 930B and their corresponding locations on enclosure 904. A suitable elastomer material is silicone rubber. A suitable adhesive for bonding silicon rubber between the enclosure 904 and the wear elements 930A or 930B may include an adhesive tape (e.g., 3M™ Adhesive Transfer Tape type 7955MP).
The flywheel assembly 1000 is similar to the flywheel assembly 900 described with reference to
The flywheel assembly 1000 includes roller element bearings 1002A and 1002B. The roller element bearings 1002A and 1002B provide mechanical support and spin isolation for the flywheel rotor 902. The roller element bearings 1002A and 1002B are positioned between the shaft 920 and a rotor bearing interface 1004. In some embodiments, the roller element bearings 1002A and 1002B may be attached to the shaft 920 or the rotor bearing interface 1004.
The rotor bearing interface 1004 provides a mechanical interface between the outer surfaces of roller element bearings 1002A and 1002B and the flywheel rotor 902. The rotor bearing interface 1004 may be comprised of materials such as elastomers that provide compliance and/or damping.
The flywheel assembly 1000 also includes capture components 1006A and 1006B. The capture components 1006A and 1006B provide a mechanical interface between shaft 920 and locations on the inner surface of the enclosure 904. The capture components 1006A and 1006B may be comprised of materials such as elastomers that provide compliance and/or damping.
The flywheel assembly 1100 of
The flywheel assembly 1100 is a per-panel storage device that includes an enclosure 1103. The enclosure 1103 is similar to the enclosure 904 described above. For example, the enclosure 1103 is evacuated such that a vacuum or partial vacuum is formed within the enclosure 1103. The vacuum reduces resistance to rotation of a flywheel rotor 1105. The flywheel rotor 1105 is similar to the flywheel rotor 902 in material construction. The flywheel rotor 1105 is placed in the enclosure 1103. During operation, the flywheel rotor 1105 is positioned by electromagnetic actuators. Positioning the flywheel rotor 1105 reduces or eliminates wear incident to mechanical bearings.
Referring to
Referring to
The ferromagnetic elements 1102A and 1102B may be adherently bonded to the depicted upper and lower planar surfaces, respectively, of the flywheel rotor 1105 after winding and finishing operations. Additionally or alternatively, the ferromagnetic elements 1102A and 1102B may be incorporated within the body of the flywheel rotor 1105 during winding operations. In embodiments in which the ferromagnetic elements 1102A and 1102B are incorporated within the body of the flywheel rotor 1105 they are embedded within the flywheel rotor 1105.
The flywheel rotor 1105 may also include a ferromagnetic element 1104. The ferromagnetic element 1104 may be incorporated within the flywheel rotor 1105 during its fabrication. The ferromagnetic element 1104 may be comprised of a strip of ferromagnetic material. For example, in the depicted flywheel assembly 1100, the ferromagnetic element 1104 includes a circumferential strip of 1018 alloy steel. In this and other embodiments, the ferromagnetic element 1104 may have a thickness of about 0.010 inches, a width (Z-axial extent) of about 0.5 inches, and an average radius of about 4.50 inches. The ferromagnetic element 1104 may be incorporated within the rotor structure during manufacture, which may result in the ferromagnetic element 1104 being embedded within the body of the flywheel rotor 1105. Additionally or alternatively, the ferromagnetic element 1104 may be adherently bonded to an outer cylindrical surface of the flywheel rotor 1105 after rotor winding and finishing operations.
As best depicted in
Referring back to
The flywheel assembly 1100 includes the ferromagnetic position sensors 1106A and 1106B that are positioned opposite the ferromagnetic element 1102A. For example, a first ferromagnetic position sensor 1106A is positioned on an axis that is parallel to the x-axis and a second ferromagnetic position sensor 1106B is positioned on an axis that is parallel to the y-axis. Each of the ferromagnetic position sensors 1106A and 1106B provides data for computation of distance between it and the ferromagnetic element 1102A. Because the ferromagnetic position sensors 1106A and 1106B are disposed at 90° angles about a circumference, data from the sensors 1106A and 1106B yields data about a position of the flywheel rotor 1105 relative to the an axis parallel the z-axis.
The flywheel rotor 1105 includes a levitator susceptor 1116D. The levitator susceptor 1116D may be incorporated in the flywheel rotor 1105. The flywheel assembly 1100 also includes a ferromagnetic sensor 1110. The ferromagnetic sensor 1110 is positioned in the center of the enclosure 1103 and opposite the levitator susceptor 1116D. The ferromagnetic sensor 1110 measures a distance between itself and the levitator susceptor 1116D and communicates data representative of the distance.
Combined data from the ferromagnetic sensors 1110 and 1106A may be processed to determine tilt of the flywheel rotor 1105 about the y-axis with respect to gravitational vector 1108. Combined data from the ferromagnetic sensors 1110 and 1106B similarly yield tilt of the flywheel rotor 1105 about the x-axis. Combined data from the ferromagnetic sensors 1110, 1106B, and 1106A allow computation of the flywheel rotor 1105 position on an axis parallel to the z-axis.
The flywheel assembly 1100 includes sensors 1112A and 1112B. The sensors 1112A and 1112B are fixed to the outer circumferential surface of enclosure 1103. The sensors 1112A and 1112B measure distance from each sensor to a ferromagnetic element 1104. Data from the sensors 1112A and 1112B may be processed to determine radial positions of the flywheel rotor 1105.
In the depicted embodiment position sensors are used with magnetic sensors and ferrite targets. In some embodiments, distances between the flywheel rotor 1105 and the enclosure 1103 may be measured using other types of sensors such as optical or capacitive sensors.
The levitator assembly 1200 includes a levitator pole 1116A. The levitator pole 1116A may be fabricated from 1018 alloy steel or a material having similar mechanical and ferromagnetic properties. In the depicted embodiment, the levitator pole 1116A has a first inner diameter 1202 of about 1.0 inch, a second inner diameter 1204 of about 2.50 inches, and an overall outer diameter 1206 of about 2.75 inches. The levitator pole 1116A has a first thickness 1210 (in the z-direction) of about 0.1875 inches and a second thickness 1208 of about 0.4375 inches.
Fixed to the levitator pole 1116A is a levitator magnet 1116B. The levitator magnet 1116B is a rare earth ring magnet. The magnetic properties of the levitator magnet 1116B may be those of rare earth magnet grade 42. In the depicted embodiment, the levitator magnet 1116B has its magnetization direction oriented axially as depicted by the arrow shown on the levitator magnet 1116B. The arrowhead indicating magnetic North. By reason of its high relative magnetic permeability, the levitator pole 1116A provides a confining path for magnetic flux provided by the levitator magnet 1116B.
The levitator assembly 1200 includes a levitator control coil 1116C. The levitator control coil 1116C may include about 85 turns of #26 insulated copper magnet wire helically wound in some embodiments. The levitator control coil 1116C is positioned in the annulus formed between the outer diameter of the levitator magnet 1116B and the opposed cylindrical surface of the levitator pole 1116A. The levitator control coil 1116C may be fixed in place using an epoxy adhesive. The levitator control coil 1116C is connected to and may be controllably energized by levitator control electronics 1116E. Energizing the levitator control coil 1116C may include an electrical current of about 15 Amperes in magnitude and either polarity being initiated by the levitator control electronics 1116E which may flow through the levitator control coil 1116C.
The levitator susceptor 1116D is a disc made from a ferromagnetic material. For example, the levitator susceptor 1116D may be comprised of steel alloy 1018 or a dispersion of ferromagnetic particles within a matrix material such as a plastic or other substantially non-ferromagnetic material. The levitator susceptor 1116D is subject to an attractive force generated when positioned in proximity to a magnetic field. For example, a controllable field presented by the levitator pole 1116A, the levitator magnet 1116B, and levitator control coil 1116C as controllably energized by the levitator control electronics 1116E may subject the levitator susceptor 1116D to an attractive force.
In the depicted embodiment, the levitator susceptor 1116D has an outer diameter of about 3.0 inches and a thickness of about 0.25 inches. As mentioned above, the ferromagnetic sensor 1110 is a position sensor that measures distances between itself and the levitator susceptor 1116D. Data representative of the distances are supplied to the levitator control electronics 1116E.
The electromagnetic field caused by passage of electric current through levitator control coil 1116C controllably varies magnetic flux within the levitator pole 1116A. The effect of the magnetic flux controllably changes the attractive force exerted on the levitator susceptor 1116D. The attractive force can be increased or decreased depending on the magnitude and polarity of electric current driven through the levitator control coil 1116C. Thus, the operation of the levitator assembly 1200 positions or re-positions the flywheel rotor 1105 relative to the enclosure 1103. Positioning or re-positioning the flywheel rotor 1105 relative to the enclosure 1103 assures no mechanical contact occurs between the flywheel rotor 1105 and the enclosure 1103 during operation.
On energizing the levitator assembly 1200, the levitator control electronics 1116E with rotor axial position data from the ferromagnetic sensor 1110 energizes the levitator control coil 1116C to set the magnitude of attractive force exerted on the levitation susceptor 1116D. The levitator control coil 1116C lifts flywheel rotor 1105 of
In some embodiments, the levitator control electronics 1116E are programmed to position the flywheel rotor 1105 on an axis parallel to the z-axis such that the attractive force developed by levitator magnet 1116B as resolved on levitator susceptor 1116D is essentially equal to the force exerted by gravity on the flywheel rotor 1105.
Referring back to
Referring to
The electromagnetic actuator elements 1118A-1118D and 1114A-1114D may include a coil having about 50 turns of #26 magnet wire. The average diameters of the coils may be about 0.5 inches. The coils may be fixed opposite to their respective proximate ferromagnetic elements at angular positions approximately equidistant between the sensors 1106A and 1106B. The electromagnetic actuator elements 1118A-1118D and 1114A-1114D are controllably energized by rotor position control computation (not depicted), which may include signal conditioning electronics, computation, and power drive electronics. The power drive electronics may be connected to the electromagnetic actuator elements 1118A-1118D and 1114A-1114D.
In some embodiments, different means of actuator construction, such as printed conductors on circuit boards, may be employed without departing from the scope of this disclosure. Moreover, different types of actuators, such as those which operate through generation of Lorentz forces rather than through attraction of ferromagnetic materials, are contemplated in this disclosure.
With combined reference to
The flywheel assembly 1100 further includes the arrays of magnets 910A and 910B and the electromagnetic coil assemblies 912A and 912B described with reference to
During spin operations, position control electronics maintain the position of flywheel rotor 1105 within a defined spatial envelope. Positioning or re-positioning the flywheel rotor 1105 occurs in response to the flywheel rotor 1105 exiting the defined envelope or in response to a prediction that the flywheel rotor 1105 is going to exit the defined envelop. The data representative of the position of the flywheel rotor 1105 is used in computations to make determinations regarding a current position of the flywheel rotor 1105. The flywheel rotor 1105 is otherwise not subjected to correction.
During operation, the flywheel rotor 1105 is first positioned for spin by moving it away from contact with enclosure 1103. The arrays of magnets 910A and 910B and the electromagnetic coil assemblies 912A and 912B are then energized to spin the flywheel rotor 1105. In the depicted embodiment, the flywheel rotor 1105 may be accelerated to a maximum of about 110,000 RPM by electricity produced by a PV device string (e.g., 102) at which point the flywheel assembly 1100 holds approximately 100 Watt-hours of kinetic energy. However, some embodiments may limit operation to about 73% of this maximum at which the flywheel assembly may hold about 80 Watt-hours. The stored energy may be retrieved as described elsewhere in this disclosure to maintain electrical output of a PV panel.
In some embodiments, the flywheel assembly 1100 may be configured as described in U.S. patent application Ser. Nos. 13/280,232 and 13/280,314 filed Oct. 24, 2011, the disclosures of which are incorporated herein by reference in their entireties.
Some embodiments described in this disclosure are related to a PV panel. The PV panel is configured as a modular electrical source with per-panel energy storage. Energy storage is added to a PV electrical source, such as those assemblies of PV devices commonly known as solar panels. Energy storage is provided on a per-panel basis, i.e., energy produced by a single PV panel is stored within a storage device located on that panel. When electrical output of the PV panel is reduced, the storage device delivers energy stored thereon to the panel's electrical load. Such per-panel energy storage continues a panel's nominal electrical output if insolation of the PV panel is interrupted or diminished, thereby eliminating or reducing rapid output variations and electrical distribution grid instabilities associated with solar photovoltaic electrical sources.
This application claims the benefit of and priority to U.S. Provisional Application No. 62/040,180 filed Aug. 21, 2014, which is incorporated herein by reference in its entirety.
Number | Date | Country | |
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62040180 | Aug 2014 | US |