초록 ▼

The present inventions relate to power systems (for example, fuel cell power systems) and architectures having an integration plane to incorporate various technology modules therein including, for example, one or more fuel cell stacks, fuel storage containers/tanks (for example, hydrogen, methanol a

The present inventions relate to power systems (for example, fuel cell power systems) and architectures having an integration plane to incorporate various technology modules therein including, for example, one or more fuel cell stacks, fuel storage containers/tanks (for example, hydrogen, methanol and/or hydrogen containing compounds or substances from which hydrogen can be extracted on demand (e.g., a hydride)), power unit having a power management unit to provide a conditioned and/or regulated electrical power using electrical power provided by a fuel cell, fuel cartridge having one or more fuel storage containers/tanks and electrical circuitry to monitor and/or store one or more parameters of the fuel storage container(s)/tank(s), supercapacitors, batteries, and/or electrical or electronic devices such as mobile communications (for example, phones and/or modems), data processor circuitry, and/or monitoring or surveillance device (for example, a imaging sensing device (for example, camera) and/or audio sensing device).

대표청구항 ▼

What is claimed is: 1. A fuel cell system comprising: an integration plane adapted to receive a plurality of differing types of technology modules, comprising, a bidirectional fluid bus; an electrical bus; a plurality of module bays each adapted to receive a said technology module, each said module

What is claimed is: 1. A fuel cell system comprising: an integration plane adapted to receive a plurality of differing types of technology modules, comprising, a bidirectional fluid bus; an electrical bus; a plurality of module bays each adapted to receive a said technology module, each said module bay comprising: a bidirectional fluid interface coupled to the bidirectional fluid bus; an electrical interface coupled to the electrical bus; and wherein: the bidirectional fluid interface of each module bay of the plurality of module bays has the same bidirectional interface, and the electrical interface of each module bay of the plurality of module bays has the same electrical interface; a hydrogen fuel cell stack, coupled to the bidirectional fluid bus of the integration plane, to generate unconditioned electrical power using hydrogen; a power management unit, electrically coupled to the hydrogen fuel cell stack, to generate conditioned electrical power using the unconditioned electrical power generated by the hydrogen fuel cell stack and to output the conditioned electrical power to a power management interface; and circuitry electrically coupled to at least one of (i) the integration plane, (ii) the hydrogen fuel cell stack and (iii) the power management unit, to monitor and/or control at least one of (i) the integration plane, (ii) the hydrogen fuel cell stack, and (iii) the power management unit. 2. The fuel cell system of claim 1 wherein the circuitry is electrically coupled to an external connector disposed on the integration plane. 3. The fuel cell system of claim 1 further comprising a first said technology module disposed in a module bay of the integration plane, wherein the first technology module includes the circuitry. 4. The fuel cell system of claim 1 wherein the circuitry is resident on the integration plane. 5. The fuel cell system of claim 4 further comprising a user interface having a visual display to provide information which is representative of an operating parameter of at least one of (i) the integration plane, (ii) the hydrogen fuel cell stack and (iii) the power management unit. 6. The fuel cell system of claim 1 further comprising first and second said technology modules, each said technology module comprising a vessel containing hydrogen, wherein: the first technology module is disposed in a first module bay of the plurality of module bays of the integration plane and coupled to the bidirectional fluid bus via the bidirectional fluid interface of the first module bay, to provide hydrogen to the fuel cell stack; and the second technology module is disposed in a second module bay of the plurality of module bays of the integration plane and coupled to the bidirectional fluid bus via the bidirectional fluid interface of the second module bay, to provide hydrogen to the fuel cell stack. 7. The fuel cell system of claim 6 wherein the first and second technology modules each further comprise a memory to store information which is representative of an amount of hydrogen in the associated vessel of the associated module and wherein the memory is coupled to the electrical bus of the integration plane via the electrical interface of the associated module bay. 8. The fuel cell system of claim 7 further comprising a user interface having a visual display to provide information which is representative of the amount of hydrogen in the vessel of each of the first and the second technology modules. 9. The fuel cell system of claim 7 further comprising a user interface having a visual display to provide information which is representative of the total amount of hydrogen in the vessels of the first and second technology modules. 10. The fuel cell system of claim 7 wherein: the hydrogen fuel cell stack is fixed to the integration plane and outputs the unconditioned electrical power on a power management bus; and the power management unit is fixed to the integration plane and coupled to the power management bus to receive the unconditioned electrical power. 11. The fuel cell system of claim 1 wherein the hydrogen fuel cell stack comprises a first said technology module which is disposed in a first module bay of the integration plane and to the bidirectional fluid bus of the integration plane via the bidirectional fluid interface of the first module bay. 12. The fuel cell system of claim 1 wherein the hydrogen fuel cell stack is any one of: (i) coupled to the bidirectional fluid bus of the integration plane via an external connector disposed on the integration, plane or (ii) fixed on the integration plane. 13. The fuel cell system of claim 1 wherein: the hydrogen fuel cell stack outputs the unconditioned electrical power on a power management bus; and the power management unit is a first said technology module which is disposed in a first module bay of the integration plane and coupled to the power management bus of the integration plane to receive the unconditioned electrical power. 14. The fuel cell system of claim 1 wherein: the hydrogen fuel cell stack outputs the unconditioned electrical power on a power management bus; and the power management unit is fixed to the integration plane and coupled to the power management bus to receive the unconditioned electrical power. 15. The fuel cell system of claim 1 further comprising a power management bus coupled between the hydrogen fuel cell stack and the power management unit, wherein: the hydrogen fuel cell stack is fixed to the integration plane and outputs the unconditioned electrical power on the power management bus; and power management unit is fixed to the integration plane and coupled to the power management bus to receive the unconditioned electrical power. 16. The fuel cell system of claim 1 wherein the power management unit comprises a DC-DC converter and/or a DC-AC inverter to generate the conditioned electrical power using the unconditioned electrical power. 17. The fuel cell system of claim 1 further comprising first said and second said technology modules, each technology module comprising a vessel containing hydrogen and a memory to store information which is representative of the amount of hydrogen which is in the associated vessel, wherein: the first technology module is disposed in a first module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the first module bay to provide hydrogen to the fuel cell stack; and he electrical bus of the integration plane via the electrical interface of the first module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the first technology module; the second technology module is disposed in a second module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the second module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the second module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the second technology module; and a battery or an ultra-capacitor, coupled to the power management unit, to provide electrical power to the power management unit. 18. The fuel cell system of claim 17 wherein the battery or ultra-capacitor is disposed in a third technology module which is attached to a third module bay of the integration plane. 19. A fuel cell system comprising: an integration plane adapted to receive a plurality of differing types of technology modules, comprising, a bidirectional fluid bus; an electrical bus; a plurality of module bays each adapted to receive a said technology module, each said module bay comprising: a bidirectional fluid interface coupled to the bidirectional fluid bus; an electrical interface coupled to the electrical bus; and wherein: the bidirectional fluid interface of each module bay of the plurality of module bays has the same bidirectional fluid interface, and the electrical interface of each module bay of the plurality of module bays has the same electrical interface; a hydrogen fuel cell stack, coupled to the bidirectional fluid bus of the integration plane, to generate unconditioned electrical power using hydrogen and output the unconditioned electrical power on a power management bus; and a power management unit, electrically coupled to the hydrogen fuel cell stack via the power management bus, to generate conditioned electrical power using the unconditioned electrical power and to output the conditioned electrical power to a power management interface; a user interface; and circuitry electrically coupled to at least one of (i) the hydrogen fuel cell stack, (ii) the power management unit, and (iii) at least one module bay of the plurality of module bays, to monitor and/or control at least one of (i) the hydrogen fuel cell stack, (ii) the power management unit and (iv) a said technology module disposed in the at least one module bay. 20. The fuel cell system of claim 19 wherein the circuitry is electrically coupled to an external connector disposed on the integration plane. 21. The fuel cell system of claim 19 further comprising a first said technology module disposed in a module bay of the integration plane, wherein the first technology module includes the circuitry. 22. The fuel cell system of claim 19 wherein the user interface is fixed to/on the integration plane. 23. The fuel cell system of claim 19 wherein the user interface comprises a visual display to provide information which is representative of an operating parameter of at least one of the integration plane, the hydrogen fuel cell stack and the power management unit. 24. The fuel cell system of claim 19 wherein: the hydrogen fuel cell stack is a first said technology module which is disposed in a first module bay of the integration plane; and the first module bay comprises an interface that couples the hydrogen fuel cell stack to the power management bus such that the hydrogen fuel cell stack outputs the unconditioned electrical power on the power management bus. 25. The fuel cell system of claim 19 wherein any one of: the power management bus is fixed to/on the integration plane; and the hydrogen fuel cell stack is fixed to/on the integration plane. 26. The fuel cell system of claim 19 wherein: the power management bus is fixed to/on the integration plane; the power management unit is a first technology module which is disposed in a first module bay of the integration plane; and the first module bay comprises an interface that couples the power management unit to the power management bus such that the power management unit receives the unconditioned electrical power from the hydrogen fuel cell stack. 27. The fuel cell system of claim 19 further comprising first and second said technology modules, each technology module comprising a vessel containing hydrogen and a memory to store information which is representative of the amount of hydrogen which is in the associated vessel, wherein: the first technology module is disposed in a first module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the first module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the first module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the first technology module; the second technology module is disposed in a second module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the second module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the second module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the second technology module. 28. The fuel cell system of claim 27 wherein any one of: hydrogen fuel cell stack is fixed to/on the integration plane; and power management unit is fixed to/on the integration plane. 29. The fuel cell system of claim 27 further comprising a user interface having a visual display to provide information which is representative of the amount of hydrogen in the vessel of each of the first and the second technology modules. 30. The fuel cell system of claim 27 further comprising a user interface having a visual display to provide information, which is representative of the total amount of hydrogen in the vessels of the first and second technology modules. 31. The fuel cell system of claim 19 wherein the power management bus is coupled between the hydrogen fuel cell stack and the power management unit. 32. The fuel cell system of claim 19 wherein the power management unit comprises a DC-DC converter and/or a DC-AC inverter to generate the conditioned electrical power using the unconditioned electrical power. 33. The fuel cell system of claim 19 further comprising first and second technology modules, each technology module comprising a vessel containing hydrogen and a memory to store information which is representative of the amount of hydrogen which is in the associated vessel, wherein: the first technology module is disposed in a first module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the first module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the first module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the first technology module; the second technology module is disposed in a second module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the second module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the second module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the second technology module; and a battery or an ultra-capacitor, coupled to the power management bus, to provide electrical power on the power management bus. 34. The fuel cell system of claim 33 wherein the battery or ultra-capacitor is in a third technology module that is disposed in a third module bay of the integration plane. 35. A fuel cell system comprising: an integration plane adapted to receive a plurality of differing types of technology modules, comprising, a bidirectional fluid bus; an electrical bus; a plurality of module bays each adapted to receive a said technology module, each said module bay comprising: a bidirectional fluid interface coupled to the bidirectional fluid bus; an electrical interface coupled to the electrical bus; and wherein (i) the bidirectional fluid interface of each module bay of the plurality of module bays has the same bidirectional fluid interface and (ii) the electrical interface of each module bay of the plurality of module bays has the same electrical interface; first and second said technology modules, each technology module comprising a vessel containing hydrogen and a memory to store information which is representative of the amount of hydrogen which is in the associated vessel, wherein: the first technology module is disposed in a first module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the first module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the first module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the first technology module; the second technology module is disposed in a second module bay of the plurality of module bays of the integration plane and coupled to: the bidirectional fluid bus via the bidirectional fluid interface of the second module bay to provide hydrogen to the fuel cell stack; and the electrical bus of the integration plane via the electrical interface of the second module bay of the integration plane to receive information which is representative of the amount of hydrogen which is in the vessel of the second technology module; a hydrogen fuel cell stack, coupled to the bidirectional fluid bus of the integration plane, to generate unconditioned electrical power using hydrogen and output the unconditioned electrical power on a power management bus; a power management unit, having a DC-DC converter and/or a DC-AC inverter, to generate the conditioned electrical power using the unconditioned electrical power, electrically coupled to the hydrogen fuel cell stack via the power management bus, to generate conditioned electrical power using the unconditioned electrical power and to output the conditioned electrical power to a power interface; and circuitry electrically coupled to at least one of (i) the hydrogen fuel cell stack, (ii) the power management unit, and (iii) at least one module bay of the plurality of module bays to monitor and/or control at least one of (i) the hydrogen fuel cell stack, (ii) the power management unit and (iii) a said technology module disposed in the at least one module bay.