Abstract: A system for a blended wing body aircraft with a combustion engine is illustrated. The aircraft comprises a blended wing body, at least a fuel source located within the blended wing body and configured to store a fuel, wherein the fuel includes liquid hydrogen, and at least a propulsor configured to propel the blended wing body aircraft. The at least a propulsor comprises a combustion engine configured to burn the fuel from the fuel source and produce mechanical work to power the at least a propulsor.

Abstract: A system for a blended wing body aircraft with a combustion engine is illustrated. The aircraft comprises a blended wing body, at least a fuel source located within the blended wing body and configured to store a fuel, wherein the fuel includes liquid hydrogen, and at least a propulsor configured to propel the blended wing body aircraft. The at least a propulsor comprises a combustion engine configured to burn the fuel from the fuel source and produce mechanical work to power the at least a propulsor.

Abstract: Certain aspects relate to a blended wing body aircraft with a fuel cell and methods of use. An exemplary aircraft includes a blended wing body, at least a propulsor mechanically affixed to the aircraft and configured to propel the aircraft, at least a first fuel store configured to store a first fuel, and at least a fuel cell configured to combine the first fuel with oxygen to produce electricity.

Abstract: In an aspect, an aircraft fueling apparatus is disclosed. The apparatus includes at least a container comprising a fuel tank configured to store liquified gas fuel. The apparatus may also include a translocation device configured to carry the at least a container. An orientation guidance track may also be included in the apparatus. The orientation guidance track may be configured to direct a movement of the translocation device to a first position.

Abstract: In an aspect, an aircraft fueling apparatus is disclosed. The apparatus includes at least a container comprising a fuel tank configured to store liquified gas fuel. The apparatus may also include a translocation device configured to carry the at least a container. An orientation guidance track may also be included in the apparatus. The orientation guidance track may be configured to direct a movement of the translocation device to a first position.

Abstract: A system for a blended wing body aircraft with a combustion engine is illustrated. The aircraft comprises a blended wing body, at least a fuel source located within the blended wing body and configured to store a fuel, wherein the fuel includes liquid hydrogen, and at least a propulsor configured to propel the blended wing body aircraft. The at least a propulsor comprises a combustion engine configured to burn the fuel from the fuel source and produce mechanical work to power the at least a propulsor.

Abstract: A power control module and a method to create the power control module is provided. The power control module includes a plurality of transformers, wherein each transformer of the plurality of transformers includes a stack of ferrite cores comprising a plurality of ferrite cores and a continuous winding. The continuous winding has a plurality of turns through each ferrite core of the plurality of ferrite cores. The plurality of ferrite cores are oriented such that the plurality of ferrite cores are stacked together with legs of the plurality of ferrite cores oriented in opposite directions, and wherein the continuous winding comprises a folded section that extends between the plurality of ferrite cores of the stack of ferrite.

Abstract: Certain aspects relate to a blended wing body aircraft with a fuel cell and methods of use. An exemplary aircraft includes a blended wing body, at least a propulsor mechanically affixed to the aircraft and configured to propel the aircraft, at least a first fuel store configured to store a first fuel, and at least a fuel cell configured to combine the first fuel with oxygen to produce electricity.

Abstract: A power control module and a method to create the power control module is provided. The power control module includes a plurality of transformers, wherein each transformer of the plurality of transformers includes a stack of ferrite cores comprising a plurality of ferrite cores and a continuous winding. The continuous winding has a plurality of turns through each ferrite core of the plurality of ferrite cores. The plurality of ferrite cores are oriented such that the plurality of ferrite cores are stacked together with legs of the plurality of ferrite cores oriented in opposite directions, and wherein the continuous winding comprises a folded section that extends between the plurality of ferrite cores of the stack of ferrite.

Abstract: In an example, a system for increasing solid oxide fuel cell (SOFC) efficiency is described. The system comprises a series of SOFC stacks, a fuel flow path through the series, and an air flow path through the series. In the fuel flow path between two sequential SOFC stacks in the series, fuel exhaust from a first SOFC stack of the two sequential SOFC stacks is input into a second SOFC stack of the two sequential SOFC stacks. In the air flow path between the two sequential SOFC stacks, air exhaust from the first SOFC stack is input into the second SOFC stack. Further, between the two sequential SOFC stacks, (i) the fuel flow path comprises a fuel inlet positioned for injecting fuel into the fuel flow path and/or (ii) the air flow path comprises an air inlet positioned for injecting air into the air flow path.

Abstract: Example methods and systems described herein include periodically adjusting load applied to a power generating device according to a testing cycle, detecting a peak power point of the power generating device and an associated load that results in the peak power point, adjusting the load applied to the power generating device to match the associated load that results in the peak power point, and based on the adjusted load drawing power outside of a threshold amount of the peak power point, (i) calculating a correction factor to apply to a reference voltage of the power generating device and (ii) adjusting a frequency of the testing cycle.

Abstract: A rapid start power unit and a method of operating a rapid start power unit are disclosed. A fuel cell converts combustible fuel into electrical power during a normal operational period after an initial start-up period when little to no electrical energy is produced. One combustion chamber receives unspent fuel emitted by the fuel cell and combusts the unspent fuel to generate a first heated gas stream. Another combustion chamber receives combustible fuel and burns the combustible fuel to generate a second heated gas stream during the initial start-up period. A turbine receives and is driven by the first and second heated gas streams to drive a drive shaft. A generator coupled to the drive shaft generates electrical power during the initial start-up period and supplemental power during the normal operational period. In an alternative embodiment, a two-stage combustion chamber is used instead of two serially-arranged separate combustion chambers.

Abstract: A rapid start power unit and a method of operating a rapid start power unit are disclosed. A fuel cell converts combustible fuel into electrical power during a normal operational period after an initial start-up period when little to no electrical energy is produced. One combustion chamber receives unspent fuel emitted by the fuel cell and combusts the unspent fuel to generate a first heated gas stream. Another combustion chamber receives combustible fuel and burns the combustible fuel to generate a second heated gas stream during the initial start-up period. A turbine receives and is driven by the first and second heated gas streams to drive a drive shaft. A generator coupled to the drive shaft generates electrical power during the initial start-up period and supplemental power during the normal operational period. In an alternative embodiment, a two-stage combustion chamber is used instead of two serially-arranged separate combustion chambers.

Abstract: A method for assembling an electrochemical cell stack may include arranging a plurality of electrochemical cells into an electrochemical cell stack, the electrochemical cell stack including at least a first substack and a second substack; connecting the first substack and second substack such that reactant fluid flows in series from the first substack to the second substack; and coupling the first substack to a first electrical control device such that the first electrical control device selectively electrically reconfigures the first substack to operate in series and in parallel with the second substack.

Abstract: A method for assembling an electrochemical cell stack may include arranging a plurality of electrochemical cells into an electrochemical cell stack, the electrochemical cell stack including at least a first substack and a second substack; connecting the first substack and second substack such that reactant fluid flows in series from the first substack to the second substack; and coupling the first substack to a first electrical control device such that the first electrical control device selectively electrically reconfigures the first substack to operate in series and in parallel with the second substack.

Abstract: An electrochemical cell system including a plurality of electrochemical cells arranged in an electrochemical cell stack, the stack including a plurality of substacks configured such that fluid flows in series from substack to substack, a first electrical control device coupled to a first substack and a second electrical control device coupled to a second substack, wherein the first electrical control device is controllable independently of the second control device to selectively electrically configure the first and second substacks.

Abstract: Apparatus, systems, and methods provide for the management of a high temperature electrolysis process. According to embodiments described herein, a fuel cell electrolyzer stack is utilized in an electrolysis process. One implementation includes the use of a solid oxide electrolyzer. Input voltage is cycled around a thermal neutral voltage such that the fuel cell electrolyzer stack cycles between operation in an exothermic mode and an endothermic mode. The waste heat generated by operation in the exothermic mode is used to support the endothermic operation. By cycling between operation modes, the temperature of the fuel cell electrolyzer stack may be controlled without the use of a cooling loop or recirculated reactant flow, and the efficiency of the electrolysis process is maximized.

Abstract: An aerospace platform includes a structure having a cavity and a light-transmissive portion that exposes the cavity to sunlight. The aerospace platform further includes a fluid heating system. The fluid heating system includes a fluid-carrying, thermally absorptive structure within the cavity, and a solar collector for collecting light transmitted through the light-transmissive portion and focusing the collected light onto the absorptive structure. The thermally absorptive structure has a high surface absorptivity that retains thermal energy when exposed to solar irradiance and heats fluid contained therein.

Abstract: Methods and systems provide for the creation of power, water, and heat utilizing a fuel cell. According to embodiments described herein, fuel is provided to a fuel cell for the creation of power and a fuel byproduct. The fuel byproduct is routed to a byproduct separation phase of a power and water generation system, where water is separated from the fuel byproduct. The remaining mixture is reacted in a burner phase of the system to create additional heat that may be converted to mechanical energy and/or utilized with other processes within the system or outside of the system. According to other aspects, the separated water may be utilized within a biofuel production subsystem for the creation of biofuel to be used by the fuel cell.

Abstract: An electrochemical cell system including a plurality of electrochemical cells arranged in an electrochemical cell stack, the stack including a plurality of substacks configured such that fluid flows in series from substack to substack, a first electrical control device coupled to a first substack and a second electrical control device coupled to a second substack, wherein the first electrical control device is controllable independently of the second control device to selectively electrically configure the first and second substacks.