Abstract: Some implementations of the described methods relate to a process for frying coffee beans (and/or another food product) in a fry medium (such as cooking oil) and then centrifuging the coffee beans (and/or other food product) to remove a significant portion of the fry medium. Although the frying and centrifugation can occur in separate devices, in some cases, the described systems comprise a device that acts as both a fryer and a centrifuge. Indeed, in some cases, after the coffee beans (or other food product) has been fry roasted in a perforated container (e.g., a basket), the fry medium is drained from the container, and container is spun. In some cases, liquid nitrogen is also applied to the beans (or other food product), before and/or after being fry roasted. Other implementations are described.

Abstract: The present invention provides apparatus, devices, methods, and configurations to carry and assist the loading and unloading of heavy loads or loads having irregular or elongated shapes such as ladders, lumber, personal recreation equipment including but not limited to surfboards, paddleboards, canoes, kayaks, skis, snowboards, bicycles, and other items to reduce effort and impediments to loading a vehicle's roof rack and to allow full utilization of the vehicle's receiver. The device can pivot into either the loading and unloading position or the transport position when a pin is removed from the device at a pivot point in its vertical member. The device is mounted to a hitch receiver extension which is secured to the vehicle's hitch receiver. The hitch receiver extension allows the vehicle to transport another apparatus such as a trailer or bike rack mounted to the hitch receiver extension.

Abstract: Some implementations of the described methods relate to a process for frying coffee beans (and/or another food product) in a fry medium (such as cooking oil) and then centrifuging the coffee beans (and/or other food product) to remove a significant portion of the fry medium. Although the frying and centrifugation can occur in separate devices, in some cases, the described systems comprise a device that acts as both a fryer and a centrifuge. Indeed, in some cases, after the coffee beans (or other food product) has been fry roasted in a perforated container (e.g., a basket), the fry medium is drained from the container, and container is spun. In some cases, liquid nitrogen is also applied to the beans (or other food product), before and/or after being fry roasted. Other implementations are described.

Abstract: A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data to, and to receive flight management data from, the FMS component to which it is coupled. The platform interface manager can be adapted to provide each FMS component access to the avionics system, such that an aircraft operator can control each FMS component via the FMS.

Abstract: A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data to, and to receive flight management data from, the FMS component to which it is coupled. The platform interface manager can be adapted to provide each FMS component access to the avionics system, such that an aircraft operator can control each FMS component via the FMS.

Abstract: A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data to, and to receive flight management data from, the FMS component to which it is coupled. The platform interface manager can be adapted to provide each FMS component access to the avionics system, such that an aircraft operator can control each FMS component via the FMS.

Abstract: Systems and methods for reducing problems and disadvantages associated with traditional approaches to cooling information handling resources are provided. A method for cooling information handling resources, may include conveying a flowing fluid proximate to one or more information handling resources such that the flowing fluid is thermally coupled to the one or more information handling resources and heat generated by the one or more information handling resources is transferred to the flowing fluid. The method may also include conveying the flowing fluid to a cooling unit such that heat is transferred from the flowing fluid.

Abstract: A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data to, and to receive flight management data from, the FMS component to which it is coupled. The platform interface manager can be adapted to provide each FMS component access to the avionics system, such that an aircraft operator can control each FMS component via the FMS.

Abstract: Flexible seals for process control valves are disclosed. An example disclosed seal includes a seal for use with a butterfly valve. The example seal includes a substantially flexible ring-shaped carrier configured to be moveably fixed within the butterfly valve and to surround a flow control aperture therein. The example seal includes a seal stiffener adjacent the substantially flexible ring-shaped carrier to increase the stiffness of the substantially flexible ring-shaped carrier in a first flow direction. The example seal includes a substantially rigid seal ring to engage an opposing surface.

Abstract: Flexible seals for process control valves are disclosed. An example disclosed seal includes a seal for use with a butterfly valve. The example seal includes a substantially flexible ring-shaped carrier configured to be moveably fixed within the butterfly valve and to surround a flow control aperture therein. The example seal includes a seal stiffener adjacent the substantially flexible ring-shaped carrier to increase the stiffness of the substantially flexible ring-shaped carrier in a first flow direction. The example seal includes a substantially rigid seal ring to engage an opposing surface.

Abstract: A method for collaborative document editing determines a document update upload rate based on edit characteristics. The document update upload rate is used to determine when edits made via a particular user device are sent to a document collaboration server. The edit characteristics include a number of a plurality of users collaboratively editing a document, a current edit location within the document for one of the users, and the type of connection and speed of the connection between a user device and the document collaboration server. The document update upload rate can be determined in response to a change in one of the edit characteristics.

Abstract: A flight management system (FMS) including a plurality of FMS components that can include a civil FMS component and a tactical FMS component. Each FMS component can have a processor programmed to execute an FMS software product. The FMS can also include a multi core FMS manager configured to control a plurality of flight management systems and coupled to the plurality of FMS components. The multi core FMS manager can include a plurality of FMS managers, each coupled to one of the FMS components, and a platform interface manager coupled to an avionics system. Each FMS manager can be adapted to transmit flight management data to, and to receive flight management data from, the FMS component to which it is coupled. The platform interface manager can be adapted to provide each FMS component access to the avionics system, such that an aircraft operator can control each FMS component via the FMS.

Abstract: A computerized method for providing a unified user interface to a plurality of flight management components encapsulated within a flight management system. The method can include receiving a flight management system input dataset from a first flight management system user interface device. The method can also include creating, with a processor programmed to provide a unified user interface, a plurality of flight management system input data portions to be transmitted to a plurality of destination flight management system components. The plurality of flight management system input data portions can be based on the flight management system input dataset and each flight management system input data portion can correspond to one of said plurality of destination flight management system components. Each of said plurality of flight management system input data portions can be transmitted from the processor to said corresponding destination flight management system component.

Abstract: The present invention provides novel systems and methods for processing packages through a delivery network using a hub assist label. Generally described, the hub assist label includes indicia of a sequence of sorting locations that designates the flow of a package through a delivery network.

Abstract: A computerized method for transmitting data between a multi core vehicle management system and a vehicle system. The method can include receiving, at a vehicle management system computer, a vehicle system request message from a requesting vehicle management system component. The requesting vehicle management system component can be one of a plurality of vehicle management system components, and the vehicle system request message can have a destination vehicle system component. The method can include generating a sanitized vehicle system request message based on the requesting vehicle management system component and the destination vehicle system component. The sanitized vehicle system request message can be transmitted to said destination vehicle system component.

Abstract: A computerized method for performing countermeasure transmission of decoy vehicle data. The method can include receiving a vehicle management data message from one of a plurality of vehicle management system components. The vehicle management data message can have data indicating at least one destination component, and the at least one destination component can include a civil transponder. The method can include transforming said vehicle management data message into a decoy vehicle management data message and transmitting the decoy flight management data message to at least one of the at least one destination component(s).

Abstract: A computerized method for providing a unified user interface to a plurality of flight management components encapsulated within a flight management system. The method can include receiving a flight management system input dataset from a first flight management system user interface device. The method can also include creating, with a processor programmed to provide a unified user interface, a plurality of flight management system input data portions to be transmitted to a plurality of destination flight management system components. The plurality of flight management system input data portions can be based on the flight management system input dataset and each flight management system input data portion can correspond to one of said plurality of destination flight management system components. Each of said plurality of flight management system input data portions can be transmitted from the processor to said corresponding destination flight management system component.

Abstract: A computerized method for providing a unified user interface to a plurality of flight management components encapsulated within a flight management system. The method can include receiving a flight management system input dataset from a first flight management system user interface device. The method can also include creating, with a processor programmed to provide a unified user interface, a plurality of flight management system input data portions to be transmitted to a plurality of destination flight management system components. The plurality of flight management system input data portions can be based on the flight management system input dataset and each flight management system input data portion can correspond to one of said plurality of destination flight management system components. Each of said plurality of flight management system input data portions can be transmitted from the processor to said corresponding destination flight management system component.

Abstract: A computerized method for transmitting data between a multi core vehicle management system and a vehicle system. The method can include receiving, at a vehicle management system computer, a vehicle system request message from a requesting vehicle management system component. The requesting vehicle management system component can be one of a plurality of vehicle management system components, and the vehicle system request message can have a destination vehicle system component. The method can include generating a sanitized vehicle system request message based on the requesting vehicle management system component and the destination vehicle system component. The sanitized vehicle system request message can be transmitted to said destination vehicle system component.