Abstract: A method is provided. The method includes: forming a stator for a high-power density electric machine, the stator having a plurality of slots for receiving stator coils and having a back-iron; inserting the stator coils in the plurality of slots; and inserting a potting material in the plurality of slots of the stator, the potting material in thermal contact with adjacent stator coils and in thermal contact with the back-iron; wherein the potting material is formed by: mixing silicon carbide particles with a silicon carbide preceramic polymer to form a mixture; diluting the mixture with solvents to form a slurry; drying the slurry to form a paste; forming the paste into a shape; and firing the paste to form a ceramic material.

Abstract: This invention relates to thermoset, thermal insulating panel, pour-in-place and pour-in-place foams having desirable and unexpectedly low thermal conductivity, and to compositions, method and systems which use and/or are used to make such foams comprising: (a) providing thermosetting foam forming component and a blowing agent for forming predominantly closed cells in the foam, wherein the blowing agent comprises: (i) cis-1,1,1,4,4,4-hexafluoro-2-butene (HFO-1336mzzm(Z)) and cyclopentane, with the HFO-1336mzzm(Z) and cyclopentane in the blowing agent together comprising at least about 50% by weight of the total of all components in the blowing agent and (ii) the weight ratio of HFO-1336mzzm(Z) to cyclopentane in the blowing agent is from about 45:55 to less than 68:32 and (b) forming foam from said provided foamable composition.

Abstract: A method of querying a set of raw data includes: receiving raw data; generating a base table having a primary key including a partition key and a sort key; generating a first set of local secondary indexes for the base table, the specific local secondary index sort key being a different one of the plurality of attributes than the sort key of the base table; developing one or more usage factors for each of the one or more local secondary indexes of the base table; receiving a second set of raw data having a plurality of attributes; generating a second base table including the second set of raw data; and generating a second set of local secondary indexes for the second base table based on the usage factors associated with the set of local secondary indexes.

Abstract: A system and method for detecting ground resonance and providing a warning regarding the same includes supplying, from an inertial navigation system (INS), inertial data indicative of an inertial profile of a rotorcraft, and supplying, from a sensor system, sensor data that indicates when the rotorcraft is at least partially on a landing surface. The sensor data is processed, in a processing system, to determine when the rotorcraft is at least partially on the landing surface, and when the rotorcraft is determined to be at least partially on the landing surface, the inertial data is processed, in the processing system to determine when the inertial profile of the rotorcraft indicates ground resonance may occur. Upon determining that ground resonance may occur, one or more alert signals are generated in the processing system.

Abstract: Embodiments relate generally to systems and methods for gas detection. A method may comprise operating a gas detector with a first alarm setting comprising a first predefined threshold; receiving sensed data of oxygen content in the ambient air; when the sensed data is below the first predefined threshold, activating an alarm; generating an acknowledgement request asking if the gas detector has entered an inert work zone; receiving a response from the user acknowledging that the gas detector has entered an inert work zone; deactivating the alarm; changing the alarm settings of the gas detector to a second alarm setting comprising a second predefined threshold; continuing to receive sensed data of oxygen content in the ambient air; when the sensed data is above the second predefined threshold, activating an alarm; and generating an acknowledgement request for the user asking if the gas detector has entered a normal operation work zone.

Abstract: Cascaded refrigeration systems containing: a plurality of refrigeration units, each refrigeration unit containing a first refrigeration circuit, each first refrigeration circuit comprising an evaporator and a heat exchanger; and a second refrigeration circuit; wherein each first circuit heat exchanger is arranged to transfer heat energy between its respective first refrigeration circuit and the second refrigeration circuit.

Abstract: The present invention relates to a system for identifying identify of interest data structures based on a trained identity of interest model and using individual-incident data structures integrating individual identification data received from third party resources based on an incident data structure.

Abstract: Systems and methods for reconfigurable on-vehicle data routing are provided. In one embodiment, a data link communication system comprises: a router to communicate with at least one communication bus and at least one data bus, and monitor data communicated over the communication data buses, wherein the communication bus communicates data link messages with an off-vehicle service provider system, wherein the data bus transports data between the router and a plurality of on-vehicle systems; a routing control logic; and a conditional logic database, wherein the database comprises definitions of one or more datatypes and definitions for at least one data forwarding command; wherein, in response to receiving a first set of data associated with a datatype defined by the database, the logic executes the at least one data forwarding command to control the router to output a second set of data to one or more of the plurality of on-vehicle systems.

Abstract: Systems and methods are provided for detecting potential vehicle operator incapacitation based on operator physiological state data. Raw operator physiological state data is received from a biosensing wearable device of an operator of a vehicle. The raw operator physiological state data includes raw operator actigraphy state data. Contextual motion data is received from at least one environmental motion sensor. The contextual motion data is associated with movement of the vehicle. A motion filter mask is generated based on the contextual motion data. The motion filter mask is applied to the raw operator actigraphy state data to filter the contextual motion data from the raw operator actigraphy state data to generate actual operator actigraphy state data. A determination is made regarding whether the actual operator actigraphy state data is less than an actigraphy threshold. An operator incapacity alert is issued based on the determination.

Abstract: Systems and methods are provided for generating a modified flight to avoid a no turn situation. A current flight path of an aircraft is received from a source of current flight path of the aircraft. Current aircraft location data is received from at least one geospatial sensor of the aircraft. Terrain data is retrieved from an onboard database based on the current aircraft location data. The terrain data includes a first terrain obstacle and a second terrain obstacle. A determination is made regarding whether the current flight path of the aircraft leads to a no turn situation with respect to the first terrain obstacle and the second terrain obstacle. A first notification associated with implementation of a modified flight path in accordance with a viable turn with respect to the first terrain obstacle and the second terrain obstacle is displayed on an onboard display device based on the determination.

Abstract: Compositions comprising multi-fluorinated olefins and HFC-32 are disclosed. Such compositions are useful particularly for in stationary refrigeration and air conditioning equipment.

Abstract: The present invention relates to a refrigerant composition, including difluoromethane (HFC-32), pentafluoroethane (HFC-125), and trifluoroiodomethane (CF3I) for use in a heat exchange system, including air conditioning and refrigeration applications and in particular aspects to the use of such compositions as a replacement of the refrigerant R-410A for heating and cooling applications and to retrofitting heat exchange systems, including systems designed for use with R-410A.

Abstract: Disclosed are methods of applying a leave-on personal care treatment products comprising: a) providing a container having a nozzle or opening for selectively releasing the contents thereof; b) including in the container a leave-on personal care formulation comprising: (i) an active component for affecting the personal care of the user; (ii) a carrier for the active component, said carrier comprising at least about 50% by weight of trans-HCFO-1233zd and optionally a co-carrier in amounts of up to about 50% by weight; and c) spraying said leave-on personal care formulation from the container and onto the area of the user to be treated.

Abstract: A system configuration significantly reduces the number of interconnections needed between an electromechanical actuator (EMA) and an EMA controller (EMAC) while maintaining redundancy and other safety aspects needed by the target application. This allows simplification of communication interfaces between multiple sensors in the EMA and EMAC and unification of the interface to multiple sensors inside the EMAC, leading to cost and weight reduction that can be significant for many aerospace products and applications, including unmanned vehicle (e.g., UAM/UAV) applications.

Abstract: A digital surface position sensor includes a position sensor, an adaptable hardware interface, and a processing circuit. The position sensor is adapted to be coupled to an aircraft flight control surface and is configured to sense a position of the aircraft flight control surface and supply a position signal representative thereof. The adaptable hardware input supplies an identification signal that identifies the aircraft flight control surface to which the position sensor is coupled. The processing circuit is coupled to receive the position signal and the identification signal. The processing circuit is configured, upon receipt of the signals, to process the position signal and the identification signal and generate (i) a first digital position signal representative of the position of, and the identification of, the aircraft flight control surface and (ii) and independent second digital signal representative of the position of, and the identification of, the aircraft flight control surface.

Abstract: A system for detecting ice accretion on a rotor of an aircraft includes a processing system that is configured to: receive torque data indicative of actual torque supplied from an electric motor to the rotor; implement a model of the electric motor and the rotor that determines an estimated torque that should be supplied from the electric motor to the rotor; compute a load on the rotor from the actual torque and the estimated torque; compare the computed load to a predetermined magnitude; and when the computed load exceeds the predetermined magnitude, generate an alert that indicates ice is accreting on the rotor.

Abstract: Systems for an integrated photonic responsive material sensor are described herein. In certain embodiments, a system includes a carrier wafer that includes a cavity formed in the carrier wafer. The carrier wafer also includes a responsive waveguide coupled to the cavity, the responsive waveguide formed from responsive material responsive to a force by shifting a resonance frequency of point defects in the responsive material in response to the force, wherein a pump light is directed to the responsive waveguide to prepare the responsive waveguide to absorb a probe light when exposed to a radio frequency at the point defect resonance frequency. Additionally, the system includes components coupled to the carrier wafer, wherein the components include a probe light source that generates the probe light, wherein the components are positioned in relation to the carrier wafer to couple the probe light into the cavity.

Abstract: Printer circuits and components for detecting a media low condition on a printer are provided. The printer circuit comprises a motor coupled to a platen roller, a current sense resistor coupled in series with the motor, a current measuring circuit comprising an operational amplifier circuit configured to receive input voltage and output voltage of the current sense resistor, generate a differential voltage based at least in part on the input voltage and the output voltage, and convert the differential voltage to a current, and an analog-to-digital converter and control mechanism configured to receive the current from the current measuring circuit and control operation of the motor based at least in part on the current.