Abstract: A two degree-of-freedom brushless DC motor includes a stator, a rotor, a plurality of distributed stator windings, and a stator voice coil winding. The stator includes an inner stator structure and a plurality of arc-shaped stator poles. The inner stator structure includes a main body and a plurality of spokes that are spaced apart from each other to define a plurality of stator slots. Each arc-shaped stator pole is connected to a different one of the spokes. The rotor is spaced apart from the stator, includes a plurality of magnets, and is configured to rotate about a plurality of perpendicular axes. The distributed stator windings are wound around the plurality of spokes and extend through the stator slots. The stator voice coil winding is wound around the outer surfaces of the arc-shaped stator poles. The arc-shape and spacing of the stator poles define the stator as being spherically shaped.

Abstract: A two degree-of-freedom electromagnetic machine includes an inner stator, a plurality of stator windings, an outer stator, a voice coil winding, a rotor, a plurality of spin magnets, and a plurality of tilt magnets. The plurality of stator windings, when electrically energized, impart a torque on the rotor that causes the rotor to rotate, relative to the inner and outer stators, about a first rotational axis, and the voice coil winding, when electrically energized, imparts a torque on the rotor that causes the rotor to rotate, relative to the inner and outer stators, about a second rotational axis that is perpendicular to the first rotational axis.

Abstract: Systems for communicating over a network and between two or more network connected devices. In particular, the disclosure reveals systems which include a first node having a first node message sequence counter, a second node having a second node message sequence counter, and wherein the second node is configured to synchronize the first node message sequence counter based on the second node message sequence counter.

Abstract: Systems and methods for an integrated photon source and detector of entangled photons are provided. In certain embodiments, a system includes a first waveguide layer comprising a photon producing waveguide configured to provide two photons propagating in orthogonal modes of a single waveguide. The system also includes a second waveguide layer comprising a photon conditioning waveguide network, the second waveguide layer formed on the first waveguide layer, the second waveguide layer having a different index of refraction.

Abstract: Devices, systems, and methods for an alarming system for multi-unit buildings are described herein. One system includes a number of remote sensors positioned in a building having common areas and individual units occupied by occupants, the remote sensors are provided for sensing an alarm condition, a central control panel located in the common areas of the building for collecting data from the remote sensors, the control panel utilized for analyzing the collected data, determining whether to initiate an alarm, and sending one or more signals to initiate an alarm, if an alarm is to be initiated, and an occupant input device located in at least one individual unit for requesting a delay in initiating the alarm.

Abstract: Methods and systems for controlling a building. An illustrative method includes receiving sensor data from one or more sensors of the building, using the received sensor data to control one or more building management components to control one or more environmental conditions within the building, normalizing the sensor data and storing the normalized sensor data, comparing the normalized sensor data with normalized sensor data from one or more other buildings to identify one or more anomalies associated the building, and providing a recommended action to improve at least one of the one or more identified anomalies of the building.

Abstract: This disclosure is related to devices, systems, and techniques for determining, using an electro-opto-mechanical accelerometer system, a frequency value in order to determine an acceleration value. For example, an accelerometer system includes a light-emitting device configured to emit an optical signal and a circuit. The circuit is configured to determine a frequency value corresponding to the optical signal and determine an acceleration value based on the frequency value. Additionally, the accelerometer system includes a housing that encloses the light-emitting device, the circuit, and Helium gas, where the Helium gas defines a partial pressure within a range between 0.1 torr and 760 torr.

Abstract: A system and approach for verifying and validating a room condition and its behavior in a critical environment. The system and approach may be a room controller built on top of a Niagara™ framework or launched from a Niagara workbench, and leverages extensible of Niagara. The system and approach may be web-based and used to test and verify the room condition per preset conditions. The system may have steps or tabs. They may incorporate screens for a create/open task, select test zone, read flow, hood/booster, T-stat set-up or temperature lever set-up, visual checks, and a report. One may create a new task and edit any existing task on the controller. One may move from task to task in either direction or go directly to the report of a completed task.

Abstract: A stimulated Brillouin scattering gyroscope is provided. A pump laser generates continuous wave (CW) energy that travels through at least one bus waveguide to a waveguide resonator. A reflector is positioned within the waveguide resonator. The reflector is configured to pass at least some of the CW energy in a first direction and reflect at least some stimulated Brillouin scattering (SBS) energy in a second direction. A first detector is in operational communication with the at least one bus waveguide to detect CW energy. An output of the first detector used to at least adjust a pump laser frequency of the pump laser. A second detector is also in operational communication with the at least one bus waveguide. The second detector is used to determine phase shifts in detected SBS energy to determine at least rotation.

Abstract: A retention component for retaining a coil in a slot of a stator for a generator having a rotor includes a first segment and a second segment, both of which are configured to be inserted into the slot. At least one of the first and second segments is made entirely of laminated sheets that together form a unitary structure of magnetic material. At least one of the first and second segments has an interfacing surface configured to directly interface a rotor surface in the absence of a structure therebetween. A channel is between the first and second segments, and a third segment that extends along and within the channel. The third segment is less magnetic or non-magnetic than at least one of the first and second elements.

Abstract: In some examples, a radar system is configured to mount on an ownship vehicle for interleaving a weather detection mode and an object detection mode. The radar system comprises a phased-array radar device configured to receive weather signals in the weather detection mode, receive sensing signals in the object detection mode, and interleave the weather detection mode and the object detection mode. The radar system further comprises processing circuitry configured to determine weather conditions based on the received weather signals and detect an object based on the received sensing signals.

Abstract: Embodiments relate generally to gas detector connectivity devices, for example a dongle, to allow for continuous communication of real-time data between a gas detector and a central station. Dongle embodiments typically comprise an IR transceiver, a processor, a wireless interface device, a power source, and a means of attachment. Such dongle embodiments, and their related methods of operation, may allow for retrofitting of legacy gas detectors to provide wireless capabilities.

Abstract: Methods and systems are provided for generating a user and phase of flight dependent cockpit display. The methods and systems generate a display for a display device using display settings included in a user profile and a current phase of flight. The display settings include preferences defining a range of a map to be displayed that are different for different phases of flight, and preferences defining a level of declutter of a map to be displayed that are different for different phases of flight.

Abstract: Provided systems and methods for an aircraft lighting system (ALS) include a centralized blue generator that supplies blue light to a plurality (N) of passive light-heads distributed at various locations on the aircraft. A load profile for use of the N passive light-heads during all flight phases and operational phases is developed and uploaded into the system. Each of the passive light-heads is operationally coupled to the blue light generator via a respective light transmission element that is gated with a respective one of N light switches. A light generating control unit (LGCU) is coupled to the blue light generator, and controls the generation and actuation of blue light, in addition to controlling light switch positions, as a function of navigation data and the load profile. Each of the N passive light-heads comprises a respective light conversion element to convert the blue light into red, green, or white light.

Abstract: Systems and methods provide dynamically modifiable parameters in required time of arrival (RTA) speed regions of an assigned flight path of an aircraft. The system includes a vertical situation display (VSD) rendering thereon a vertical flight profile of the assigned flight path. A control module is coupled to the display system and configured to: demark the vertical flight profile with a plurality of RTA speed regions related to an initial speed profile; render an RTA speed band graphic having demarked sections vertically representing a speed minimum and speed maximum for an respective RTA speed region, the RTA speed band graphic representing a normalized speed range between zero and a maximum value for each respective RTA speed region. The control module accepts user modifications and updates the RTA speed band graphic and the current speed profile to reflect user input.

Abstract: A multi degree-of-freedom electromagnetic machine includes an outer case, an inner case, a stator, stator windings, a voice coil winding, a tilt magnet, a rotor, and rotor magnets. The inner case is disposed within an inner cavity of the outer case and is mounted to rotate relative to the outer case about one or more rotational axes. The stator is fixedly mounted within the inner case, and the stator windings are wound thereon. The voice coil winding is fixedly coupled to either the inner surface of the outer case or the outer surface of the inner case. The tilt magnet is fixedly coupled to either the outer surface of the inner case or the inner surface of the outer case. The rotor is rotationally mounted within the inner case and is operable to rotate, relative to the stator, about a rotational axis.

Abstract: Techniques for integrating a travel control system and attitude and heading (AHR) system in a vehicle are disclosed. The integrated system includes interface circuitry that enables data communication between constituent travel control system and AHR system of the integrated system, and can further communicate data between the travel control system and/or the AHR system and other system(s) or device(s) in or on the vehicle. In some embodiments, the travel control system includes processing circuitry that is fault tolerant. Alternatively, or additionally, the AHR system may include processing circuitry that has a processing power greater than the travel control system processing circuitry.

Abstract: Provided are technologically improved systems and methods for reducing controller-pilot data link (CPDLC) rejection ratio on an aircraft. The system is programmed to receive a user provided tentative CPDLC request. The system receives traffic data from an external traffic data source and data from a navigation system and a sensor system. The system predicts whether the tentative CPDLC request will be accepted by air traffic control (ATC), based on the received data. The system further predicts a potential delay time until the ATC will accept the tentative CPDLC request. The system additionally provides one or more alternative CPDLC requests and their potential delay times when the system has predicted that the tentative CPDLC request will be rejected. The system displays this information and receives user selections based thereon. Upon receiving a user selection, a CPDLC request is sent to ATC in accordance with a predicted delay time.

Abstract: Methods and systems for speech recognition in an aircraft are disclosed. Methods and systems include executing an air traffic control transcription application using first acoustic and language models and executing a command and control speech recognition application using second acoustic and language models. Flight context data is processed to identify additional words not included in training of the second acoustic and language model but included in training of the first acoustic and language models. Acoustic and language model parameters are extracted corresponding to the additional words from the first acoustic and language models. The extracted acoustic and language model parameters are added to the second acoustic and language models. An aircraft control command is generated that encapsulates at least one of the additional words using the command and control speech recognition application.

Abstract: A flight deck system and a method for providing a flight crew with a ground path to a destination at an aerodrome for taxiing is disclosed. The flight deck system includes a controller configured to: set a destination point on the ground at the aerodrome for an airborne aircraft that is preparing to land; estimate a stopping point for the aircraft on a runway; and predict a ground path for the aircraft to follow at the aerodrome from the runway to the destination point. To predict the controller is further configured to: determine a starting point on the runway for the predicted ground path; and determine a runway exit point to a taxiway. The controller is further configured to cause the predicted ground path to be displayed on a flight deck display device.