Abstract: An integrated optical beam steering device includes a planar Luneburg lens that collimates beams from different inputs in different directions within the lens plane. It also includes a curved (e.g., semi-circular or arced) grating coupler that diffracts the collimated beams out of the lens plane. The beams can be steered in the plane by controlling the direction along which the lens is illuminated and out of the plane by varying the beam wavelength. Unlike other beam steering devices, this device can operate over an extremely wide field of view—up to 180°—without any aberrations off boresight. In other words, the beam quality is uniform in all directions, unlike with aplanatic lenses, thanks to the circular symmetry of the planar Luneburg lens, which may be composed of subwavelength features. The lens is also robust to misalignment and fabrication imperfections and can be made using standard CMOS processes.

Abstract: A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.

Abstract: A system for both onboard piloting and remote piloting an aircraft having thereon at least one onboard pilot includes an aircraft having an onboard flight control system, onboard flight control devices, and onboard condition indicators mounted proximal the pilot seat. A remote flight control system, in electronic communication with the onboard flight control system, includes remote flight control devices and remote condition indicators. At least in a remote piloting mode, the onboard flight control system transmits flight and aircraft condition-related signals to the remote flight control system, receives flight control signals from the remote flight control system, and actuates, according to the flight control signals received from the remote flight control system, onboard actuators thereby remote piloting the aircraft. In the remote piloting mode, the aircraft may be cooperatively piloted by a remote pilot and at least one alert onboard pilot as another onboard pilot rests.

Abstract: A combination adaptive energy absorption and emergency flotation device for positioning beneath a plurality of seat pans of a seat assembly in an aircraft seating application. The device includes a plurality of fluidly coupled inflatable elastic bladders, at least one constrictor valve fluidly coupling at least two adjacent ones of the plurality of inflatable elastic bladders allowing fluid flow therethrough in response to predetermined pressure on the device from the plurality of seat pans, and a fluid supply source fluidly coupled to the plurality of inflatable elastic bladders for outputting a positive flow of fluid to the plurality of inflatable elastic bladders, wherein the adaptive energy absorption device is detached from the plurality of seat pans to allow removal from beneath the plurality of seat pans for use as an emergency flotation device.

Abstract: A sensor pod system includes one or more sensor pods with a plurality of sensors configured to collect data from an environment. A sensor pod may have an effective field of view created by individual sensors with overlapping fields of view. The sensor pod system may include sensors of different types and modalities. Sensor pods of the sensor pod system may be modularly installed on a vehicle, for example, an autonomous vehicle and collect and provide data of the environment during operation of the vehicle. A combination of techniques may be used to calibrate a sensor pod prior to installation in the vehicle and may be used to determine if the sensor pod is compatible with other sensor pods and may also be used to calibrate other sensors when integrating the sensor pod into the vehicle.

Abstract: An aircraft passenger compartment suite may include a privacy divider configured to separate a first side of the aircraft passenger compartment suite including a first aircraft seat and a second side of the aircraft passenger compartment suite including a second aircraft seat. The aircraft passenger compartment suite may include a collapsible display device positioned proximate to the privacy divider of the aircraft passenger compartment suite. The aircraft passenger compartment suite may include a first display device and a first plate configured to be an extension of a horizontal surface in the first side when the first display device is in a first display device stowed position. The aircraft passenger compartment suite may include a second display device and a second plate configured to be an extension of a horizontal surface in the second side when the second display device is in a second display device stowed position.

Abstract: A sensor pod system includes one or more sensor pods with a plurality of sensors configured to collect data from an environment. A sensor pod may include a housing and extend from a portion of a body of a vehicle. The sensor pod housing may have energy absorbing structures configured to absorb and dissipate energy during an impact in order to protect a pedestrian. The sensor pod may have deformable portions of the housing configured to absorb and dissipate energy during the impact. The sensor pod may have deformable fasteners coupling a sensor to the sensor pod configured to deform to absorb and dissipate energy during the impact.

Abstract: An aircraft passenger compartment suite may include a privacy shell element proximate to an aircraft seat installed within the aircraft passenger compartment suite. The privacy shell element may include a first section configured to conform to a primary section of the aircraft seat, and a second section configured to conform to an auxiliary section of the aircraft seat. The privacy shell element may include a first profile configured to conform with the aircraft seat when the aircraft seat is in a first position, and a second profile configured to conform with the aircraft seat when the aircraft seat is in a second position. The second profile of the privacy shell element may be configured to occupy a greater amount of passenger aircraft living space surrounding the aircraft passenger compartment suite than an amount of passenger aircraft living space occupied by the first profile of the privacy shell element.

Abstract: A slanted aircraft seat privacy panel may include a body. The body may be defined by a contour line along at least a portion of a height of the body. The contour line may be a straight line slanted at an angle relative to a vertical line. The vertical line may be defined relative to a floor of the aircraft cabin. The contour line being slanted may generate increased shoulder space in the passenger compartment in the aircraft cabin. The increased shoulder space in the passenger compartment may use a portion of non-fully utilized space in an adjacent passenger compartment in the aircraft cabin. The passenger compartment and the adjacent passenger compartment may be offset relative to an aisle in the aircraft cabin. A portion of each of the passenger compartment and the adjacent passenger compartment may be formed by the slanted aircraft seat privacy panel.

Abstract: A female urinary relief device is disclosed. The device may include an intimate interface device (IID) configured to be positioned intimate with a user's body. The IID may include a tray including a raised perimeter forming a seal between the user's body and the tray. The IID may include a fluid cavity configured to capture fluid from the user's body. The IID may include a pad including a slot configured to provide an unobstructed route to the fluid cavity. The device may include a fluid removal system configured to remove the fluid from the fluid cavity and route the fluid to a storage device. The fluid removal system may include a suction sub-system configured to pull the fluid against gravity to remove the fluid from the fluid cavity. The fluid removal system may include discharge hoses configured to fluidically and mechanically couple the IID to the storage device.

Abstract: A static aircraft seat privacy panel may include a body. At least a portion of a surface of the body may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge of the body may be configured to couple to a floor via a set of floor-mounted components. The set of floor-mounted components may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge of the body may be configured to be offset a selected distance from a surface of one or more overhead structures of the aircraft cabin when the body is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel may be compliant with 9G force requirements for aviation transport.

Abstract: An integrated optical beam steering device includes a planar Luneburg lens that collimates beams from different inputs in different directions within the lens plane. It also includes a curved (e.g., semi-circular or arced) grating coupler that diffracts the collimated beams out of the lens plane. The beams can be steered in the plane by controlling the direction along which the lens is illuminated and out of the plane by varying the beam wavelength. Unlike other beam steering devices, this device can operate over an extremely wide field of view—up to 180°—without any aberrations off boresight. In other words, the beam quality is uniform in all directions, unlike with aplanatic lenses, thanks to the circular symmetry of the planar Luneburg lens, which may be composed of subwavelength features. The lens is also robust to misalignment and fabrication imperfections and can be made using standard CMOS processes.

Abstract: An aircraft passenger compartment suite may include at least one single passenger compartment including at least one single aircraft seat. The at least one single aircraft seat may be configured to seat a single passenger. The aircraft passenger compartment suite may include a combined divan passenger compartment with a combined divan aircraft seat. The combined divan aircraft seat may be configured to seat at least one passenger. The combined divan aircraft seat may have a width greater than a width of the at least one single aircraft seat. The combined divan passenger compartment may include a stowage compartment configured to stow large passenger amenities in a substantially vertical orientation. The aircraft passenger compartment suite may include a privacy divider separating the combined divan passenger compartment and the at least one single passenger compartment.

Abstract: Systems and methods for monitoring passenger activity in an aircraft cabin environment to predict immediate future passenger needs. The systems and methods make use of sensors positioned within an aircraft cabin environment configured to sense condition changes of objects corresponding to predetermined service issues, device(s) usable by the service crew indicating the sensed condition changes, and processing circuitry configured to receive sensor signals and indicate the condition changes through the device(s) such that the service crew is made aware of the condition changes requiring actions to be completed by the service crew to attend to the immediate future passenger needs.

Abstract: An economy class (Y class) private suite includes a continuous seatback and a stowable aisle-side panel. The continuous seatback covers the gaps between seats of a 3-seat or 4-seat PAX and the stowable aisle-side panel slides to close off the PAX from the aisle when desirable. Each seat in the PAX includes an extension element to extend from the anterior surface of the seat cushion and establish a substantially flat surface including the seat cushions and extension elements. A separate padded element may be placed over the substantially flat surface. Each seatback cushion in the PAX is removable and reconfigurable as a reclining support or expanded armrest.

Abstract: A seat usage prevention device is disclosed. The seat usage prevention deice includes at least one device component being configured to interact with one or more seat components of a first seat. The device component is configured to prevent usage of at least one of a seat pan or seatback of the first seat. The device component further separates a second seat from at least a third seat, wherein the third seat is proximate to at least one of the first seat or the second seat. The seat usage prevention device may include a device component that further includes a cushion, a base, an amenity console, or a vertical separator, or combination thereof.

Abstract: A system and method for autonomous inspection and sanitation of an aircraft interior cabin employs a plurality of unmanned aircraft system (UAS) for autonomous operation to inspect, sense, identify, and cure an abnormal found onboard an aircraft cabin prior to passenger boarding. UAS mounted on a nearby jetway as well as in various locations throughout the aircraft cabin are equipped with a plurality of sensors to autonomously sense and cure, or sense and communicate to maintenance the identification and location of the abnormal. A single multi-role UAS inspects and sanitizes using onboard systems while multiple types of UAS including inspection UAS and sanitation UAS singularly function to sense an abnormal and sanitize if able or communicate to higher authority if unable to cure the abnormal.

Abstract: A sensor pod system includes one or more sensor pods with a plurality of sensors configured to collect data from an environment. A sensor pod may include a housing and extend from a portion of a body of a vehicle. The sensor pod housing may have energy absorbing structures configured to absorb and dissipate energy during an impact in order to protect a pedestrian. The sensor pod may have deformable portions of the housing configured to absorb and dissipate energy during the impact. The sensor pod may have deformable fasteners coupling a sensor to the sensor pod configured to deform to absorb and dissipate energy during the impact.

Abstract: A sensor pod system includes one or more sensor pods with a plurality of sensors configured to collect data from an environment. A sensor pod may have an effective field of view created by individual sensors with overlapping fields of view. The sensor pod system may include sensors of different types and modalities. Sensor pods of the sensor pod system may be modularly installed on a vehicle, for example, an autonomous vehicle and collect and provide data of the environment during operation of the vehicle.