An air curtain device and an air circulation system are provided. The air curtain device includes a main body, an air supply opening configured to receive air, an armrest air jet aperture configured to discharge the received air, and a headrest air jet aperture configured to discharge the received air. The air circulation system includes an air supply device and the air curtain device.

A cushion assembly such as an aircraft passenger seat cushion assembly including a solid foam component and an elastomeric lattice insert disposed in a void in the solid foam component, the elastomeric lattice insert having a compression profile that mimics a predetermined compression profile of a solid foam. The elastomeric lattice insert including repeating like cuboid structures such as interconnected repeating face-centered cube structures, interconnected repeating body-centered cube structures, or interconnected repeating kagome structures. The elastomeric lattice insert may be in thermal communication with an air conditioning system for delivering conditioned air through the elastomeric lattice insert.

A ventilated seat assembly such as an aircraft passenger seat including a cushion assembly supported by a structural element, a plurality of Venturi tubes positioned to direct a flow of air through the cushion assembly, an air compressor supplying compressed air, a manifold assembly coupled in fluid communication with the air compressor, a conduit network fluidly coupling the manifold assembly with the plurality of Venturi tubes, and a controller for activating the air compressor and actuating the manifold assembly. Supplying a small volume of pressurized air to the Venturi tubes induces a larger flow of ambient air and a multiplied air effect to ventilate the passenger seat.

A ventilated seat assembly such as an aircraft passenger seat including a cushion assembly supported by a structural element, a plurality of Venturi tubes positioned to direct a flow of air through the cushion assembly, an air compressor supplying compressed air, a manifold assembly coupled in fluid communication with the air compressor, a conduit network fluidly coupling the manifold assembly with the plurality of Venturi tubes, and a controller for activating the air compressor and actuating the manifold assembly. Supplying a small volume of pressurized air to the Venturi tubes induces a larger flow of ambient air and a multiplied air effect to ventilate the passenger seat.

A conditioning system for a vehicle passenger seat and a vehicle passenger seat assembly, the system including at least one conditioning unit including a Venturi device configured to generate air flow relative to a seat element and a temperature element configured to heat or cool the Venturi device or the air flow, a temperature sensor configured to sense a temperature in relation to the at least one conditioning unit, and a controller communicatively coupled to the temperature sensor and operably coupled to the at least one conditioning unit. The controller is configured to operate in a first operating condition in which the Venturi device is activated and the temperature element is inactive to ventilate the seat, and a second operating condition in which both the Venturi device and the temperature element are activated to heat or cool the seat.

A ventilated seat assembly with active air circulation including a structural frame element, a cushion assembly supported by the structural frame element, a perforated dress cover, a conduit network embedded in the cushion assembly configured to direct air to at least one target region of the cushion assembly, an air mover coupled in fluid communication with the conduit network, and a controller operable for activating the air mover to cause air to flow through the conduit network to the at least one target region. In operation, the controller activates the air mover to flow air, such as unconditioned air, through the conduit network to be released through the dress cover in the at least one target region.

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.

An integrated passenger service unit (PSU) is disclosed. The integrated PSU includes a housing installable into an aircraft overhead panel and a control knob set into, and positionable relative to, the housing. The housing incorporates signage elements (e.g., fasten seat belts, no smoking) visible through its exterior surface, as well as reading lights and gasper outlets set thereinto (e.g., as adjacent segments of an annulus). Each reading light includes an LED array selectably configured to illuminate the corresponding seat, and each gasper outlet directs an airstream toward the seat. The housing includes a notification ring configured to illuminate when the passenger calls a flight attendant. A control knob is set within the housing and positionable relative thereto. The control knob incorporates an LCD display and user interface (UI) which allows the occupant or passenger to view and adjust the status of the reading lights, gasper outlets, and notification ring.

The present invention achieves technical advantages as an aircraft having an augmented reality flight control system integrated with and operable from the pilot seat and an associated pilot headgear unit, wherein the flight control system is supplemented by flight-assisting artificial intelligence and geo-location systems. The present invention includes an augmented reality flight control system incorporating real-world objects with virtual elements to provide relevant data to a pilot during aircraft flight. A translucent substrate is disposed in the pilot's field of view such that the pilot can see therethrough, and observe virtual elements displayed on the substrate. The system includes a headgear that is worn by the pilot. A flight assistance module is configured to receive ii data related to the aircraft and provide predictive assistance to the pilot during flight based on the received data based in part on a pilot profile having preferences related to the pilot.

Described is an aircraft suite having an aircraft seat for use by a passenger, the aircraft suite also having a controller, for controlling a number of output states of the aircraft suite, the controller having a logic condition receiver for receiving a logic condition input, and distance measurement equipment for measuring a distance between a first location within the suite and a second location within the suite, and providing a distance input to a distance receiver of the controller, wherein, in use, the controller controls at least one of the output states of the aircraft suite based upon both the logic condition input and the distance input. The invention also provides a method of controlling an environment within an aircraft suite.