Abstract: An apparatus has an upright gantry. A tube arm assembly and a compression arm assembly are rotatably coupled to the gantry. The tube arm assembly independently rotates relative to the compression arm assembly. A controller disposed on the gantry is operably connected to at least one of the tube arm assembly and the compression arm assembly.

Abstract: An apparatus has an upright gantry. A tube arm assembly and a compression arm assembly are rotatably coupled to the gantry. The tube arm assembly independently rotates relative to the compression arm assembly. A controller disposed on the gantry is operably connected to at least one of the tube arm assembly and the compression arm assembly.

Abstract: An aircraft seat for an aircraft passenger compartment suite may include a primary section with an upper actuatable portion and a lower actuatable portion. The primary section may be configured to actuate between a primary upright position and a primary lie-flat position. The aircraft seat may include an auxiliary section including an auxiliary seatback portion coupled to a privacy shell element of the aircraft passenger compartment suite and an auxiliary seat base portion configured to actuate between an auxiliary upright position and an auxiliary lie-flat position. The auxiliary seatback portion may include an actuatable element. The actuatable element may be configured to actuate between an open position and a closed position. The actuatable element may be configured to provide access to a stowage compartment when the actuatable element is in the open position.

Abstract: A headgear device for a user including an integrated face shield, mask and hood. More specifically, the headgear device includes a hood, a face shield, and a moisture barrier fabric to cover the user's mouth when the headgear device is worn and direct air out through a breathable particle filtration fabric.

Abstract: An aircraft seat for an aircraft passenger compartment suite is disclosed. In embodiments, the aircraft seat includes a primary section including a primary seatback portion and a primary seat base portion, and an auxiliary section including an auxiliary seatback portion and an auxiliary seat base portion. In embodiments, the aircraft seat may further include an actuatable element configured to actuate between an open position and a closed position. The actuatable element may include a first surface which defines at least a portion of the auxiliary seatback portion when the actuatable element is in the closed position, and a second surface which defines a surface of an armrest when the actuatable element is in the open position.

Abstract: An apparatus has an upright gantry. A tube arm assembly and a compression arm assembly are rotatably coupled to the gantry. The tube arm assembly independently rotates relative to the compression arm assembly. A controller disposed on the gantry is operably connected to at least one of the tube arm assembly and the compression arm assembly.

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: An apparatus has an upright gantry. A tube arm assembly and a compression arm assembly are rotatably coupled to the gantry. The tube arm assembly independently rotates relative to the compression arm assembly. A controller disposed on the gantry is operably connected to at least one of the tube arm assembly and the compression arm assembly.

Abstract: An aircraft seat for an aircraft passenger compartment suite may include a primary section with an upper actuatable portion and a lower actuatable portion. The primary section may be configured to actuate between a primary upright position and a primary lie-flat position. The aircraft seat may include an auxiliary section including an auxiliary seatback portion coupled to a privacy shell element of the aircraft passenger compartment suite and an auxiliary seat base portion configured to actuate between an auxiliary upright position and an auxiliary lie-flat position. The auxiliary seatback portion may include an actuatable element. The actuatable element may be configured to actuate between an open position and a closed position. The actuatable element may be configured to provide access to a stowage compartment when the actuatable element is in the open position.

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: An aircraft seat for an aircraft passenger compartment suite is disclosed. In embodiments, the aircraft seat includes a primary section including a primary seatback portion and a primary seat base portion, and an auxiliary section including an auxiliary seatback portion and an auxiliary seat base portion. In embodiments, the aircraft seat may further include an actuatable element configured to actuate between an open position and a closed position. The actuatable element may include a first surface which defines at least a portion of the auxiliary seatback portion when the actuatable element is in the closed position, and a second surface which defines a surface of an armrest when the actuatable element is in the open position.

Abstract: A headgear device for a user including an integrated face shield, mask and hood. More specifically, the headgear device includes a hood, a face shield, and a moisture barrier fabric to cover the user's mouth when the headgear device is worn and direct air out through a breathable particle filtration fabric.

Abstract: An apparatus has an upright gantry. A tube arm assembly and a compression arm assembly are rotatably coupled to the gantry. The tube arm assembly independently rotates relative to the compression arm assembly. A controller disposed on the gantry is operably connected to at least one of the tube arm assembly and the compression arm assembly.

Abstract: A system may include an aircraft passenger seat implemented in an aircraft and an aircraft passenger computing device implemented in, on, or in proximity to the aircraft passenger seat. The aircraft passenger computing device may be communicatively coupled to an animal crate assembly onboard the aircraft. The aircraft passenger computing device may include an aircraft passenger display viewable by a passenger and a processor communicatively coupled to the aircraft passenger display. The processor may be configured to: receive sensor data from a sensor implemented in or on the animal crate assembly; receive captured animal crate assembly video data from a camera implemented in or on the animal crate assembly; generate graphical data based on the sensor data and the captured animal crate assembly video data; and output the graphical data to the aircraft passenger display for presentation to the passenger.

Abstract: In an illustrative embodiment, systems and methods for controlling projection of graphical elements onto surfaces of an aircraft cabin interior may include a projector mounted to a surface of a static element of an aircraft passenger suite that outputs the graphical element onto a projection surface. The graphical element may correspond to a received projection request. A controller may receive a projection request from a computing device indicating a type of graphical element for display onto the projection surface. The type of graphical element may correspond to a type of communication message such as a message between a passenger and a flight attendant within the aircraft cabin. The graphical element may generated for display by the projector based on at least one of the type of graphical element associated with the received projection request and a native language of the passenger or flight attendant.

Abstract: An aircraft seating group has first and second laterally-adjacent passenger seats; a center console positioned between the first and second passenger seats; a center console disposed between the first and second laterally-adjacent passenger seats and having a shelf for supporting a handheld electronic device at approximately an eye level of a passenger in the first passenger seat. The center console may further include a retention system to maintain the electronic device in the shelf in a position allowing the passenger to comfortably view the screen of the electronic device.