An apparatus to separate water droplets from an air stream includes an elongated tube having a first end and a second end. The elongated tube includes an opening at a first end of the elongated tube, the opening may be positioned to accept the air stream. A reservoir is positioned at a second end of the elongated tube. A helix structure is positioned within the elongated tube. The helix structure includes an upper surface, a lower surface arranged opposite the upper surface, an outer edge, and a variable pitch along a length of the elongated tube. The variable pitch may provide a variable interior angle between an inner wall of the elongated tube and the upper surface of the helix structure.

An apparatus to separate water droplets from an air stream includes an elongated tube having a first end and a second end. The elongated tube includes an opening at a first end of the elongated tube, the opening may be positioned to accept the air stream. A reservoir is positioned at a second end of the elongated tube. A helix structure is positioned within the elongated tube. The helix structure includes an upper surface, a lower surface arranged opposite the upper surface, an outer edge, and a variable pitch along a length of the elongated tube. The variable pitch may provide a variable interior angle between an inner wall of the elongated tube and the upper surface of the helix structure.

The disclosure belongs to the field of aerospace technology, and in particular relates to a method of urination and defecation in space. The method may include: forming a sealed space between a spacesuit below the waist and above the two thighs and the human skin before an astronaut urinates or defecates, and using, by the astronauts, the sealed space to urinate or defecate. The disclosure can confine the excrements in a small sealed space, and the operation thereof is simple, convenient and fast, and no excessive cost is required, and no pollution is caused in the spacesuit and the cabin, facilitating the astronauts' work in space.

The disclosure belongs to the field of aerospace technology, and in particular relates to a method of urination and defecation in space. The method may include: forming a sealed space between a spacesuit below the waist and above the two thighs and the human skin before an astronaut urinates or defecates, and using, by the astronauts, the sealed space to urinate or defecate. The disclosure can confine the excrements in a small sealed space, and the operation thereof is simple, convenient and fast, and no excessive cost is required, and no pollution is caused in the spacesuit and the cabin, facilitating the astronauts' work in space.

An actuatable emergency exit door with a door actuating device that comprises at least two connection rods that are pivotally mountable to an associated structural frame that is adapted for accommodating the actuatable emergency exit door in closed state, the at least two connection rods being provided for enabling an opening movement of the actuatable emergency exit door with respect to the associated structural frame during opening, wherein at least one door-mounted goose neck-shaped structure is mountable to the associated structural frame for enabling an initial translational opening movement and subsequently a swiveling opening movement of the actuatable emergency exit door with respect to the associated structural frame during opening. The invention is further related to an aircraft or space craft with a pressurized cabin having such an actuatable emergency exit door.

An actuatable emergency exit door with a door actuating device that comprises at least two connection rods that are pivotally mountable to an associated structural frame that is adapted for accommodating the actuatable emergency exit door in closed state, the at least two connection rods being provided for enabling an opening movement of the actuatable emergency exit door with respect to the associated structural frame during opening, wherein at least one door-mounted goose neck-shaped structure is mountable to the associated structural frame for enabling an initial translational opening movement and subsequently a swiveling opening movement of the actuatable emergency exit door with respect to the associated structural frame during opening. The invention is further related to an aircraft or space craft with a pressurized cabin having such an actuatable emergency exit door.

A conformal seat insert for an adjustable vehicle seat, the conformal seat insert comprising an insert frame, the insert frame having one or more insert reference features for locating the insert frame on a seat frame of the vehicle seat in a predetermined position relative to the seat frame, and a contoured support surface formed in the insert frame, the contoured support surface having a crew reference point corresponding to an acromial point of a shoulder of a seat occupant of the adjustable vehicle seat, the crew reference point being a datum from which an eye position of the seat occupant is established relative to instrumentation of an aerospace vehicle in which the adjustable vehicle seat is located.

A conformal seat insert for an adjustable vehicle seat, the conformal seat insert comprising an insert frame, the insert frame having one or more insert reference features for locating the insert frame on a seat frame of the vehicle seat in a predetermined position relative to the seat frame, and a contoured support surface formed in the insert frame, the contoured support surface having a crew reference point corresponding to an acromial point of a shoulder of a seat occupant of the adjustable vehicle seat, the crew reference point being a datum from which an eye position of the seat occupant is established relative to instrumentation of an aerospace vehicle in which the adjustable vehicle seat is located.

A method for configuring an interior of a reconfigurable vehicle using one or more cabin modules. The method comprises providing, by a user interface system, a plurality of possible cabin configuration options to a plurality of users for selection by the plurality of users so as to generate selection data indicative of cabin configuration options selected by the users. The cabin configuration options relate to types of configuration of the one or more cabin modules. The method comprises determining an availability of cabin configuration options based on inventory data which relates to types of configuration of cabin modules that are currently available for use so as to generate availability data, and generating a forecast of cabin modules predicted to be loaded on the reconfigurable vehicle based on the selection data and the availability data. The method further comprises updating the availability data and the selection data substantially in real time based on the inventory data and user input to the user interface system so as to generate updated availability data and updated selection data, and modifying the forecast based on the updated availability data and the updated selection data. The method comprises finalizing the forecast so as to generate commissioning data indicative of cabin modules to be loaded on the reconfigurable vehicle, loading the reconfigurable vehicle with one or more cabin modules based on the commissioning data, and updating the inventory data based on the cabin modules that are loaded on the reconfigurable vehicle.

A method for configuring an interior of a reconfigurable vehicle using one or more cabin modules. The method comprises providing, by a user interface system, a plurality of possible cabin configuration options to a plurality of users for selection by the plurality of users so as to generate selection data indicative of cabin configuration options selected by the users. The cabin configuration options relate to types of configuration of the one or more cabin modules. The method comprises determining an availability of cabin configuration options based on inventory data which relates to types of configuration of cabin modules that are currently available for use so as to generate availability data, and generating a forecast of cabin modules predicted to be loaded on the reconfigurable vehicle based on the selection data and the availability data. The method further comprises updating the availability data and the selection data substantially in real time based on the inventory data and user input to the user interface system so as to generate updated availability data and updated selection data, and modifying the forecast based on the updated availability data and the updated selection data. The method comprises finalizing the forecast so as to generate commissioning data indicative of cabin modules to be loaded on the reconfigurable vehicle, loading the reconfigurable vehicle with one or more cabin modules based on the commissioning data, and updating the inventory data based on the cabin modules that are loaded on the reconfigurable vehicle.