Abstract: To provide improved guidance for visually impaired passengers in lavatory situations on-board of vehicles, a vehicle guidance system for guiding visually impaired passengers on-board a vehicle is provided. The vehicle guidance system includes an interior space on-board the vehicle with at least one lavatory with enclosing cabin walls, and at least one guiding sanitary-handrail. The guiding sanitary-handrail is mounted along at least a part of the enclosing cabin walls inside the lavatory. The guiding sanitary-handrail is provided as a tactile guide. Further, the guiding handrail is provided with visually highlighted information and manually touchable information, both related to cabin information. Still further, a plurality of operating elements for controlling functions of the lavatory is provided inside the lavatory, and at least a part of the operating elements is arranged on the guiding sanitary-handrail.

Abstract: A system for installing modules on a fuselage structure has modules with holders arranged thereon for fastening on a fuselage structure, assembly stands, which can be moved on a floor level, and a flexible connecting element, extending via all the modules and coupling them together. Each assembly stand has a base for supporting the stand on the floor level and a holding device, designed to support the module. The assembly stands, the modules and the at least one connecting element are designed to form a chain of assembly stands, such that two successive groups of assembly stands enclose a pivot point at which the mutually facing modules have a larger spacing relative to one another than the modules within the respective groups. The connecting element allows the pivoting of the groups relative to one another at the pivot point through an angle of at least 90°.

Abstract: A tool for use in consolidation of a fibre-reinforced component has an outer casing supported by an internal structure. The outer casing has a first contact surface, which is provided for the purpose of resting flat against the component during the consolidation of the component and predetermining a shape of the component in some section or sections. The internal structure and the outer casing are configured in such a way that, when the tool is heated from an initial temperature to a consolidation temperature required for the consolidation of the component, the tool expands in such a way perpendicularly to the first contact surface that a defined first pressure is exerted on the component by the first contact surface. The use of a component of this kind is furthermore claimed and described.

Abstract: A system for monitoring a passenger cabin, in particular a passenger cabin of an aircraft, has a power supply channel (PSC) having a recess and extending longitudinally in a passenger cabin, wherein the recess points in the direction of the passenger cabin, a multiplicity of power supply unit modules (PSU) for arrangement in the recess, a multiplicity of cover modules for partially covering the recess, wherein the multiplicity of power supply unit modules and the multiplicity of cover modules can be arranged in the power supply channel such that the recess is partially covered by the multiplicity of power supply unit modules and the multiplicity of cover modules in the longitudinal orientation of the power supply channel in the direction of the passenger cabin, and at least one camera for capturing images of at least one part of the passenger cabin.

Abstract: In one embodiment, a dual configuration aircraft lavatory includes a plurality of walls enclosing and defining a lavatory interior space, wherein one of the walls is coextensive with a portion of the cabin. Within the lavatory interior space are a toilet, a washing station and a waste receptacle movable between a first position and a second position. In the first position, the waste receptacle is attached to a wall of the lavatory between the washing station and a door wall. In the second position, the waste receptacle occupies a second predetermined volume of space in the aircraft cabin separated from a first predetermined volume of space occupied by the waste receptacle in the first position. Moving the waste receptacle from the first position to the second position reveals additional space within the lavatory sufficient so that two adult humans simultaneously fit within the lavatory interior space.

Abstract: A pressure bulkhead for a pressurized cabin of an aerospace craft includes: a pressure wall and a frame for connecting the pressure wall to the aerospace craft; wherein the frame is connected to the pressure wall; wherein the pressure wall has: a core layer; and a first covering layer and a second covering layer; wherein the core layer is arranged between the first covering layer and the second covering layer; and wherein the core layer comprises an auxetic foam. Such a pressure bulkhead has increased stiffness, thus ensuring that smaller bending deformations and lower stresses occur. Hence costs can be saved, and the volume of the pressurized cabin which can be made available to the crew and passengers is maximized.

Abstract: A system for generating a moving image in an aircraft, includes a multiplicity of LEDs, a signal input unit, into which image information is fed, a signal output unit coupled to the multiplicity of LEDs and configured for transmitting the image information to the multiplicity of LEDs, and a gyroscopic sensor for acquiring a spatial position of the aircraft, wherein the LEDs are arranged in the form of a grid on an aircraft interior wall, such that the image is a schematic reproduction of the image information and the signal output unit is coupled to the gyroscopic sensor in such a way that the position of the image is matched to the spatial position of the aircraft, such that the image forms an artificial horizon for a viewer.

Abstract: A device providing a signal indicating whether a deployed aircraft evacuation slide is ready for use. A tilt sensor measures tilt angle about a predetermined axis and a tilt sensor measurement signal is provided. An inertial sensor detects acceleration and provides an inertial sensor measurement signal. A slide signal input terminal receives a slide signal indicating deployment of an evacuation slide and of a deployment length. A tilt angle signal output terminal at which a tilt angle signal is provided, and a slide status output terminal and a control unit to determine, based on the detected acceleration, a moment when the device is at rest with respect to earth and to set orientation of the reference plane to a predetermined orientation. The control unit stores data depending on position of a door, and can determine a slide length. A slide status signal is provided at the slide status output terminal.

Abstract: An aircraft tail region including a cooling system installed in the aircraft tail region. The cooling system comprises a cooler, which forms a section of an outer skin of the aircraft tail region, and includes coolant channels allowing a flow of ambient air therethrough, and extending from a first surface of the cooler to a second surface of the cooler. The cooling system also includes a fan system, which is adapted to convey ambient air through the coolant channels of the cooler at least in specified operating phases of the cooling system, and a first opening, which is formed in the outer skin of the aircraft tail region, and which allows, in conveying operation of the fan system, ambient air which is supplied through the coolant channels of the cooler into an interior of the aircraft tail region to be discharged back into the aircraft environment.

Abstract: An apparatus for controlling appliances aboard a vehicle, including a first data processing device having a network interface that can have a vehicle network for bidirectional data transmission between the first data processing device and connected network appliances. Also provided are an input/output device, a graphics processor device connected to the screen thereof and to the first data processing device, a user interface module provided in the first data processing device and that implements a graphical user interface having pages, and at least one separate second data processing device connected to the first data processing device via a separate bidirectional data link and having a network interface for connection to a vehicle network. Via each bidirectional data link it is exclusively possible to transmit predefined data records having data of predefined data types for display on pages from the second data processing device to the first data processing device.

Abstract: A service box for storing in a storage rack arrangement of a cargo container of a vehicle, in particular an aircraft, including a rectangular bottom wall, a rectangular upper wall, side walls and narrow end walls and forms an interior space adapted to receive a trolley for catering goods. The service box is provided with a door at at least one of its narrow ends, the door forming at least the main part of the narrow wall and in the open state permits insertion and removal of the trolley and in the closed state provides for an essentially closed space for the trolley.

Abstract: A system and a method for dynamic in flight seat management of an aircraft are provided. The system comprises an on board memory unit for storing the current booking status of the seats of the aircraft. Furthermore, the system comprises an output unit for providing the current booking status to a user and an input unit for receiving requests from a user to change the booking status. Therein, the system is adapted to change the booking status in real-time during the flight. In this way, passengers can book a time-limited upgrade during the flight.

Abstract: Described is a method for transmitting continuously created data items from an aircraft to a receiver. The data items are of a plurality of data types and each have a different priority. For each data type a live LIFO buffer and a main LIFO buffer are provided. In a regular operation mode continuously created data items are continuously stored in the main buffers. In a transmission operation mode continuously created data items are continuously stored in the live buffers, consecutive data packets are transmitted and for each data packet the data is selected from the buffers, wherein data items stored in live buffers are transmitted before data items stored in main buffers and data items of higher priorities are transmitted before data items of lower priorities. Further, a transmitter and an aircraft are described and claimed.

Abstract: A passenger lavatory unit has an enclosing structure enclosing a lavatory space, and a toilet assembly inside the lavatory space. The toilet assembly has a toilet bowl and a shroud to support the user during use. The toilet assembly serves as a hybrid toilet to be used as a sitting toilet or as a squatting toilet. The shroud includes an upper edge surrounding an upper opening of the toilet bowl. To accommodate a user sitting position, the upper edge is provided as a toilet seat, and a feet-placing area is provided on a floor segment in front of the toilet assembly. The shroud has two lateral tread portions, one on either side of the toilet bowl. To accommodate a user squatting position, the tread portions are provided as elevated rest-platforms arranged on an intermediate level provided above a floor level and below a toilet seat level.

Abstract: A vacuum bagging system for vacuum bagging a fiber-reinforced polymer component for an aircraft or spacecraft includes a vacuum bagging film or membrane which is configured to cover and seal the component during molding. The vacuum bagging film or membrane is pre-formed, e.g. thermoformed, to a shape or to an external geometry of the component to be molded. A method of vacuum bagging a fiber-reinforced polymer component of an aircraft or space-craft, includes the steps of: arranging a component to be molded in a vacuum bagging assembly for forming a fiber-reinforced polymer component; pre-forming a vacuum bagging film or membrane to a shape or external geometry of the component; and arranging the vacuum bagging film or membrane on or over the component in the vacuum bagging assembly such that the film or membrane form-fittingly covers the component.

Abstract: A system for air conditioning at least one partial region of an aircraft includes an air providing device for providing air to be supplied to a region of the aircraft to be ventilated at a desired temperature and pressure. A supply air duct is connected at a first end to the air providing device. A second end of the supply air duct is connected to an air inlet which opens near the floor into the aircraft region to be ventilated. A control device is set up to ensure that the air provided by the air providing device enters the aircraft region to be ventilated via the air inlet at such a speed that the air is distributed near the floor in the aircraft region to be ventilated and rises at heat sources present in the aircraft region to be ventilated.

Abstract: A method for producing a component from a fibre-reinforced plastic includes the steps of providing a moulding tool having a tool surface, positioning a first layer of a textile semifinished product comprising dry fibres on the tool surface, arranging a second layer of an electrically conductive, resin-permeable grid on the first layer, arranging an uppermost arrangement of layers, sealing the arrangement of layers by a closure device to form a mould, introducing resin into the mould for infiltration of all the layers with the resin and curing and removal of the component.

Abstract: A coupling system has two coupling halves, each having a main body and a closure device arranged therein. The coupling halves can be pressed onto one another in order to release the closure devices and establish a fluid connection. By virtue of the configuration of the seals and of the closure devices, only a coarse tolerance is required for placing the coupling halves on one another.

Abstract: An aircraft has: a cargo hold, a first fire-extinguishing agent container with a fluid-like fire-extinguishing agent, a first line section extending from the first container to the cargo hold, such that the fire-extinguishing agent can flow from the first container into the cargo hold, a controllable valve coupled to the first line section for controlling a flow of fire-extinguishing agent through the first line section, a concentration sensor arranged in the cargo hold for sensing a concentration of the fire-extinguishing agent in the cargo hold, and a monitoring unit. The concentration sensor is coupled to the monitoring unit for transmitting to the monitoring unit a concentration sensor signal representing the sensed concentration of the fire-extinguishing agent in the cargo hold. The monitoring unit is coupled, to the valve for controlling the valve. The monitoring unit is configured to control the valve on the basis of the sensed concentration.

Abstract: A battery core has a positive electrode layer, a separator layer and a negative electrode layer. The separator layer is arranged between the positive electrode layer and the negative electrode layer. The positive electrode layer, the separator layer and the negative electrode layer have nanocellulose fibres. The battery core is folded and forms a cellular structure as a core for a sandwich component. The sandwich component has an upper covering layer, a lower covering layer and a battery core. The battery core is arranged between the upper covering layer and the lower covering layer. A method for producing such a battery core is also described.