Abstract: A manufacturing method for thermoforming a fiber-reinforced composite laminate with fiber rovings embedded within a thermoplastic matrix includes: mounting fiber rovings to a transport frame, the mounted rovings being arranged to form a support grid layer laterally framed by the transport frame, each roving being mounted on both ends under tension to the transport frame; placing a matrix material layup of thermoplastic material on top of the support grid layer, wherein the tension of the rovings and a density of the support grid layer are configured such that the support grid layer supports the matrix material layup; softening the matrix material layup by heating the support grid layer together with the matrix material layup within a heating station; forming a semi-finished composite laminate by pressing the support grid layer together with the softened matrix material layup; and consolidating the semi-finished composite laminate to form the fiber-reinforced composite laminate.

Abstract: A vehicle cargo compartment, comprising a housing receivable in a vehicle, and at least one latch mounted to the housing for locking a cargo unit in a fixed position. The latch comprises a latch housing mounted to the housing, and at least a first latch claw moveably mounted to the latch housing moveable between a latched and an unlatched position. A latch sensor system comprises a position sensor and a target, the position sensor adapted to detect and generate a latch signal when the target is in the predetermined position. The vehicle cargo compartment can be monitored easily and reliably when the first latch claw is in the latched position due to the position sensor and the target being arranged and adapted such that the predetermined position of the target is detected and the latch signal is generated, when the first latch claw is in the latched position.

Abstract: A ventilation system (10) for installation in an aircraft passenger cabin comprises an air supply pipe (12), which has a plurality of air outlet openings (14) disposed in a distributed manner along its longitudinal axis (L). An air chamber housing (16) is connectable to the air supply pipe (12) at various positions along the longitudinal axis (L) of the air supply pipe, such that air-conditioning air flowing through the air supply pipe (12) is supplyable, through an air outlet opening provided in the air supply pipe (12), into the air chamber housing (16). A connection device (34) is designed to connect the air chamber housing (16) to an air supply device (36) for supplying air-conditioning air into the aircraft passenger cabin.

Abstract: An aircraft fuselage includes an exterior skin; at least one window frame; at least one window package disposed in a breakout of the exterior skin and attached to the at least one window frame; and a plurality of stiffening elements configured to stiffen the exterior skin, wherein at least one of the stiffening elements crosses the at least one window package.

Abstract: An aircraft and system for minimizing the influence of unsteady flow states, wherein the wing has a respective main wing and at least one control flap adjustably arranged relative thereto, an adjusting drive for activating the at least one control flap, and a sensor arrangement for acquiring the setting position of the control flap. The system exhibits at least one arrangement of flow-influencing devices for influencing the fluid flow over the surface segment, a detection device for detecting unsteady flow states acting on the aircraft, and an actuating function connected with the flow-influencing devices to influence the flow in the different segments of a wing, designed so that the latter, based on the unsteady flow states detected by the detection device and setting position of the control flap acquired by the sensor arrangement, actuates the flow-influencing devices so as to minimize the influence of unsteady flow states on the aircraft.

Abstract: The present invention provides a method for producing a fiber composite component, the method comprising arranging a first and a second mold in relation to one another in such a way that these together form a first cavity; laying a fiber material on the first and/or second mold; filling the first cavity with a casting material and solidifying the casting material in order to seal the first and second molds to one another and/or to interconnect them; and infiltrating the fiber material with a matrix and curing the matrix to form the fiber composite component.

Abstract: A modular cabin segment for a vehicle includes a first lateral segment module accommodating a first toilet arrangement with a toilet compartment, a second lateral segment module, and at least one central module, wherein in each case an outer lateral face of the first segment module and of the second lateral segment module is designed to adapt in each case to an inner wall of a cabin of the vehicle so as to correspond to the aforesaid. At least one of the modules includes a cabin attendant seat that on one side is held on the at least one module so that it can be pivoted on an axis. In this manner very good integration of many different functions in the manner of a construction kit is achieved in order to be able to accommodate a greater number of passenger seats elsewhere within the limited space provided in a cabin.

Abstract: A thermally optimised circulation fluid system is proposed which comprises a circulation line, a circulation pump unit and a control unit. The circulation pump unit and the circulation line together form a circulation circuit. The circulation pump unit is configured for transferring an amount of thermal energy directly or indirectly to a fluid located in the circulation line. The control unit is configured for adjusting the amount of thermal energy which is transferrable to the fluid.

Abstract: A high lift system for an aircraft includes a basic body, a flap which is movably mounted on the basic body and has a flap edge, and a retaining element. The high lift system is set up to form a gap between the flap edge and the basic body. The retaining element is mounted on a region of the flap close to the flap edge and extends towards the basic body to restrict the distance between the flap edge and the basic body. The retaining element is preferably configured as a linear attachment means. Consequently, a gap dimension between a flap and a basic body can be influenced to restrict flexing effects during loading of the flap and of the basic body.

Abstract: A passenger service module including a fitting element, an individual ventilation arrangement connected to the fitting element and having at least one air nozzle, a lighting arrangement connected to the fitting element and having at least one reading lamp, and an operating element connected to the fitting element. The operating element includes a touch panel having at least one input field for individually controlling the operation of the air nozzle and/or of the reading lamp.

Abstract: A holding device is provided for fastening passenger seats in a means of passenger transport and a corresponding passenger seating system. The holding device comprises a seat leg fixing element, a sliding element and a rail element. The seat leg fixing element is designed to receive a seat leg of a passenger seat. The sliding element is provided on the opposite side of the holding device to the seat leg fixing element and is designed to be inserted in a seat rail located on the floor of the means of passenger transport. The rail element is provided on the same side as the seat leg fixing element and is designed to receive and fix a sliding element of an additional holding device. The holding device is provided on a front seat leg and the additional holding device is provided on a rear seat leg of a folding passenger seat.

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 furnishing item for a vehicle includes a first wall with an access opening situated therein, a door and an oblong flap. The door is arranged on the first wall so that it is swivable relative to the access opening around a first rotational axis. The oblong flap is arranged on the access opening in a vertical direction parallel to the door, and swivelably arranged on a second rotational axis, which is situated on a side of the access opening lying opposite the first rotational axis, and arranged parallel to the first rotational axis. The door and oblong flap extend from the first rotational axis or second rotational axis to the second rotational axis or first rotational axis and together completely close the access opening in a closed state.

Abstract: A foldable wing for an aircraft includes a base wing having a base wing end region, a wing tip having a connection region, a first engagement means integrated into the base wing, a second engagement means integrated into the wing tip, and a drive mechanism coupled with the wing tip for moving the wing tip relative to the base wing. The first and second engagement means are adapted for engaging each other along a sliding course from a first position, in which the connection region of the wing tip and the base wing end region are in a flush contact to form a continuous wing, up to a second position, in which the first engagement means and the second engagement means disengage. The drive mechanism includes a first movement element and a second movement element at least partially extending in a spanwise direction, and supported in a linear guide each.

Abstract: A luggage system includes a luggage compartment having a base body and a flap which is movable between a closed position and an open position and is configured to make accessible or close an interior space of the base body. The flap includes a first flap element facing the interior space of the base body and a second flap element facing away from the interior space of the base body, wherein an installation space for components which are to be installed in the region of the luggage compartment is provided between the first and the second flap element.

Abstract: The invention relates to a contamination recording apparatus (12) for recording contaminations in a flowing hydraulic fluid (10) to be examined in aircraft (11a), which comprises a conveying device (14) for conveying the flowing hydraulic fluid (10), a light source (34) for exposing the hydraulic fluid (10) flowing in the conveying device (14) to light (46), and a detection device (36) for recording a fraction of the light (46) absorbed by the exposed hydraulic fluid (10), the light source (34) being formed in order to emit light (46) having a wavelength in the near-infrared range. The invention furthermore relates to a hydraulic system (11) equipped with such a contamination recording apparatus (12) and to an aircraft (11a), and also to a method for recording contaminations in a hydraulic fluid (10) flowing in a hydraulic system (11) of an aircraft (11a).

Abstract: An electrical consumer of an aircraft comprises an electric motor and an inverter for producing an alternating voltage for the electric motor. A method for controlling the electrical consumer comprises determining a rotational frequency for the electric motor. The method also includes establishing whether the rotational frequency leads to oscillations in the input current of the inverter which are below a predefined threshold, the oscillations being produced by the inverter when producing a supply voltage for the electric motor, and changing the rotational frequency if it has been established that the rotational frequency leads to oscillations below the predefined threshold.

Abstract: A cabin attendant seat comprises a seat element and a backrest. The backrest is movable relative to the seat element between an upright position, wherein a backrest surface of the backrest extends at an angle of approximately 80 to 100° relative to a seat surface of the seat element, and a folded-back position, wherein the backrest surface of the backrest extends substantially co-planar with the seat surface of the seat element.

Abstract: Device for exhaust air cooling of aircraft air-conditioning systems comprising a bypass channel that bypasses an aircraft air-conditioning system arranged downstream of a ram air channel with a ram air inlet channel portion, and merges into an outlet channel, arranged downstream of the aircraft air-conditioning system, before a discharge opening for exhaust air, a common inlet being provided for the ram air channel and the bypass channel.

Abstract: A seating arrangement in a cabin of an aircraft includes a floor with a first surface area, a furnishing item with a respective boundary surface, which extends in a vertical direction from the cabin floor, and toward which is directed a first surface area, at least two folding seats, and optionally a partitioning system. The folding seats are arranged on the boundary surface of the furnishing item, and set up to be swiveled into a neutral position and use position, wherein an individual located in the first surface area can sit on the at least two folding seats in the use position. At least one of the at least two folding seats is not designed as a flight attendant seat.