Abstract: A conveyor bowl for a vibratory conveyor device includes a main body made of stainless steel and manufactured by primary shaping. The main body has an interface section for coupling to a vibration unit, and a conveyor section for conveying conveyed parts. The main body may be designed as a cast part. The main body may be a precision cast part or an investment cast part. The main body may be made of austenite. The interface section and the conveyor section may be formed in one piece or formed integrally with the main body.

Abstract: The invention relates to a cabin air inlet module (16). The cabin air inlet module (16) comprises a streaming channel body (8). The streaming channel body (8) comprises at least one wall which limits a streaming channel wherein incoming air (5) is supplied to a zone (2) of a cabin (3). The cabin air inlet module (16) comprises an electric heating element (9) which is used for heating the incoming air (5). According to the invention it is proposed that the electric heating element (9) is embodied as a two-dimensional heating element (in particular as a heating paper, a heating web, a heating foil or a heating varnish). The two-dimensional heating element extends along a wall of the streaming channel body (8). The inventive cabin air inlet module (16) is arranged upstream with a small distance (25) from an inlet opening (6) into the zone (2) of the cabin (3). The inventive cabin air inlet module (16) is used for a tempering zones (2) of a cabin (3) of an airplane according to the needs.

Abstract: A conveyor bowl for a vibratory conveyor device includes a main body made of stainless steel and manufactured by primary shaping. The main body has an interface section for coupling to a vibration unit, and a conveyor section for conveying conveyed parts. The main body may be designed as a cast part. The main body may be a precision cast part or an investment cast part. The main body may be made of austenite. The interface section and the conveyor section may be formed in one piece or formed integrally with the main body.

Abstract: A cladding element having a heating layer in a sandwich construction. In the case of a cladding element in a sandwich construction for an interior space of an aircraft, the cladding element includes a core layer and a first cover layer. The first cover layer forms a visible side of the cladding element. An electrically heating layer extends at least across a sub-face of the first cover layer and serves for generating heat for emission through the first cover layer is disposed between the core layer and the first cover layer.

Abstract: The invention relates to a cabin air inlet module (16). The cabin air inlet module (16) comprises a streaming channel body (8). The streaming channel body (8) comprises at least one wall which limits a streaming channel wherein incoming air (5) is supplied to a zone (2) of a cabin (3). The cabin air inlet module (16) comprises an electric heating element (9) which is used for heating the incoming air (5). According to the invention it is proposed that the electric heating element (9) is embodied as a two-dimensional heating element (in particular as a heating paper, a heating web, a heating foil or a heating varnish). The two-dimensional heating element extends along a wall of the streaming channel body (8). The inventive cabin air inlet module (16) is arranged upstream with a small distance (25) from an inlet opening (6) into the zone (2) of the cabin (3). The inventive cabin air inlet module (16) is used for a tempering zones (2) of a cabin (3) of an airplane according to the needs.

Abstract: In a method for manufacturing a sandwich component having a first and a second flat side, in a pre-assembly state all components of the sandwich component in relation to one another are placed in a nominal position: at least one shape-imparting structural layer and a conductor layer having an electrical conductor, and are connected in an assembly step with an adhesive, wherein in the pre-assembly state on both sides of the conductor layer two barrier layers which are vapor-tight are placed as further components and interconnected in such a manner that said two barrier layers enclose the conductor in a vapor-tight manner.

Abstract: A light-emitting composite arrangement for stationary arrangement in an interior of an aircraft is provided. The light-emitting composite arrangement has a base layer, a covering layer and a core portion at least partially provided between the base layer and the covering layer. The covering layer can be a prepreg layer. A lighting device is integrated in the core portion. The covering layer is cured with the lighting device integrated in the core portion.

Abstract: In a method for manufacturing a sandwich component having a first and a second flat side, in a pre-assembly state all components of the sandwich component in relation to one another are placed in a nominal position: at least one shape-imparting structural layer and a conductor layer having an electrical conductor, and are connected in an assembly step with an adhesive, wherein in the pre-assembly state on both sides of the conductor layer two barrier layers which are vapour-tight are placed as further components and interconnected in such a manner that said two barrier layers enclose the conductor in a vapour-tight manner.

Abstract: A light-emitting composite arrangement 1 for stationary arrangement in an interior of an aircraft is proposed, comprising a base layer and a covering layer 2, 3, wherein the covering layer 3 is a prepreg layer, comprising a core portion 4, which is arranged, at least in some areas, between the base layer and the covering layer 2, 3, comprising at least one lighting device 5, which is integrated in the core portion 4, wherein the covering layer 3 is cured with the lighting device 5 ntegrated in the core portion 4.

Abstract: Aircraft panel 1 for an interior of an aircraft, wherein the aircraft panel 1 has a sandwich structure 2, wherein the sandwich structure 2 comprises a core section 4 and a covering section 3 as sandwich layers, wherein the covering section 3 comprises a prepreg layer 6 and wherein the aircraft panel 1 comprises at least one switching element 8 for activating at least one electrical device of the aircraft, wherein at least one switching element 8 is fixed in the covering section 3 by the prepreg layer 6.

Abstract: This disclosure generally pertains to connectors having a signal contact assembly containing a plurality of rod-shaped signal contact members, generally cylindrical dielectric material encasing the sides of the signal contact members and a generally cylindrical conductive shield in contact with the dielectric material. The signal contact assembly along with rod-shaped power contact members are placed in the connector. This combination can be considered to be in the nature of a connector within a connector. The connector can transmit data at 100 Mbps or greater along with power while minimizing the space required for the contacts. The connectors may be generally circular in cross-section.

Abstract: This disclosure generally pertains to circular connectors having a signal contact assembly containing four rod-shaped signal contact members, generally cylindrical dielectric material encasing the sides of the signal contact members and a generally cylindrical conductive shield in contact with the dielectric material. The signal contact assembly along with four rod-shaped power contact members are placed in the connector in an array such that the cluster of signal contact members is offset from the array of power contact members. This combination can be considered to be in the nature of a connector within a connector. The connector provides good electrical performance while minimizing the space required for the contacts.

Abstract: This disclosure generally pertains to connectors having a signal contact assembly containing a plurality of rod-shaped signal contact members, generally cylindrical dielectric material encasing the sides of the signal contact members and a generally cylindrical conductive shield in contact with the dielectric material. The signal contact assembly along with rod-shaped power contact members are placed in the connector. This combination can be considered to be in the nature of a connector within a connector. The connector can transmit data at 100 Mbps or greater along with power while minimizing the space required for the contacts. The connectors may be generally circular in cross-section.