Abstract: The present disclosure relates to an aircraft. The aircraft has a primary structural element, which extends along a main axis of the aircraft, and at least one monolithic structural component, which is produced by a three-dimensional printing method. The aircraft also has an aircraft system for carrying out an aircraft-specific function. The at least one monolithic structural component is fixed on the primary structural element by a fixing device, system, means, or mechanism. The monolithic structural component is embodied to accommodate the aircraft system. The disclosure also relates to a method for producing an aircraft.

Abstract: A device for accommodating and deploying at least one payload on a flying machine includes at least one housing. The housing includes at least two opposite first side surfaces which extend over at least a portion of a length of a payload to be accommodated. The payload to be accommodated is releasably held between the two first side surfaces of the housing. The housing is at least partially arranged in a cavity on an outer surface of a flying machine. The cavity includes at least one outwardly open first opening, and the housing can be at least partially moved out of the cavity for deploying and/or receiving the payload to be accommodated.

Abstract: A method for the additive manufacturing of a receptacle for storing and/or transporting a product includes three-dimensionally capturing the external form of the product, compiling a computer-readable data set with information about the captured external form of the product, and additively manufacturing the receptacle. In a computer-controlled manner on the basis of the compiled data set, a modelling material is deposited in layers, liquefied and cured. The receptacle is formed having an internal structure which surrounds a receiving chamber that is adapted to the external form of the product.

Abstract: The present disclosure relates to an aircraft. The aircraft has a primary structural element, which extends along a main axis of the aircraft, and at least one monolithic structural component, which is produced by a three-dimensional printing method. The aircraft also has an aircraft system for carrying out an aircraft-specific function. The at least one monolithic structural component is fixed on the primary structural element by a fixing device, system, means, or mechanism. The monolithic structural component is embodied to accommodate the aircraft system. The disclosure also relates to a method for producing an aircraft.

Abstract: A method for the additive manufacturing of a receptacle for storing and/or transporting a product includes three-dimensionally capturing the external form of the product, compiling a computer-readable data set with information about the captured external form of the product, and additively manufacturing the receptacle. In a computer-controlled manner on the basis of the compiled data set, a modelling material is deposited in layers, liquefied and cured. The receptacle is formed having an internal structure which surrounds a receiving chamber that is adapted to the external form of the product.