Abstract: A shipment packaging for elongate components is provided. Turbine blades must be sent from remote locations of the world to another location. During shipment, the coating of the turbine blades must be protected. The turbine blades are fixed at both ends by means of shipment packaging so that the turbine blades are protected.

Abstract: A shipment packaging for elongate components is provided. Turbine blades must be sent from remote locations of the world to another location. During shipment, the coating of the turbine blades must be protected. The turbine blades are fixed at both ends by means of shipment packaging so that the turbine blades are protected.

Abstract: A shipment packaging for elongate components is provided. Turbine blades must be sent from remote locations of the world to another location. During shipment, the coating of the turbine blades must be protected. The turbine blades are fixed at both ends by means of shipment packaging so that the turbine blades are protected.

Abstract: A shipment packaging for elongate components is provided. Turbine blades must be sent from remote locations of the world to another location. During shipment, the coating of the turbine blades must be protected. The turbine blades are fixed at both ends by means of shipment packaging so that the turbine blades are protected.

Abstract: A power distribution device has a number N1 of conversion devices comprising a respective cascade generator for converting a first part of a mechanical power into a first electrical power with an alternating voltage of constant amplitude and constant frequency, and comprising a respective frequency converter for supplying a second electrical power with the alternating voltage of constant amplitude and constant frequency as a function of a second part of the mechanical power; a number N2 of constant frequency buses for the respective transfer of the electrical power of constant frequency supplied by the at least one conversion device to a number N3 of loads which comprises at least a number N4 of loads to be controlled in terms of their power consumption; and a number N4 of control devices, wherein the respective control device is coupled between the respective load to be controlled and the constant frequency bus and is designed to control the power consumption of the load to be controlled.

Abstract: The present invention relates in to a device for supplying mechanical power to start at least one engine, with a power supply device for supplying electrical power with an alternating voltage and constant frequency; and with a number, N1, of conversion devices for the conversion of the supplied electrical power to a respective mechanical power for a respective engine, wherein a respective conversion device has a cascade starter generator for direct conversion of the supplied electrical power to mechanical power, wherein the cascade starter generator has a first stator, a second stator, a first rotor and a second rotor, the first stator being integrally formed with the second stator and the first rotor being integrally formed with the second rotor. The present invention further relates to an aircraft comprising such a power distribution network and a method for supplying mechanical power to start at least one engine in an aircraft.

Abstract: A shipment packaging for elongate components is provided. Turbine blades must be sent from remote locations of the world to another location. During shipment, the coating of the turbine blades must be protected. The turbine blades are fixed at both ends by means of shipment packaging so that the turbine blades are protected.

Abstract: A power distribution device has a number N1 of conversion devices comprising a respective cascade generator for converting a first part of a mechanical power into a first electrical power with an alternating voltage of constant amplitude and constant frequency, and comprising a respective frequency converter for supplying a second electrical power with the alternating voltage of constant amplitude and constant frequency as a function of a second part of the mechanical power; a number N2 of constant frequency buses for the respective transfer of the electrical power of constant frequency supplied by the at least one conversion device to a number N3 of loads which comprises at least a number N4 of loads to be controlled in terms of their power consumption; and a number N4 of control devices, wherein the respective control device is coupled between the respective load to be controlled and the constant frequency bus and is designed to control the power consumption of the load to be controlled.

Abstract: The present invention relates in to a device for supplying mechanical power to start at least one engine, with a power supply device for supplying electrical power with an alternating voltage and constant frequency; and with a number, N1, of conversion devices for the conversion of the supplied electrical power to a respective mechanical power for a respective engine, wherein a respective conversion device has a cascade starter generator for direct conversion of the supplied electrical power to mechanical power, wherein the cascade starter generator has a first stator, a second stator, a first rotor and a second rotor, the first stator being integrally formed with the second stator and the first rotor being integrally formed with the second rotor. The present invention further relates to an aircraft comprising such a power distribution network and a method for supplying mechanical power to start at least one engine in an aircraft.