A multi-axis passenger-carrying aircraft comprises: an electrical system; a heat exchange system; a cabin; and an accommodating compartment arranged inside the cabin; wherein the electrical system is arranged inside the accommodating compartment, and wherein the heat exchange system comprises at least an air inlet communicated with the exterior of the cabin, an air outlet communicated with the accommodating compartment, and a cooler with an air inlet end communicated with the air inlet and an air outlet end communicated with the air outlet. In operation, air outside the aircraft may enter the heat exchange system via the air inlet and the cooler via the air inlet end to be cooled by the cooler. The cooled air may be discharged via the air outlet end and then enter the accommodating compartment via the air outlet, providing cool air to the accommodating compartment and dissipating heat from the electrical system.

A display device may include a display panel, and first member, and a second member. The display panel has a first section and a second section. The first member includes an electromagnet, extends parallel to the first section and has a first side and a second side. The first side is oriented a first obtuse angle with respect to the second side. The second member directly contacts the first member, extends parallel to the second section, and has a third side and a fourth side. The third side is oriented a second obtuse angle with respect to the fourth side. The first member is connected through the second member to the second section. The second member is connected through the first member to the first section.

An integrated electronic assembly including a first electronic component defining a receptacle and at least a second electronic component wherein at least a portion of the second electronic component is disposed in the receptacle of the first electronic component, and a method for conserving space in a circuit or on a printed circuit board by integrating a plurality of electronic components so that the plurality of electronic components collectively take up a smaller amount of space on a substrate than the plurality of electronic components would if the plurality of electronic components were not integrated.

A modular planar electrical wiring system for providing a planar electrical wiring according to a desired configuration includes a planar electrical distribution cable, at least one planar electrical appliance embedded in a planar sheet and connectable to the planar electrical distribution cable; and at least one planar connector for connecting a corresponding planar electrical appliance to the electrical distribution cable at any given location therealong according to the desired configuration, to thereby provide a modular planar electrical wiring system having a low height profile. There is also provided a modular power distribution system provided with a power source, an enclosure for a planar power distribution cable, a crimp connector including a control system, and power sources for a planar modular power distribution system.

A kit for manufacturing electronic aircraft control units having different specifications, the units including electronic modules of different types, including avionics platform modules comprising at least an electronic monitoring circuit and an electronic control circuit that are segregated from each other; first protection modules for protecting the avionics platform modules; first extended connection modules; and second protection modules for protecting the extended connection modules; the modules of each type being identical with one another.