Abstract: An emergency evacuation slide has an internal energy dissipation characteristic so that the slide is especially suitable for evacuation of persons from a relatively great height. By dissipating the energy internally in the slide rather than by frictional heating of the clothing and skin of the evacuating persons, the danger of skin burns and other injuries to the persons is reduced or avoided. The slide surface of the slide is made up of a plurality of slide modules that each include an elastically elongatable segment, an interconnecting segment, and an anti-slip segment, which are respectively connected together one after another. The anti-slip segment has an upper anti-slip surface with a high coefficient of friction so that the anti-slip segment remains in static frictional contact and moves along with the evacuating person. The bottom surface of the anti-slip segment has a predefined coefficient of friction.

Abstract: The invention relates to a system for removing the heat that is incident upon an aircraft, and especially a supersonic aircraft, during flight. The incident heat is generated by the constant heating effect of aerodynamic friction on the outer skin of the fuselage, by compression heating at the ram or stagnation point and stagnation edges of the aircraft fuselage, and by the heating of external air as it is compressed to cabin pressure. In the present system, the used cabin air is exhausted out of the cabin through a space between the cabin interior panels and the fuselage outer skin, where the airflow absorbs the heat incident through the outer skin and is heated to approximately the temperature of the outer skin. Next, the heated airflow is preferably first filtered through a filter and is then expanded and cooled through an expansion turbine. The output shaft of the turbine can drive a generator to recover useful electrical energy.