An aircraft motive flow line includes an outer tube made out of a first material and an inner tube extending longitudinally inside the outer tube. The inner tube is made out of a second material having a thermal conductivity coefficient lower than that of the first material. The first material has a strength coefficient greater than that of the second material. The inner tube is sized and held in position relative to the outer tube so as to define a gap between an exterior of the inner tube and an interior of the outer tube. A port fluidly connects an interior of the inner tube to the gap.
Aircraft motive flow line
21.09.2021
Patent
Elektronische Ressource
Englisch
Electric taxi motive control system and method of an aircraft
Europäisches Patentamt | 2017
|