Pylon mounting assemblies are provided for mounting an engine (e.g., a turbojet engine) to a wing of an aircraft. The pylon mounting assemblies include an upper pylon connection member, and a lower pylon connection box, wherein the upper pylon connection member and the lower pylon connection box respectively include multiple opposed pairs of connection lobes. At least one pair of the connection lobes includes a pin connection to restrict degrees of freedom thereat along an x-axis and a mutually perpendicular z-axis, while at least one other pair of connection lobes includes a connection rod to restrict degrees of freedom thereat along the z-axis.
Узел крепления пилона двигателя самолета к крылу
2018-03-27
Patent
Electronic Resource
Russian
European Patent Office | 2019
УЗЕЛ КРЕПЛЕНИЯ СЪЕМНОГО АККУМУЛЯТОРА ЭЛЕКТРИЧЕСКОГО ТРАНСПОРТНОГО СРЕДСТВА И СПОСОБ КРЕПЛЕНИЯ
European Patent Office | 2016