DESIGN AND CALCULATION OF ENGINE MOUNTS AND ENGINE NACELLES FOR AIRPLANE WITH TAKE-OFF WEIGHT OF 2000 KG

Abstract

The thesis describes the design and calculation of an engine mount and engine nacelle for airplane with take-off weight of 2000 kg. The thesis describes the analysis of the current state of engine mounts, engine nacelles, fire dams, flexible storage engine airplanes with similar configuration and performance. The next part deals with own design and calculation of a engine mount and nacelle in the program PRO ENGINEER according to official regulations FAR/CS-23. Follows the calculation of the load acting on the engine mount mount, the material analysis and MKP analysis of eight model situations that can occur in flight. Thesis in the end solves the control to the loss of stability and strength of rods.