By V. Shmyrov, et al.,
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Additional info for Airplane Power Plants Systems Designing (synopsis)
These crystals clog fuel filters, equipment, pipelines. Solubility of water in petrol is higher, than in kerosene. However 61 negative effect of water in the fuel system on kerosene is stronger, than in the fuel system on petrol. It is caused by the greater viscosity of kerosene. Kerosene keeps the water educed from a solution in a suspension. In petrol water rapidly falls out by gravity. Besides with increase of viscosity, water can hardly been separated in fuel filters. To fight against an ice formation in the fuel system, the following methods are applied.
Besides the distance from the engine center of mass up to shock absorbers is more, hence, the loads, which act to shock absorbers, are more too. The struts–dampers are installed in the engine mounts for shockabsorption. Sometimes the shock absorbers are installed in both attachment fittings of engine mounts to engine and in attachment fittings of engine mounts to aircraft structure. Thus the complete separation of the aircraft structure from vibrations of engine is reached (ref. Fig. 4). At oscillations around y and z axes (normal to propeller axis) there is a gyroscopic precession oscillation, which is very harmful to propeller and to rotating rotor of engine.
8, b) in addition to the beam 1 there are rods 2. These rods should not prevent engine from thermal expansions. 38 a b Fig. 8. 2. Engine Mounts of Turboprops Attachment of turboprops at airplanes is usually performed by threedimensional frame structures. Its airframe can be truss (An-10, An-24) or truss-girder (Il-18). The engine mounts of turboprops (Fig. 9) consists of eight rods. They are made of high-strength alloyed steel. The rods are provided with regulated ends and check holes. These check holes serve to control minimal required number of turn of thread.
Airplane Power Plants Systems Designing (synopsis) by V. Shmyrov, et al.,