| 摘要 |
FIELD: aeronautical engineering and space engineering. SUBSTANCE: proposed method includes change of altitude and speed of flight in route and monitoring of supercharging of thin-walled reservoir. Supercharging of reservoirs depends on their strength and resistance of envelope. Change in flight altitude is performed by ratio taking into account limiting altitude of this aircraft, certified data on cargo to be transported and present magnitude of pressure in reservoir. Change in flying speed is performed by ratio taking into account initial ground temperature of air, flying altitude, temperature change linear coefficient depending on altitude, certified data on cargo, present magnitude of pressure in reservoir and present magnitude of barometric pressure in cargo compartment. EFFECT: enhanced reliability of transportation. 3 cl, 6 dwg |
