Flight Data Technologies analyzes the collected flight data to improve the calculations of aerodynamic characteristics, increase the efficiency, environmental friendliness and safety of the flight. Two options are available:
- Flight Fuel Calculation consumed in flights for each aircraft and for the entire fleet of the airline, for analysis and further procedures to reduce fuel consumption;
- Optimal Values of Aircraft Parameters calculation of the optimal values of aircraft flight parameters to optimize CO2 emissions and noise.
1.Flight Fuel Calculation at a given distance.
Take-off weight, route and balance of the aircraft.
Initial data:
- Determination of altitudes and flight speeds at which the minimum fuel consumption is guaranteed during level flight at a given range;
- Determination of fuel consumption at a given altitude, flight speed and duration of a horizontal section;
- The results of comparing the values of the parameters of the performed horizontal flight with the calculated optimal values;
Received results:
- Recommendations for choosing a flight profile;
- Simplification of engineering and navigational calculations;
- Analysis of the optimazation of the choice of the values of the horizontal flight parameters at a distance;
- Fuel economy when performing a standard flight plan at a distance of 4000 km with a maximum takeoff weight of up to 1 t (with a flight intensity of 100 flights / month - savings of 100 t of fuel);
2. Calculation and correction of the optimal values of aircraft flight parameters for a given range
Maintaining optimal aircraft operation modes helps to reduce CO2 and noise.
Initial data:
- Flight Plan;
- Current values of flight parameters, considering priorities;
- Weight and centering of the aircraft;
- Aerodynamic characteristics of a particular aircraft, engine characteristics;
Received results:
- Optimal flight profile with MACH number and flight speed required to ensure minimum fuel consumption;
- Detailed tables of cruise flight parameters, considering its real conditions (current flight weight, balance and temperature);
- Creation of the current values of flight parameters recommended to ensure the minimum fuel consumption and their registration for comparison with already performed flights;
