초록 ▼

A computerized system for examining single engine performance capabilities and developing alternate routes/routings for two-engine aircraft in compliance with FAR 121.19 (driftdown, one engine inoperative) such that an attendant loss of altitude will not result in the aircraft dropping below a net f

A computerized system for examining single engine performance capabilities and developing alternate routes/routings for two-engine aircraft in compliance with FAR 121.19 (driftdown, one engine inoperative) such that an attendant loss of altitude will not result in the aircraft dropping below a net flight path altitude and clearance distance with respect to the earth's surface along a given route between a flight originating point and a destination. Included as a part of the computation are the radius of action fuel capabilities which takes into consideration the "maximum continuous thrust", the power demands on the remaining engine, air density-temperature change attendant with altitude loss, and real time wind conditions.

대표청구항 ▼

1. A method for preparing driftdown plans for aircraft, comprising the steps of: (a) developing a first data base defining the height above sea level of terrain at predetermined geographic coordinate locations; (b) storing said first data base in the memory of a digital computer, each height val

1. A method for preparing driftdown plans for aircraft, comprising the steps of: (a) developing a first data base defining the height above sea level of terrain at predetermined geographic coordinate locations; (b) storing said first data base in the memory of a digital computer, each height value entry in said data base being at a predetermined addressable location in said memory; (c) developing a second data base defining driftdown flight performance characteristics of a variety of multi-engine aircrafts upon the loss of power of at least one of said engines for a variety of engine types; (d) storing said second data base in said memory of said digital computer; (e) entering flight specification data, including the type of aircraft, the type of engine on said aircraft, the load factor of the aircraft and the geographic location of a flight origin and a flight destination for a proposed route into said computer; (f) executing a program of instructions in said computer for comparing terrain height information in said first data base related to the routing of the aircraft between said origin and said destination to driftdown altitude in said flight performance characteristics along said proposed route in said second data base; and (g) providing a visual manifestation based on the result of the comparison of alternate landing sites which the aircraft would be capable of reaching, while maintaining a predetermined safe clearance distance above the terrain, in the event the loss of power of at least one engine at predetermined, spaced points along said proposed route. 2. The method for preparing driftdown plans for aircraft as in claim 1 wherein said addressable locations in said memory storing said first data base are addressed as a function of geographic information. 3. The method for preparing driftdown plans for aircraft as in claim 2 wherein said geographic information comprises the longitude and latitude coordinates of predetermined areas of the earth's surface. 4. The method for preparing driftdown plans for aircraft as in claim 1 and further including the steps of: (a) entering into said computer data relating to wind conditions at said predetermined point; (b) computing from the data contained in said second data base the amount of fuel remaining; (c) calculating the range of the aircraft based upon said wind conditions and the amount of fuel remaining; and (d) determining whether a manually entered proposed landing site is within said range of the aircraft.