A method and apparatus are provided for indicating the altitude at which an aircraft should fly so the W/d ratio (weight of the aircraft divided by the density of air) more closely approaches the optimum W/d for the aircraft. A passive microwave radiometer on the aircraft is directed at different angles with respect to the horizon to determine the air temperature, and therefore the density of the air, at different altitudes. The weight of the aircraft is known. The altitude of the aircraft is changed to fly the aircraft at an altitude at which is W/d ratio more closely approaches the optimum W/d ratio for that aircraft.
System for indicating fuel-efficient aircraft altitude
02.10.1984
Sonstige
Keine Angabe
Englisch
System for Indicating Fuel-Efficient Aircraft Altitude
NTIS | 1982
|Digital fuel quantity indicating system for aircraft
AIAA | 1984
|New HIGH-ALTITUDE FUEL SYSTEM for AIRCRAFT
SAE Technical Papers | 1941
|New high-altitude fuel system for aircraft
Engineering Index Backfile | 1941
|Indicating System for Aircraft
NTIS | 1971
|