FIELD: physics.
SUBSTANCE: integrated system of backup devices has an information sensor unit 1, an information processing unit 2, a display unit 3, a device 4 for changing frames, a device 5 for inputting pressure values, a converting device 6, two devices 7, 9 for controlling a converter 8 which converts the turning angle of a shaft to a digital code and a switching device 10. During takeoff and landing, the pilot selects frame display corresponding to the given flight conditions, and also enters the value of atmospheric pressure at the altitude of the takeoff strip of the aerodrome to determine the true flight altitude.
EFFECT: broader functional capabilities.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
FLIGHT SIMULATING PILOTAGE COMPLEX | 2006 |
|
RU2310909C1 |
INTEGRATED ONBOARD EQUIPMENT SET OF DIFFERENT ARCHITECTURE | 2015 |
|
RU2592193C1 |
HELICOPTER AVIONICS COMPLEX | 2021 |
|
RU2771577C1 |
INTEGRATED SYSTEM OF RESERVE DEVICES FOR AIRCRAFT | 2017 |
|
RU2682134C1 |
COMPLEX ELECTRONIC DISPLAY SYSTEM FOR LIGHT MULTI- PURPOSE AIRCRAFT | 2002 |
|
RU2219108C1 |
AIRCRAFT TRAINING COMPLEX | 2004 |
|
RU2250511C1 |
AIRCRAFT ELECTRONIC DISPLAY COMPLEX | 2004 |
|
RU2264953C1 |
AIRPLANE AND HELICOPTER INTEGRATED STANDBY EQUIPMENT SYSTEM | 2006 |
|
RU2337315C2 |
FLIGHT DISPLAY SYSTEM AND COGNITIVE FLIGHT DISPLAY FOR SINGLE-ROTOR HELICOPTER | 2012 |
|
RU2497175C1 |
LIGHT SUPERSONIC MULTI-PURPOSE AIRCRAFT | 2004 |
|
RU2271305C1 |
Authors
Dates
2012-09-20—Published
2011-01-24—Filed