FIELD: aviation engineering. SUBSTANCE: system of indication of artificial horizon has immobile aircraft symbol, pitching scale coupled with rotating casing to line of artificial horizon advancing in vertical plane, rolling scale designed in the form of mobile grid-perspective composed of horizontal and radial elements kinematically coupled to rotating casing of pitching scale. Aircraft symbol is fabricated in the form of ring with central point, shortened wing cantilevers and elongated fin. Line of artificial horizon is made contrast in central part and blurred in direction of end sections. Ring element of dark color is mounted on periphery of rotating casing of pitching scale. EFFECT: increased accuracy and safety of piloting. 3 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
GYROHORIZON | 1976 |
|
SU705838A1 |
METHOD FOR INTEGRAL DISPLAY OF FLIGHT SITUATION PARAMETERS | 2019 |
|
RU2722888C1 |
TAKE-OFF AND LANDING DISPLAY SYSTEM OF THE AIRCRAFT | 2016 |
|
RU2647344C2 |
FLIGHT DIRECTOR DISPLAY | 2011 |
|
RU2474862C1 |
ELECTRONIC ARTIFICIAL HORIZON | 2017 |
|
RU2664789C1 |
FLIGHT DIRECTOR WITH LOGICAL INDICATION OF POSITION AND STEERING OF AIRCRAFT (VERSIONS) | 2006 |
|
RU2331848C2 |
FLIGHT DIRECTOR | 2002 |
|
RU2207514C1 |
METHOD OF FORMING PILOTAGE NAVIGATION INFORMATION ON MULTI-FUNCTIONAL INDICATOR FOR PERFORMING LANDING | 2005 |
|
RU2297596C1 |
METHOD OF CONTROL OF AIRCRAFT ON THE APPROACH | 2004 |
|
RU2267747C1 |
METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2011 |
|
RU2478523C2 |
Authors
Dates
1995-04-10—Published
1993-04-28—Filed