FIELD: physics.
SUBSTANCE: true horizon indicator comprises two spherical sealed vessels placed inside the other, between which there is a supporting medium, where the inner vessel is fitted with a magnetic sensor consisting of similarly directed permanent magnets mounted on a flat support attached to the vessel. The indicator is fitted with pitch angle indicator elements and is in a suspended state in the outer vessel, fitted with a roll scale. The inner vessel is filled with air and the flat support with the magnetic sensor therein is mounted in the horizontal centre-line plane, on the axis of which a weight is placed and attached to the lower part of the spherical vessel, on the outer diametrical circle, which coincides with the plane of the support of the magnetic sensor, of which a bright-red line is deposited with thickness of 1.0-2.0 mm. The outer sealed spherical vessel has a working hole with diameter of about 1.5 mm and has a white line with thickness of about 2.0-3.5 mm on the horizontal diametrical circle.
EFFECT: simple design.
4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR MEASURING THE ANGLE OF INCLINATION OF AN OBJECT | 0 |
|
SU705254A1 |
| DEVICE FOR DETERMINATION OF ANGLE ORIENTATION OF OBJECT | 0 |
|
SU1831653A3 |
| FLIGHT DIRECTOR WITH LOGICAL INDICATION OF POSITION AND STEERING OF AIRCRAFT (VERSIONS) | 2006 |
|
RU2331848C2 |
| DEVICE FOR DETERMINATION OF BANK AND PITCH ANGLES | 1983 |
|
SU1313105A3 |
| ELECTRONIC ARTIFICIAL HORIZON | 2017 |
|
RU2664789C1 |
| EXTRA INDICATOR OF PITCH AND/OR VERTICAL SPEED (VERSIONS) | 2014 |
|
RU2567985C2 |
| GYROHORIZON WITH PITCH AND BANK INDICATORS SPACED IN HEIGHT | 2013 |
|
RU2561311C9 |
| TAKE-OFF AND LANDING DISPLAY SYSTEM OF THE AIRCRAFT | 2016 |
|
RU2647344C2 |
| SYSTEM OF INDICATION OF ARTIFICIAL HORIZON | 1993 |
|
RU2032883C1 |
| FLIGHT DIRECTOR DISPLAY | 2011 |
|
RU2474862C1 |
