FIELD: aviation instrumentation engineering. SUBSTANCE: accelerometer has case accommodating movable part of sensor mounted on flexible hanger 2 and provided with pendulum 1. The latter mounts torque sensor coils 3 and movable plates 6 of differential capacitive position sensor. Movable part carries magnets 4 of torque sensor and fixed plates 5 of position sensor. Surface area of movable plate 6 of position sensor mounted above line parallel to hanger line and crossing geometric center of movable part equals surface area of same plate 6 of this sensor placed below mentioned line. Geometric center on surface of each movable plate 6 of position sensor is aligned with center of symmetry of torque sensor coils. EFFECT: improved design. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
ACCELEROMETER | 1984 |
|
RU2120641C1 |
METHOD OF REDUCTION OF STRESS MOMENT IN PENDULOUS ACCELEROMETER | 1990 |
|
RU2112987C1 |
ACCELEROMETER | 1981 |
|
RU2120638C1 |
ACCELEROMETER | 1985 |
|
RU2045761C1 |
ACCELEROMETER | 1982 |
|
RU2120639C1 |
ACCELEROMETER | 1990 |
|
RU2120642C1 |
ACCELEROMETER | 1990 |
|
RU2063047C1 |
ACCELEROMETER | 1985 |
|
SU1840346A2 |
ACCELEROMETER | 1983 |
|
RU2046346C1 |
ACCELEROMETER | 1983 |
|
RU2120640C1 |
Authors
Dates
1997-07-27—Published
1986-11-03—Filed