FIELD: aircraft control systems. SUBSTANCE: compensation-type measuring system uses two transducers of the same type placed in one hermetically sealed chamber and in one working fluid. EFFECT: decreased dimensional and mass characteristics, simplified design and enhanced accuracy. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
PROCESS OF ADJUSTMENT OF GYROSCOPE TUNED DYNAMICALLY | 1988 |
|
RU2065575C1 |
COMPENSATION-TYPE ACCELEROMETER | 1987 |
|
RU2050549C1 |
COMPENSATION-TYPE ACCELEROMETER | 1986 |
|
RU2042955C1 |
ACCELEROMETER | 1979 |
|
RU2041464C1 |
ELECTROMAGNETIC ANGLE-DATA TRANSMITTER OF GYROSCOPE ROTATING ROTOR | 1979 |
|
RU2107261C1 |
PROCESS OF ADJUSTMENT OF GYROSCOPE TUNED DYNAMICALLY WHICH IS PART OF GYROSTABILIZER | 1989 |
|
RU2065574C1 |
DYNAMICALLY TUNED GYRO | 1988 |
|
RU2101679C1 |
METHOD OF MEASURING ROTARY ELEMENT TEMPERATURE OF ROTOR VIBRATION GYROSCOPE | 1985 |
|
RU2120107C1 |
MOMENT DEVICE FOR GYRO | 1986 |
|
RU2129255C1 |
METHOD OF DETERMINATION OF SLOPE OF OUTPUT CHARACTERISTICS OF GYROSCOPE | 1983 |
|
RU2062986C1 |
Authors
Dates
1996-09-20—Published
1992-10-04—Filed