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AIT930 Servo-inclinometer with taut-band suspension, stackable for X and Y measurements

Inclinometer AIT930

The AIT935 series is a high precision closed loop gravity referenced servo inclinometer. It is designed for use where overall space is limited. The unit can be stacked to provide dual axis x and y measurements. Models are available in a wide variety of angle ranges. Solder pin terminations are standard.

AIT935 series inclinometers carry the tradition of a long and successful market history for servo inclinometers marketed under the Schaevitz® brand.

More Features

  • Fully self contained and compact – connect to a DC power source and a readout or control device for a complete operating system
  • Extremely rugged, fluid filled, withstands 1500 g shock
  • Extended pins with chamfered housing edge for ease of soldering
  • Laser marked part and serial number
  • Stackable for x and y measurements

Applications

  • Bore Hole Mapping
  • Structural Health Monitoring
  • Continuous Casting Mold Alignment
  • Railway Maintenance Equipment
  • Mobile and Stationary Antenna Aiming

Principles of Operation

Principles of Operation AIT930

The Schaevitz inclinometer is a precision inertial instrument (accelerometer) that responds to the normal component of the gravitational acceleration vector (gravity). Pendulous mass (A) is attached to the torsionally suspended armature of torque motor (C). Stops on either side of the mass (A) limit its travel when the device is not powered. When the power is applied, the pendulous mass (A) automatically moves to its “zero” position.

As the inclinometer is tilted through some angle (θ) along its sensitive axis, mass (A) tries to move in the direction of tilt as a result of a force (torque) applied to the mass by normal component of gravitation acceleration. The resulting change in position of mass (A) is detected by position sensor (B), which produces an error signal output. This DC error signal is fed to a servo amplifier whose output is a DC current coupled to the armature of torque motor (C) through Ro. Current applied to the torque motor armature produces a torque that opposes the gravitational force acting on the mass (A) and moves it back toward its original position. When the torque developed by the servo system output current just balances the torque developed by the gravity vector component acting on pendulous mass (A), the mass no longer moves and is at rest almost in its original position, being displaced by some minute amount that produces the required error signal from position sensor (B). Because the gravity component’s force is exactly equal in magnitude to the torque motor’s output, which, in turn, is directly proportional to the applied current, this current, passed through Ro generates a voltage across Ro that is proportional to the normal component of the gravity vector. The normal component is the product of the essentially constant gravity vector times the sine of angle (θ). Therefore, the output voltage, Eo x across Ro is proportional to the sine of the tilt angle (θ).

Specifications

Performance by Range at 20 °C

Range

 

±1°

±3°

±14.5°

±30°

±90°

Excitation voltage

VDC

±12 to ±18

±12 to ±18

±12 to ±18

±12 to ±18

±12 to ±18

Current consumption

mA (nom.)

±15

±15

±15

±15

±15

Full range output (FRO) (see note 1)

VDC

±5

±5

±5

±5

±5

Output standardisation

% FRO

±1

±1

±1

±1

±1

Output impedance

Ohm (max)

10

10

10

10

10

Output noise

Vrms (max)

0.002

0.002

0.002

0.002

0.002

Non-linearity (see note 2)

% FRO

0.08

0.05

0.02

0.02

0.05

Non-repeatability

% FRO

0.02

0.01

0.002

0.001

0.0005

Resolution

arc seconds

0.1

0.2

1.0

2.0

4.0

Frequency -3 dB

Hz

10

15

30

40

55

Sensitive axis to case misalignment

deg (max)

±0.15

±0.15

±0.25

±0.50

±1.0

Cross axis sensitivity (see note 3)

% FRO

0.1

´0.1

0.1

0.1

0.1

Zero offset (see note 4)

VDC

±0.08

±0.04

±0.04

±0.02

±0.02

Thermal zero shift

% FRO/°C

±0.05

±0.03

±0.01

±0.005

±0.003

Thermal sensitivity

% reading/°C

±0.05

±0.03

±0.01

±0.006

±0.006

 

Environmental Characteristics

Temperature range – operating

18 … +70 °C (0 … 160 °F)

Temperature range - storage

-40 … +70 °C (-40 … 160 °F)

Constant acceleration overload

50 g

Shock survival

1500 g, 0.5 ms, ½ sine

Vibration endurance

35 g rms, 20 Hz to 2000 Hz sinusoidal

Environmental sealing

IP65

Notes:
1. Full Range Output is defined as the full angular excursion from positive to negative, i.e. ±90° = 180°
2. Non linearity is determined by the method of least squares.
3. Cross axis sensitivity is the output of unit when tilted to full range angle in cross-axis.
4. Zero offset is specified under static conditions with no vibration inputs.

Electrical Connections

Pin A

+12 VDC to +18 VDC

Pin B

0 V

Pin C

-12 VDC to +18 VDC

Pin D

output

Pin E

self test

Please note:
The pin connections of new AIT930 differ from the connections of prior model AIT430!

Dimensions

Dimensions of inkinometer AIT930

Dimensions in mm, values in brackets in inch, approx. values. These drawings are for information only and not intended for construction purpose. Please ask for detailed drawings.

Note: Slots and 1-72 tapped holes permit piggyback mounting two units at 90° to each other

Ordering Information

Specify model type with appropriate range e.g.
AIT935-0001-14.5 is a standard inclinometer with a range of ±14.5°