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Turbulence Damping Function Overview

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Questions and Answers

What is the primary function of the turbulence damping function?

To increase the maximum speed of the aircraft

To stabilize yaw motion without external input

To damp structural modes induced by atmospheric turbulence (correct)

To enhance fuel efficiency during flight

Which sensors does the turbulence damping function specifically utilize?

Two Nz accelerometers and one dedicated Ny accelerometer

Three independent Nz accelerometers

Only external wind sensors

One Nz accelerometer and two dedicated Ny accelerometers (correct)

Under what condition does the turbulence damping function become inoperative?

When a failure is detected (correct)

If the autopilot is disengaged

If the aircraft exceeds a speed of 250 kt

When the temperature falls below freezing

What must be true for the turbulence damping function to be available?

<p>The aircraft speed must be greater than 200 kt</p> Signup and view all the answers

Study Notes

Turbulence Damping Function

Dampens structural modes caused by atmospheric turbulence.
Employs Nz accelerometer and two Ny accelerometers.
Computes a turbulence damping command using PRIMs.
Added to elevator and yaw damper commands.
Automatically deactivated upon failure detection.
Manually inhibitied by switching off TURB DAMP pushbutton if comfort is degraded.
Only active under specific conditions:
- Aircraft in flight.
- Aircraft speed exceeding 200 kt.
- Autopilot engaged or normal law active.
- Aircraft within normal flight envelope.

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Description

This quiz covers the turbulence damping function in aircraft, which mitigates structural modes caused by atmospheric turbulence. It discusses the use of various accelerometers, the computation of damping commands, and conditions for its activation. Additionally, it addresses manual deactivation processes and operational parameters.