Turbulence Damping Function Overview

Choose a study mode

Play Quiz
Study Flashcards
Spaced Repetition
Chat to Lesson

Podcast

Play an AI-generated podcast conversation about this lesson

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 (B)</p> Signup and view all the answers

Flashcards

Turbulence Damping Function

A function that reduces structural vibrations caused by air turbulence.

Sensors for Turbulence Damping

The system uses accelerometers (Nz and Ny) to detect turbulence.

Turbulence Damping Command

A signal generated by the PRIMs, controlling elevator and yaw damper.

Automatic Monitoring of Turbulence Damping

The system automatically checks for malfunctions during operation.

Signup and view all the flashcards

Manual Inhibition of Turbulence Damping

Pilot can deactivate the system if comfort is reduced.

Signup and view all the flashcards

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.

Studying That Suits You

Use AI to generate personalized quizzes and flashcards to suit your learning preferences.

Quiz Team

More Like This

Turbulence and Airmass Fronts Quiz
12 questions
Final Closure Models for Turbulence
5 questions

Final Closure Models for Turbulence

CompliantLeaningTowerOfPisa avatar
CompliantLeaningTowerOfPisa
Wake Turbulence Safety Guidelines
6 questions
CFD Turbulence Modeling Overview
12 questions

CFD Turbulence Modeling Overview

WellBeingSolarSystem3950 avatar
WellBeingSolarSystem3950
Use Quizgecko on...
Browser
Browser