Trunnion Link in Aircraft Engineering

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Questions and Answers

What is the primary function of the trunnion link in landing gear systems?

  • To retract the main gear
  • To hold the landing gear in place during flight
  • To stabilize the wing area
  • To transmit shock loads to the aircraft structure (correct)

Where is the trunnion link mounted in relation to the aircraft components?

  • Between the wing area and the fuselage
  • Between the landing gear and the cockpit
  • Between the shock strut and the wing area (correct)
  • Between the main landing gear and the tail

Which part of the trunnion link connects to the shock strut?

  • Drag strut interface
  • Main gear attachment
  • Forward hinge point
  • Aft end, called the trunnion fork (correct)

How does the trunnion link facilitate main gear retraction?

<p>Through its forward and aft hinge points (B)</p> Signup and view all the answers

What is the significance of the shock loads transmitted by the trunnion link?

<p>They must be absorbed by the aircraft structure (A)</p> Signup and view all the answers

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Study Notes

  • The trunnion link connects the shock strut to the wing area of an aircraft.
  • It transmits landing gear shock loads from the drag strut to the aircraft structure.
  • The trunnion link has both forward and aft hinge points, allowing for the retraction of the main gear.
  • The trunnion fork is located at the aft end of the trunnion link and connects to the shock strut.

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