Chapter 6 - Landing Gear Flashcards
Landing Gear Types?
Rubber Bungee
Cantilever Spring
Oleo Pneumatic Strut
Rubber Bungee
- Use Tubular Struts
- Landing forces directed against the turns in the rubber.
Cantilever Spring
- Comprises a tube or strip of tapered spring steel.
- Upper end is attached to the fuselage and the lower end terminates at the axle.
Oleo Pneumatic Strut
- Found on more advanced light aircraft.
- Combination of air and Hydraulic fluid is used to absorb the shock during landing.
- Often just the Nose gear that uses this.
Wheel Bogie?
- Used to fit additional wheels to the landing gear.
- At least 4 wheels per landing leg.
- Mounted to a ‘bogie beam’.
Requires a large amount of space to stow.
Shock Absorbers?
90% of landing shock.
Connected to the wing spars.
- Gas (Nitrogen) inside cylinder acts as spring to absorb loads.
- Hydraulic oil acts to dampener the gas springs during rebound.
Preflight check that should be carried out on the Shock Absorbers?
Fescalized Portion should be checked to see if it has bottomed out:
- Sign of low pressure
- or Fluid leak.
Purpose of:
Oleo Leg
Absorbs loads and dampens recoil
Purpose of:
Wheel Axles
Wheel mounting shaft, allows rotation.
Purpose of:
Bogie
Axles connected by a central bogie beam to support complete wheel assembly.
Purpose of:
Drag Strut
Braces the landing gear against the forward & rear shock loads.
Purpose of:
Upper Sidestay
Braces the landing gear against side motion (Taxing creates the biggest loads of the sides).
Purpose of:
Gear Doors
Provide aerodynamic closure to the landing gear bay.
Purpose of:
Torque Link (Scissor Link)
Prevents rotation of the inner oleo cylinder.
Purpose of:
Free Castoring?
Uses wheel brakes to turn the aircraft