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Functionality of a
Landing Gear Suspension
Bazil M H
S5 AERO
What is a landing gear suspension?
• It is the part of landing
gear which absorbs the
impact energy during
landing and provides a
smooth touchdown.
suspension
Parts of oleo strut
• An oleo strut consists of the following
components.
Outer cylinder
Inner cylinder
Tapered metering pin
Wheel axle
Servicing valve
Torque links
Parts of oleo strut
• Tapered metering pin :- used for controlling
the rate of flow of hydraulic fluid through the
orifice.
• Wheel axle :- Provision for connecting aircraft
wheels.
• Servicing valve :- Provides a means for filling
hydraulic fluid or air.
• Torque links :- It is provided for keeping the
piston and wheels aligned.
Functioning
• A shock strut or oleo strut is constructed of
two telescoping cylinders which that are closed
on external ends.
• The upper cylinder is fixed to the aircraft and
the lower cylinder is free to slide in and out of
the upper cylinder.
• Two chambers are formed.
Functioning
• The lower chamber is always filled with hydraulic
fluid and the upper chamber is filled with
compressed air or nitrogen.
• An orifice is located between the two cylinders.
• During landing, the inner cylinder is moved
upward and the hydraulic fluid in the lower
chamber moves to upper chamber through the
metered orifice, which causes heat.
• This heat is the converted impact energy.
THANK YOU

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Landing Gear Suspension Function Explained

  • 1. Functionality of a Landing Gear Suspension Bazil M H S5 AERO
  • 2. What is a landing gear suspension? • It is the part of landing gear which absorbs the impact energy during landing and provides a smooth touchdown. suspension
  • 3. Parts of oleo strut • An oleo strut consists of the following components. Outer cylinder Inner cylinder Tapered metering pin Wheel axle Servicing valve Torque links
  • 4. Parts of oleo strut • Tapered metering pin :- used for controlling the rate of flow of hydraulic fluid through the orifice. • Wheel axle :- Provision for connecting aircraft wheels. • Servicing valve :- Provides a means for filling hydraulic fluid or air. • Torque links :- It is provided for keeping the piston and wheels aligned.
  • 5. Functioning • A shock strut or oleo strut is constructed of two telescoping cylinders which that are closed on external ends. • The upper cylinder is fixed to the aircraft and the lower cylinder is free to slide in and out of the upper cylinder. • Two chambers are formed.
  • 6. Functioning • The lower chamber is always filled with hydraulic fluid and the upper chamber is filled with compressed air or nitrogen. • An orifice is located between the two cylinders. • During landing, the inner cylinder is moved upward and the hydraulic fluid in the lower chamber moves to upper chamber through the metered orifice, which causes heat. • This heat is the converted impact energy.