RCAIDE.Library.Components.Landing_Gear.Main_Landing_Gear

Main_Landing_Gear#

class Main_Landing_Gear(*args, **kwarg)[source]#

Bases: Landing_Gear

Main landing gear component that handles the primary loads during landing, takeoff, and ground operations.

tag#

Unique identifier for the main landing gear component, defaults to ‘main_gear’

Type:

str

units#

Number of main landing gear units in the assembly, defaults to 0

Type:

float

strut_length#

Length of the main gear strut assembly, defaults to 0

Type:

float

tire_diameter#

Diameter of the main gear tires, defaults to 0

Type:

float

wheels#

Number of wheels per main landing gear unit, defaults to 0

Type:

float

Notes

The main landing gear typically carries 80-90% of the aircraft weight and is designed to handle the primary impact loads during landing.

Major Assumptions

  • Symmetrical arrangement about aircraft centerline

  • All units in an assembly have identical properties

  • Load distribution is uniform across all wheels in a unit

Definitions

‘Multi-Bogey’

Configuration with multiple wheels per strut to distribute loads

‘Track Width’

Lateral distance between main gear units, critical for aircraft stability

See also

RCAIDE.Library.Components.Landing_Gear.Landing_Gear

Base landing gear class

RCAIDE.Library.Components.Landing_Gear.Nose_Landing_Gear

Nose gear component that works in conjunction with main gear