Source code for RCAIDE.Library.Components.Landing_Gear.Main_Landing_Gear
# RCAIDE/Compoments/Landing_Gear/Main_Landing_Gear.py
#
# Created: Nov 2024, M. Clarke
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# IMPORT
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# RCAIDE imports
from .Landing_Gear import Landing_Gear
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# Main_Landing_Gear
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[docs]
class Main_Landing_Gear(Landing_Gear):
"""
Main landing gear component that handles the primary loads during landing, takeoff,
and ground operations.
Attributes
----------
tag : str
Unique identifier for the main landing gear component, defaults to 'main_gear'
units : float
Number of main landing gear units in the assembly, defaults to 0
strut_length : float
Length of the main gear strut assembly, defaults to 0
tire_diameter : float
Diameter of the main gear tires, defaults to 0
wheels : float
Number of wheels per main landing gear unit, defaults to 0
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
"""
def __defaults__(self):
"""
Sets default values for the main landing gear attributes.
"""
self.tag = 'main_gear'
self.units = 0. # number of main landing gear units
self.strut_length = 0.
self.tire_diameter = 0.
self.wheels = 0. # number of wheels on the main landing gear