Systems Flashcards
How likely is a minor failure
Probable
How likely is a major failure
Remote
How likely is a hazardous failure
Extremely remote
How likely is a catastrophic failure
Extremely improbable
What is “safe life”
Life given to a aircraft in which it will not suffer a catastrophic failure
What is fail safe
A failure of a particular part is compensated by an alternative part for a limited time
Limited time is until next periodic inspection
Disadvantage is it’s heavy
What is a damage tolerant structure
Spreading load over a large area
Damage can be detected during normal inspection cycles before failure occurs
What is a stress
Internal force per unit area inside a structural component as a result of external loads
What is strain
Deformation caused by stress on a material
% dimension of original
What are the 4 types of stress
Tension (traction)
Compression
Torsion
Shear
What strain is placed on a component during bending
Compression inside of bend
Tension outside of bend
Shear in middle (@spar)
It is a combined load
What is torsion
Twisting
Tension is at outer edge
Compression in the centre
Shear cross structure
What is elasticity
A material can elongate then return to original shape
What is plasticity
Material permanently reform
What is a stringer used for
To prevent compression load on outside of skin buckling
What is buckling
Occurs to thin sheet materials when subject to compressive forces
What are dynamic loads
Built up quickly due to changes in flight conditions
What are static loads
Usually Constant and build up slowly
I.e loading up with fuel
Where experiences the largest bending moment
Wing root
On ground = static force is main gear on wings
In air = upward forces by lift
Max on empty wings
How to reduce wing loading / stress
Outboard ailerons locked it at same time as flap retraction
Aileron upwards = pushes wing down at High speeds
Fuel in winds
Engines on wings
What is a cyclic load
Repetitive load placed on and off
Causes structure to fail quicker than static load
What determine the number of cycles to failure
Amplitude of the load
What is design load limit
Max load designer expects the aircraft to experience in service
Based on 2.5g for transport aircraft
Design ultimate load
Safety factor applied to design load limit
Must withstand design ultimate load without collapse
Safety factor of 1.5 added to design load limit