Airframes & Systems
T1, T2a
T1, T2a
Ab wann super?
Ab 560'000 kg or more
Super to super
4 NM
Super to heavy
6Nm and 4 minutes
Super to medium
8 NM and 3 minutes
Super so small
10 NM
Heavy to Heavy
4 Nm
Heavy to Medium
5 NM and 2 minutes
Heavy to light
6 NM and 3 minutes
Medium to heavy
3 NM
Medium to medium
3 NM
Medium to light
5 NM and 3 minutes
light to heavy, medium and light
3 NM
T/O or landing after a heavier aerplane has to be
delayed by 3 minutes
Take of after a heavier aeroplane in opposite runway direction ?
light/medium behind a heavy => 2 minutes light/medium behind super => 3 minutes
Separation minima departing aircraft Super to heavy ?
2 min
Separation minima departing aircraft Super to light?
3 minutes
Separation minima departing aircraft Super to medium ?
3 minutes
Separation minima departing aircraft: Heavy to medium ?
2 minutes
Separation minima departing aircraft: Heavy to light?
2 min
Separation minima departing aircraft: medium to light?
2 minutes
Was ist was?
vgl. Antwort
3 main assemblies
1. Airframe 2. Power plant 3. Equipment => All Systems (hydraulic, Oxygen )
fuselage
Flugzeugrumpf
Fixed wing airplanes can be divided into categories
1. Wing position 2. Tail plane design 3. Type of landing gear
most aeroplanes are monoplanes with
low or high cantilever wings
tails usually?
tail configuration or canard configuration (horizontal stabilizer vor dem Cockpit)
landing gear usually?
fixed or retractable TRICYCLE ( Nicht unter dem Flügel, sondern am fuselage) landing gear
Stress
Wiederstand; applied per unit area of surface=> internal force inside a structural member => resists deformation N/mm^2 or PSI square Inch
Strength
Strength is ability to withstand stress without failure => the maximum stress it can withstand at failure
Stregth to density ratio (specific strength)
specific strength is material strength divided by its density
Strain
deformation of a structural part is called strain and is expressed as ratio of the deformed structure to the non deformed structure
6 Major stresses
Tension 2. Compression => 3. bending 4. Shear 5. Torsion 6. Buckling
Tension
tends to pull part ==> Zieht an etwas Auseinanderziehen
compression
zusammendrücken == > Landung Gear => Feder => Gewicht Flugzeug
shear
2 Platten sind miteinander verbunden => man zieht an beiden => one layer of a material to slide over an adjacent layer
Torsion
Moment => Stossen und ziehen ==> when parts are twisted => results fromm a moment
Torsion strength
torsion strength of material is its resistance to twisting (drehen)
bending
==> Combination of compression and tension ==> verbiegen => Flügem ==> Grösste Kraft bei einem beam (Balken) is at its attachment (Befestigung) => the material of beam should be located where the stress and resulting strain are high
Buckling
A320 Lufthansa => compressing structure with length combined with a small thickness ==> Klinking ( ineinander drücken , Dose ineinader stampfen)
Klinking
result of buckling
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Cartes-fiches
Super to super
4 NM
Super to heavy
6Nm and 4 minutes
Super to medium
8 NM and 3 minutes
Super so small
10 NM
Heavy to Heavy
4 Nm
Heavy to Medium
5 NM and 2 minutes
Heavy to light
6 NM and 3 minutes
Medium to heavy
3 NM
Medium to medium
3 NM
Medium to light
5 NM and 3 minutes
light to heavy, medium and light
3 NM
T/O or landing after a heavier aerplane has to be
delayed by 3 minutes
Take of after a heavier aeroplane in opposite runway direction ?
light/medium behind a heavy => 2 minutes light/medium behind super => 3 minutes
Separation minima departing aircraft Super to heavy ?
2 min
Separation minima departing aircraft Super to light?
3 minutes
Separation minima departing aircraft Super to medium ?
3 minutes
Separation minima departing aircraft: Heavy to medium ?
2 minutes
Separation minima departing aircraft: Heavy to light?
2 min
Separation minima departing aircraft: medium to light?
2 minutes
