MT-Propeller Composite Blade |
Structural Foam Composite Blade |
---|---|
12% lower, app 143 lbs. (65 kg) Typical blade with 88,5" diameter |
app. 160 lbs. (72 kg)
Typical blade with 88,5" diameter |
30% lower, app 17760 lbsin2(5,2 kgm2) Typical blade with 88,5" diameter |
app. 23225 lbsin2 (6,8 kgm2)
Typical blade with 88,5" diameter |
45% higher vibration damping coefficient equals to 0,0396 - therefore no grond or flight RPM restrictions | A vibration damping coefficient of 0,0216 Ground RPM - limitations and possible in flight vibration limitations |
2 inch wide Nickel Cobalt erosion sheath, bonded on the blade, protects it against rain, hail, ice, sand and stones. | Less erosion protection due to the small nickel erosion sheath (less than 1 inch), but increased maintenance effort due to complex design. |
EXTREME LOW vibration due to high damping coefficient and lower moment of inertia Is your propeller as smooth? Three bladed MT prop MTV-9 on a Cessna 182P in FL85 at 135 KTAS. |
HIGHER vibration levels as a foam core has no vibration damping at all plus the higher inertia moment. Close to metal. |
Unlimited because of the reparability, maintainig original dimensions during service life. 100 000 blades with more than 180 Mio flying hours |
Same service life expected. No long time experience available. Expensive overhaul costs. |
Performance improvement Special High Lift State of the art aerodynamic airfoils invented in close cooperation with the German aeronatic research institute DLR for better take off/climb and same cruise |
Performance in take off and climb are critical due to thin airfoils which tends to stall partially due to sharp airfoil leading edge. |
Unlimited replacements of erosion sheath. Rebuilding of blad tips. Maintaining always original blade dimensions. |
Ground strike blade rapair limits unknown. Hub replacement mandatory. |
Single piece low maintenance hub. No ADs, No re-greasing needed between TBO. In field blade replacement on wing possible. |
2 piece hub with stress rising crack initiating grease fittings in the highest stressed hub area (blade bearing). Lots of ADs on those hubs. No on wing blade replacement possible. |