TWO-BLADED MAIN ROTOR

to be installed on helicopters with up to
50 kg take-off mass and rotor diameter
of 2600 mm (102.36")

OVERVIEW

The state-of-the-art carbon main rotor blades are produced with latest carbon multi- cross-layer technology using a curing oven.

The highly efficient carbon main rotor blades have been designed by gluing an all-metal edging into the leading edge. The blades are fully interchangeable and carry a life-limit of 2,600 hours.

Due to the industrial production process the main rotor blades have long-life endurance, the enhanced aerodynamic performance, the increased wear resistance under severe weather conditions. The blades have superior behavior under extreme maneuvers.

SPECIFICATIONS

Length:

1230 mm

Width:

76-38 mm

Thickness:

12.5-4.5 mm

Root thickness:

12.5 mm

Mounting Hole Size:

6 mm

Rotation:

Left (CCW) or right (CW)

Twist:

10°

Material:

Carbon fiber (prepreg), metal

Max. RPM:

1300

Weight:

0.42 kg

MTOW (2 blades):

50 kg

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