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Was (wer) ist BERP rotor - definition
BERP rotor
The BERP rotor blade design was developed under the British Experimental Rotor Programme. The initial BERP rotor blades were developed in the late 1970s to mid-1980s as a joint venture programme between Westland Helicopters and the Royal Aircraft Establishment (RAE), with Professor Martin Lowson as a co-patentee.
rotor blade
![[[Boeing CH-47 Chinook]]](https://commons.wikimedia.org/wiki/Special:FilePath/10th Combat Aviation Brigade Chinooks in action (cropped).jpg?width=200 "[[Boeing CH-47 Chinook]]")
.jpg?width=200 "MD Helicopters 520N NOTAR")
![A [[Bell 205]] with a semirigid rotor and stabilizer bar](https://commons.wikimedia.org/wiki/Special:FilePath/Bell 205 (cropped).jpg?width=200 "A [[Bell 205]] with a semirigid rotor and stabilizer bar")
![The first autogyro to fly successfully in 1923, invented by [[Juan de la Cierva]].](https://commons.wikimedia.org/wiki/Special:FilePath/Ciervas 1st autogiro.jpg?width=200 "The first autogyro to fly successfully in 1923, invented by [[Juan de la Cierva]].")
![[[de Bothezat helicopter]], 1923 photo](https://commons.wikimedia.org/wiki/Special:FilePath/De Bothezat Quadrotor.jpg?width=200 "[[de Bothezat helicopter]], 1923 photo")
.jpg?width=200 "Fenestron on an EC 120B")
![[[Kamov Ka-50]] of the Russian Air Force, with coaxial rotors](https://commons.wikimedia.org/wiki/Special:FilePath/Russian Air Force Kamov Ka-50.jpg?width=200 "[[Kamov Ka-50]] of the Russian Air Force, with coaxial rotors")
ROTARY WINGS AND CONTROL SYSTEM THAT GENERATES THE LIFT AND THRUST FOR A HELICOPTER
Articulated rotor; Main rotor; Helicopter Rotor; Helicopter rotor blade; Drag hinge; Drag hinges; Lead-lag hinge; Rotor blade; Counter-rotating rotor; Stabilizer bar (helicopter); Teetering rotor; Rotor system; Rotor blades
see rotor
Helicopter rotor
ROTARY WINGS AND CONTROL SYSTEM THAT GENERATES THE LIFT AND THRUST FOR A HELICOPTER
Articulated rotor; Main rotor; Helicopter Rotor; Helicopter rotor blade; Drag hinge; Drag hinges; Lead-lag hinge; Rotor blade; Counter-rotating rotor; Stabilizer bar (helicopter); Teetering rotor; Rotor system; Rotor blades
A helicopter main rotor or rotor system is the combination of several rotary wings (rotor blades) with a control system, that generates the aerodynamic lift force that supports the weight of the helicopter, and the thrust that counteracts aerodynamic drag in forward flight. Each main rotor is mounted on a vertical mast over the top of the helicopter, as opposed to a helicopter tail rotor, which connects through a combination of drive shaft(s) and gearboxes along the tail boom.
