The system of the present application represents a rotor hub for a rotorcraft and a rotorcraft incorporating the rotor hub.
During an airplane mode, the rotorcraft can stop and fold the rotor blades so that the rotorcraft relies upon thrust from the engine for propulsion.
A subsequent step comprises determining the no-wind operating point and the with-wind operating ranges of a special type of rotorcraft on the basis of the operating ranges of the reference rotorcraft.
A signal of the rotorcraft indicative of and proportional to the component is monitored.
The rotor and nacelle tilt of a tiltrotor rotorcraft can be controlled and effected in order to manipulate the yaw orientation and flight mode of a rotorcraft such as a tiltrotor.
The control system includes a stepped mixing linkage (53), such that a selected amount of right-left lateral cyclic output is generated for certain amounts of forward-aft cyclic input.
Some rotorcraft, such as helicopters, have a powered rotary wing or rotor, where the rotor disc can be angled slightly forward so that a proportion of its lift is directed forwards.
Described is a safety device for a rotary-wing aircraft with at least one powered rotor mounted above a central shaft which passes through the airframe roof.
A rotary-wing aircraft with an electric motor mounted along an axis of rotation to drive a rotor system about the axis of rotation.
A torque coupling for a rotor head of a rotary-wing aircraft is configured for rotation with a mast and for causing rotation of an attached yoke.
The invention relates to an adjustable blade profile of the rotor blade of a rotary wing aircraft.
A gyroplane which contains said gearwheel set is likewise proposed.
It combines the advantages of the helicopter and the gyroplane.
The invention relates to a rotor blade (20), in particular for a rotary wing aircraft.
The Rajasthan schedule could start in March next year.
A vibration isolator (20) operative for reducing vibration active on a main rotor (12) of a rotorcraft.
Using this technology will improve the safety of the rotorcraft during operations.
The AWHERO unmanned rotorcraft is designed to the international aeronautical standards.
A rotorcraft having an enhanced configuration in which a simple wing and a propulsive anti-torque system are combined is disclosed.
Hence the name of this class of aircraft heavier than air - rotorcraft.
They are nowadays classified as powered lift types and not as rotorcraft.
Such rotor blades spacing reduces the vibration that is translated into the rotorcraft through the rotor mast.
A method of providing a signal representative of blade vortex interaction (BVI) noise for a multi-blade rotorcraft.
An easily removable and lightweight horizontal stabilizer configured to provide aerodynamic stability for a rotorcraft.
A safety rescue aircraft is provided, which scheme can be adapt to a fixed-wing aircraft and a rotorcraft.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
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