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An overview of the components and main rotor system of a helicopter. It discusses the materials used in the airframe, the fuselage, and the seating arrangement in the cabin. It also explains the main rotor system, its classification, and the advantages and disadvantages of each type. Additionally, it covers the bearingless rotor system and the fully articulated rotor system.
Typology: Summaries
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-The airframe, or fundamental structure, of a helicopter can be made of either metal, wood, or composite materials, or some combination of the two. Typically, a composite component consists of many layers of fiber-impregnated resins, bonded to form a smooth panel. Tubular and sheet metal substructures are usually made of aluminum, though stainless steel or titanium are sometimes used in areas subject to higher stress or heat.
-it is the outer core of the airframe. -it is an aircraft's main body section that houses the Cabin that holds the CREW, PASSENGERS and CARGO. -fuselage house the engine, the transmission, avionics, flight control and the powerplant. Helicopter Cabin seating arrangement:
-is the rotating part of a helicopter which generates lift.
-Blades are rigidly mounted to the main rotor hub. -Has Flapping hinges: Blades move up and down(one goes up and the other goes down) and Feathering hinges: pitch angle of the blade changes. -No lead/lag hinges. If semirigid rotor system is an underslung rotor:
-Loads are absorbed through bending rather than hinges. -Blade roots are rigidly attached to the rotor hub.
-is found on aircraft with more than two blades and allows movement of each individual blade in three directions. In this design, each blade can rotate about the pitch axis to change lift; each blade can move