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Helicopter Components, Section and System, Summaries of Engineering

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

2019/2020

Available from 12/03/2022

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Helicopter Components, Section and System
Airframe
-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.
FUSELAGE
-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:
1. Two seats in the front.
2. Two seats in the rear facing backward.
3. Three seats in the rear facing forward.
4. Three front seats facing forward in a stadium style seating.
5. Four back seats facing forward in a stadium style seating.
MAIN ROTOR SYSTEM
-is the rotating part of a helicopter which generates lift.
- main rotor systems are classified according to how the main rotor blades are attached and more
relative to the main rotor hub.
Mast- a hallow cylindrical metal shaft which extends upward and sometimes supported by the
transmission.
Hub- it located at the top of the mast and attached the rotor blade.
Two Classification of Main Rotor System:
1. Semirigid
2. Rigid (fully articulated)
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Helicopter Components, Section and System

Airframe

-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.

FUSELAGE

-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:

  1. Two seats in the front.
  2. Two seats in the rear facing backward.
  3. Three seats in the rear facing forward.
  4. Three front seats facing forward in a stadium style seating.
  5. Four back seats facing forward in a stadium style seating.

MAIN ROTOR SYSTEM

-is the rotating part of a helicopter which generates lift.

  • main rotor systems are classified according to how the main rotor blades are attached and more relative to the main rotor hub. Mast - a hallow cylindrical metal shaft which extends upward and sometimes supported by the transmission. Hub - it located at the top of the mast and attached the rotor blade. Two Classification of Main Rotor System:
  1. Semirigid
  2. Rigid (fully articulated)

Semirigid System

-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:

  • Center of Gravity(CG) is below where it is attached to the mast. -With the underslung system, there will be no imbalance, because the underslinging actually makes on blade flap up, one down, and the center of mass for both blades stay at the same location, thus preventing any coriolis effect to take place. Prone to Mast Bumping! -Can cause the rotor flap stops to shear the mast. -Mast bumping is related to how much the blade can flap.

Rigid Rotor System

-Loads are absorbed through bending rather than hinges. -Blade roots are rigidly attached to the rotor hub.

  • No flapping hinges and lead/lag hinges but blades accomodate this by bending.
  • Blades can be feathered. Advantages
  • Not prone to mast bumping.
  • Reduction in weight and drag, and control inputs. Disadvantages
  • Quality of ride in turbulent and gusty Air.

Bearingless rotor system

  • has no bearings and hinges.
  • design relies on the structure of the blade and hub to absorb stresses.

Fully articulated rotor

-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