BELL 505 Mechanic's Guide
  • Welcome!
  • 🚁System Descriptions
    • Introduction
    • Airframe Systems
      • Dimensions and Areas
      • Fuselage
        • Forward Fuselage
        • Mid Fuselage
        • Aft Fuselage
        • Roof
        • Tailboom
      • Stabilizers
      • Landing Gear
      • Equipment/Furnishings
      • Fire Protection (Fire Extinguishing)
      • Doors
      • Windows
      • Environmental Control
        • Distribution
        • Avionics Fans
        • Heating
      • Ice and rain protection (Air intakes)
    • Integrated Avionics Systems
      • Systems Integration and Display
      • Indicating/Recording Systems
        • Instruments and Control Panels
        • General Computers
        • Central Warning System
        • Central Display System
      • Communications
      • Navigation
        • Dependent Position Determining
    • Main Rotor
      • Main Rotor Hub and Blade Assembly
      • Rotating Controls
      • Main Rotor Indicating
    • Main Rotor Drive
      • Engine/Gearbox Couplings
      • Mast Assembly
      • Transmission Assembly
      • Transmission Oil
      • Mounts and Attachments
      • Main Rotor Drive Indicating
    • Tail Rotor
      • Tail Rotor Hub and Blade Assembly
      • Rotating Controls
    • Tail Rotor Drive
      • Shafts
      • Gearbox
      • Tail Rotor Drive Indicating
    • Flight Control Systems
      • Rotor Flight Controls
        • Dual Controls Kit
        • Collective Control System
        • Cyclic Control System
        • Anti-torque Control System
        • Servo-Control System
      • Hydraulic Power
    • Fuel
      • Storage
      • Distribution
      • Fuel Indicating
    • Power Plant Systems
      • Power Plant
      • Air
      • Exhaust
      • Oil
      • Engine Control
      • Ignition
    • Electrical Systems
      • Electrical Power
        • DC Generation
        • External Power
        • DC Electrical Load Distribution
        • Multipurpose Equipment
      • Lights
  • 🪛Line Maintenance
    • Overview of Line Maintenance
    • Servicing
      • Replenishing and Depleting
        • Filling the hydraulic system with fluid
        • Draining fluid from the hydraulic system
      • Lubrication
        • Lubricating the main rotor grips
        • Lubricating the trunnion bearings
        • Lubricating the pillow block assemblies
        • Lubricating the duplex bearing
        • Lubricating the needle bearings
        • Lubricating the pitch change mechanism
        • Lubricating the crew seat positioning mechanism
      • Clean and Surface Protection
        • Rotor blade - Erosion tape replacement
        • Flushing the hydraulic system
      • Inspection
        • 50 flight hours/1 year inspection
        • 100 flight hours inspection
        • 100 flight hours/6 months inspection
        • 100 flight hours/1 year inspection
        • 100 flight hours/18 months inspection
        • 150 flight hours inspection
        • 200 flight hours inspection
        • 300 flight hours inspection
    • Test and Checks
      • Power Assurance Check (PAC)
      • Checking the fluid level of the hydraulic system
      • Flame Out Protection System (FOPS) test
      • Testing the operation of the hydraulic system
      • Testing operation of audio integration system
      • Testing operation of speech communication
      • Testing operation of central warning systems
    • Fault Isolation
      • Crew Alerting System (CAS) Messages
        • WARNING Messages
          • BATTERY HOT
        • CAUTION Messages
        • ADVISORY Messages
        • STATUS Messages
      • System Failures
    • Removal/Installation
      • Electrical Power
        • Installing the ground power unit (GPU)
        • Removing the ground power unit (GPU)
      • Equipment/Furnishings
        • Removing the crew seats
        • Installing the crew seats
      • Hydraulic Power
        • Installing the hydraulic power unit
        • Removing the hydraulic power unit
        • Replacing the HRFM filter element
        • Restoring/replacing the hydraulic pressure filter element
        • Removing the hydraulic pump
        • Removing the pump adapter assembly
        • Installing the pump adapter assembly
        • Installing the hydraulic pump
      • Main Rotor
        • Removing the NR sensor
        • Installing the NR sensor
    • Standard Repairs
      • Main Driveshaft
      • Air Intake
  • 🔧Base Maintenance
    • Overview of Base Maintenance
    • Servicing
      • Adjust, align and calibrate
      • Inspection
    • Function Test
    • Fault Isolation
    • Removal/Installation
    • Major Repairs
  • 🧰Component Interim Maintenance
    • Overview of Component Interim Maintenance
    • Time Limits
    • Component Interim Inspections
  • ⚙️Component Restoration (Overhaul)
    • General Information
    • Main Rotor Hub Assembly
      • Dimensions and Areas
      • Maintenance Planning Information
      • Tools and Workaids
      • Disassembly
      • Cleaning and Paint Removal
      • Inspections
        • Conditional Inspection
        • Non-Destructive Inspections
      • Repair
      • Finishing
      • Assembly
    • Swashplate and Support Assembly
    • Mast Assembly
    • Transmission Assembly
    • Freewheel Assembly
    • Tail Rotor Hub Assembly
    • Tail Rotor Gearbox
Powered by GitBook
On this page
  • Main driveshaft
  • Freewheel assembly
  • Operation
  1. System Descriptions
  2. Main Rotor Drive

Engine/Gearbox Couplings

PreviousMain Rotor DriveNextMast Assembly

Last updated 1 year ago

The engine/gearbox couplings system transmits rotational power from the engine to the mast and transmission assembly system. It is a flexible coupling that adjusts to and accommodates for the constant movement of the mast and transmission system as it moves due to changing flight attitudes and buffeting loads. During autorotation, it disengages the engine from the drive train so that the main rotor system can become the rotational power source for the mast and transmission assembly system and the tail rotor system.

The system of the engine/gearbox couplings has the components that follow:

Main driveshaft

The main driveshaft assembly is of a KAflex-type that has an assembly of four steel Flex frames on both ends of a hollow tubular steel shaft. The Flex frames are attached together and to the flanges of the shaft with bolted joints. At the forward end of the main driveshaft assembly, the Flex frame assembly connects to the input quill at the rear of the of the transmission assembly, and at the aft end of the main driveshaft assembly, the Flex frame assembly connects to the output shaft of the freewheel assembly.

Freewheel assembly

The forward end of the freewheel assembly attaches to the aft end of the main driveshaft, and the aft end of the freewheel assembly attaches to the forward driveshaft assembly of the tail rotor drive system.

The freewheel assembly includes the primary components that follow:

  • Input shaft

  • Clutch assembly

  • Output shaft

  • Housing assembly

The forward end of the freewheel assembly attaches to the aft end of the main driveshaft, and the aft end of the freewheel assembly attaches to the forward driveshaft assembly of the tail rotor drive system.

The splines of the input shaft engage with the engine Reduction Gear Box (RGB) from which it receives power during normal operation. When receiving power from the RGB, the sprags in the clutch assembly move to cause power to be transmitted from the input shaft to the output shaft. The output shaft in turn transmits power both aft and forward.

During autorotation, the RGB does not supply power to the freewheel assembly. When not receiving power from the RGB, the sprags in the clutch assembly move to disengage the input shaft from the output shaft which removes the RGB from the drive train. Removing the RGB from the drive train allows the main driveshaft, now being powered by the main rotor, to provide power to the tail rotor.

The housing assembly serves as a casing and an oil sump for the lubrication of the freewheel assembly. The transmission oil system supplies pressurized oil for the lubrication of the freewheel assembly. The housing assembly also has mount points for the components of the freewheel indicating system.

Operation

During normal operation the freewheel assembly receives power from the engine and distributes it to the main driveshaft assembly and to the forward driveshaft of the tail rotor drive system. The main driveshaft assembly then transmits power to the mast and transmission assembly system, and the forward driveshaft of the tail rotor drive system transmits power to the tail rotor.

The input shaft receives power from the engine. When the input shaft turns, sprags in the clutch assembly engage the output shaft and allow power to be transmitted to the output shaft which then transmits power both aft and forward. On the forward side, the output shaft connects to the main driveshaft assembly of the main rotor drive system. On the aft side, the output shaft connects to the forward driveshaft assembly of the tail rotor drive system. The housing assembly serves as a casing and an oil sump for the lubrication of the freewheel assembly. The transmission oil system supplies pressurized oil for the lubrication of the freewheel assembly. The housing assembly also has mount points for the components of the freewheel indicating system.

The splines of the input shaft on the freewheel assembly engage the engine power drive gear shaft. Power is then transmitted to the output shaft through the sprags of the clutch assembly.

During autorotation, the output shaft disengages from the input shaft through the effect of the clutch assembly. Thus, the engine power source no longer drives the output shaft and the main rotor then takes over to drive the mast and transmission system, its accessories, and the forward driveshaft of the tail rotor drive system.

🚁
Main driveshaft
Freewheel assembly