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Rotor Track and Balance
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Overview Rotor Balance Types of Balance Equipment Installation
Data Acquisition and Making Adjustments Troubleshooting
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Rotor Balance What is an imbalance? Advantages and disadvantages
Causes of imbalance Other sources of vibration
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Rotor Balance What is an imbalance?
A condition where there is more weight distributed on one side of a rotating component than on the other side
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Rotor Balance Advantages
Simple Cost efficient Cost effective
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Rotor Balance Disadvantages
Noise Vibration
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Rotor Balance Causes of Imbalance
Manufacturing tolerances Shimming and alignment Rotor track Static track Dynamic track
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Rotor Balance Rotor Track
Static track Perfect track if all blades produce the same lift Assumes that blade twist, profile, and stiffness are equal on all blades Assumed then to give equal lift on all surfaces of the blade
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Rotor Balance Rotor Track
Dynamic track How the rotors fly during operation More important to sacrifice a perfect tip path track for a rotor that is perfectly balanced
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Rotor Balance Other Sources of Vibration
Mechanical looseness Misalignment Track Worn bearings
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Types of Balance Dynamic track and balance Purpose of balancing
Types of imbalance
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Types of Balance Dynamic Track and Balance
First introduced in the late 1950’s Operators found that virtually all statically balanced rotors were out of balance dynamically when installed.
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Types of Balance Purpose of Balancing
Static Knife edge Suspended arbor Bubble balance
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Types of Balance Purpose of Balancing
Dynamic Performed during operation All of the rotating components are balanced as an assembly
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Types of Balance Types of Imbalance
Mass imbalance Distribution of the mass Spanwise or chordwise Aerodynamic imbalance Out-of-track condition exists
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Types of Balance Benefits to Dynamic Balance
Enhance comfort Reduce wear Increase safety by reducing component stress Lower operating costs
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Equipment Sensors Tach sources Vibration measurements
Amplitude and phase
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Equipment Sensors Accelerometers Displacement sensors Velocity sensors
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Equipment Accelerometers
Measure acceleration Typically reported in g’s More sensitive to higher frequencies Directly related to force caused by unbalance Used in balancing (after conversion to velocity or displacement)
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Equipment Displacement Sensors
Measure change in position Typically reported in mils (.001 of an inch) peak to peak More sensitive to Low frequencies Directly related to movements due to imbalance Seldom used in balance (however, displacement units are often used)
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Equipment Velocity Sensors
Measure velocity Typically reported in IPS peak More sensitive to medium frequencies Directly related to energy from imbalance Often used in balance
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Equipment Sensor Construction
PEDESTAL PIEZOELECTRIC ELEMENT IN COMPRESSION SEISMIC MASS OUTPUT CONNECTOR AND AMPLIFIER BASE PRELOAD SCREW
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Equipment Tach Sources
Magnetic pickup Phototach
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Equipment Magnetic Pickup
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Equipment Phototach
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Equipment Vibration Measurements
Amplitude and phase Correlation between the trigger of the tach source and the time until the sensor registers the maximum amplitude. The result will be a phase angle in degrees or time (clock angle)
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Installation Sensor Tach Source Tip Targets
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Installation Sensor
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Installation Tach Source
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Installation Tip Targets
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Installation Optical Tracker
Optical devices obsolete tip targets
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Data Acquisition and Making Adjustments
Polar plotting Automated solutions Rotor track and balance Rules
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Data Acquisition and Making Adjustments Polar Plotting
IPS and phase values are taken from the analyzer and manually plotted on charts to obtain a correction.
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Data Acquisition and Making Adjustments Automated Solutions
The analyzer is used to collect the phase and IPS readings then calculates a solution The calculated solution is then implemented by the user eliminating manual calculations
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Data Acquisition and Making Adjustments Rotor Track and Balance
Pitch links Tab Sweep Tip weight Hub weight Blade chordwise weight
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Data Acquisition and Making Adjustments Pitch Links
Changes the lift of the blade by adjusting the angle of attack at the rotor hub Characteristically changes the tip path plane throughout speed range Characteristically has large drag changes resulting in a strong effect on lateral balance
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Data Acquisition and Making Adjustments Tab
Changes the lift of the blade by adjusting the twist in the blade aerodynamically Characteristically changes the tip path plane at higher airspeeds Characteristically has small drag changes resulting in little affect on the lateral vibrations
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Data Acquisition and Making Adjustments Sweep
Changes the balance of the rotor head by adjusting the center of mass Characteristically changes the mass at all air speeds Characteristically it has little effect on the lift of the rotor and the vertical vibration
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Data Acquisition and Making Adjustments Tip Weight
Changes the mass of the rotor head by adjusting blade weight Characteristically no change to tip path plane Characteristically has a large effect on lateral vibration
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Data Acquisition and Making Adjustments Hub Weight
Changes the mass of the rotor by changing rotor head mass Characteristically has large effects on the lateral vibration Characteristically has no effect on tip path plane
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Data Acquisition and Making Adjustments Blade Chord Weight
Changes the center of gravity of the blade Characteristically changes tip path with changes in collective force Characteristically has large effects on verticals Characteristically has large effects on laterals at ground/hover and in letdowns
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Troubleshooting Polar Plotting - Human error Worn components
Structural resonance
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Troubleshooting Polar Plotting
Human Error The result of an adjustment increases the IPS or the moveline 180 degrees out
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Troubleshooting Worn Components
A specific vibration level is achieved and continued adjustments result in IPS levels that do not change and phase angle walks around the chart. A large amount of weight added to a location results in no change in IPS or phase
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Troubleshooting Structural Resonance
Unrepeatable reading Adjustments result in varying results Phase angles and IPS levels are very erratic and unpredictable when known good solutions are implemented.
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