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Maintaining
your Continental and Lycoming engine
Vibrations & Balance by John SchwanerTable of Contents
Warning and ApplicationWarning-- For educational purposes only. If your engine develops an unusual vibration have it checked by a properly rated professional. For example, a vibrating engine may be caused by main crankshaft bearing failure. Before you start "balancing" or analyzing vibration signatures, have a properly rated professional check the health and airworthiness of the engine.
Cracked cylinder barrel caught before the cylinder blew off of the crankcase. Another good reason to carefully inspect all oil leaks! An engine that exhibits unusual vibrations may be failing. If your engine has an unusual or out-of-character vibration, have a mechanic inspect the engine before flight. Only after the basic health of the engine has been established should you proceed to problems with balance. Something as simple as malfunctioning hydraulic lifters can cause engine vibration.
What causes vibrations?
During normal operation, the chief cause of vibrations is fluctuating engine torque -more so on four cylinder engines than six cylinder engines since the torque impulses are further apart on four cylinder engines. The turning force (torque) imposed on the crankshaft occurs on each power stroke and causes uneven torque loading because internal combustion engines are pulsating flow devices. Torque vibrations are transmitted to the engine frame primarily from the cylinder walls, and, to a lesser extent, from the crankshaft. Torque is made up of two forces: inertia and gas pressure. What is balancing?Vibration OrdersSingle blade aerodynamics 1/2 order major component Gas pressure (torque) 1/2 order ranked relative cylinder influence Continental 1,2,3,4,5,6 Lycoming 5,6,3,4,1,2 1/2 order notes Amplitude depends on mount stiffness, crankshaft torsional stiffness, cylinder position, and gas pressure
1st order minor component Slight amounts of inertia and dead weight. Torque increases with order. 1st order major component Rotating imbalance 1st order related orders 2,4,5,7,8 Higher orders are torque Higher orders are torque orders 1st order notes Amplitude increases with engine speed. Movement of propeller from rotating imbalance can cause 2nd order vibration on 2-blade propeller or 3rd order vibration on 3-blade propeller
1-1/2 order minor component none 1-1/2 order major component Gas pressure (torque) 1-1/2 order related orders at 40% power 1-1/2 and 1/2 order have approximately same amplitude. At higher power settings 1/2 order is increasingly stronger than 1-1/2 order. 1-1/2 order ranked relative cylinder influence Lycoming 5,6,3,4,1,2 Continental 1,2,3,4,5,6 1-1/2 order note All 1/2 orders are gas pressure. 1-1/2 orders may be more accurate assessment of gas pressure variation than 1/2 order. Amplitude also depends on mount stiffness, crankshaft torsional stiffness, cylinder position and gas pressure.
2nd order minor component Propeller dynamics on 2-blade propeller. Rotating balance. Connecting rod couple (slight - subtracts from inertia) and propeller phase angle. 2nd order major component Inertia 2nd order related orders 1,4,5,6 2nd order cylinder influence none 2nd order note two blade propeller phase angle in relationship to forward crank pin may have slight influence. Inertia forces increase with engine speed.
3rd order minor component Gas pressure (counteracts inertia). Phase angle of 3 blade propeller. Aerodynamic excitation of 3 blade propeller. 3rd order major component Inertia. Third order is a major order 3rd order related orders 6,9 3rd order cylinder influence none 3rd order note Amplitude increases with rpm. Amplitude decreases with gas pressure. Crankshaft resonant frequency just above red-line rpm. Propeller phase angle in relationship to phase angle of 3rd order harmonic may increase, decrease, or have a neutral affect on 3rd order amplitude. Inertia forces increase with engine speed.
4th order minor component inertia 1/3 of gas pressure and counteracts. Slight connecting rod couple adds to gas pressure. 4th order major component Gas pressure (torque) 4th order related orders 1,2,5,7,8 4th order cylinder influence Continental: 1,2,3,4,5,6 Lycoming: 5,6,3,4,1,2 4th order note Amplitude increases with manifold pressure on engines without 4th order counterweights (pendulum absorbers).
4-1/2 order minor component none 4-1/2 order major component Gas pressure (torque) 4-1/2 order related orders 1-1/2, 7-1/2 4-1/2 order cylinder influence May vary if engine has 4-1/2 order counterweight (pendulum absorber) Continental: 1,2,3,4,5,6 Lycoming: 5,6,3,4,1,2 4-1/2 order note Counterweights (pendulum absorbers) may be used to absorb 4-1/2 order torques. Amplitude increases with manifold pressure on engines without 4-1/2 order counterweights (pendulum absorbers). 4-1/2 order vibrations are especially hard on propellers.
5th order minor component 8% inertia 5th order major component Gas pressure (torque) 5th order related orders 1,2,4,6 5th order cylinder influence May vary if engine has 5th order counterweights (pendulum absorbers). Continental: 1,2,3,4,5,6 Lycoming: 5,6,3,4,1,2 5th order note 6th order minor component Less than 1% inertia. Less than 1/2 of 1% connecting rod couple. 6th order major component Gas pressure (torque) 6th order related orders 3,6,9,12 6th order cylinder influence none 6th order note Counterweights (pendulum absorbers) absorb 6th order torque. Vibration measurements may vary depending on manifold pressure and engine rpm. Especially with high manifold pressure at resonant rpm (approximately 2400).
Bifilar Pendulum Absorbers (common name Counterweights) in Lycoming engine
Order Defined
IPS definedVelocity is arrived at by simply integrating the signal that an accelerometer produces. If you integrate a second time, you get displacement. It has been found through experience that velocity is a better unit of measurement to use if you want the numbers to track with how severe a vibration is independent of RPM. In other words, a 1 IPS vibration is pretty severe no matter if the object is turning at 200 RPM or 200,000 RPM. This is not true for units of acceleration or displacement. Now, for harmonic oscillation, the acceleration is just omega times the velocity; for, say 2400 rpm (fundamental frequency of 40 Hz), your vibration of 1 IPS corresponds to an acceleration of 20.9 ft per sec^2 or about 0.7 Gs. That does seem a fairly healthy vibration for the front end of an engine with propeller. It takes on average 65 grams to correct for a 1 IPS vibration. But this value varies greatly from ship to ship. From a low of 20 to a high of 130.
Static and Dynamic Balance DefinedStatic balance is the balance of forces due to the action of gravity. Static balance involves weight matching and balance beam matching of components. If the center of gravity of a crankshaft does not lie on the mechanical axis, then the crankshaft will turn until the center of gravity is directly beneath the mechanical axis. The difference between static and dynamic balance is that dynamic balance not only balances inertia forces but also centrifugal couples. Both static and dynamic balance only affects first order vibrations. Degrees of FreedomCrankshaft balanceAdditional Vibration InformationConnecting rod balance Influence of Propeller on Engine Rocking What causes engine detuning Chart of Engine Vibrations
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