Static unbalance-aircraft maintenance , Other Engineering

Assignment Help:

Static Unbalance:

This arises when two EQUAL unbalance masses are positioned at opposite ends of a rotor and spaced at 180 from each other. If placed on knife-edges, the rotor would be statically balanced. However, when the rotor is rotated, the out of balance masses will cause a centrifugal force to act at each end and hence each end will vibrate independently as shown in figure.

235_syatic unblance.png

Dynamic Unbalance

This occurs when the unbalanced masses may be either unequal in size or positioned at some angle other than 180 to each other, or even both of these conditions. These unbalanced forces now cause the rotor to vibrate.

FAN BALANCING

Before we look at fan balancing we must first look at vibration analysis techniques adopted on modern gas turbines and the reason for doing it. One of the requirements of an on-condition maintenance policy is that defects can be detected sufficiently early to permit rectification before secondary damage occurs. The analysis of engine vibration signatures is becoming an increasingly important tool for detecting early failure in mechanical components.

A vibration monitoring system begins with a sensor, which may be a velocity transducer or a peizo electric accelerometer. They both convert the mechanical vibration of the machine into an electrical signal proportional to the vibrations produced and together with the associated electrical circuitry feed signals to either cockpit mounted gauges warning systems or a separate vibration analyser.

827_syatic unblance1.png

Velocity Transducer

This device operates on the principle of a permanent magnet to move within a coil, inducing voltage. Because of the moving parts with all the inherent disadvantages of wear, friction, etc. they have been superseded by the peizo electric principle.
Peizo Electric Accelerometer

In this device, vibrating forces are transmitted to a peizo electric disc the resultant deformation of the disc produces an electrical charge. Accelerometers have a greater frequency range than velocity transducers and their lack of moving parts makes them a much more stable and reliable means of collecting the basic vibration signal.
Many different specifications for accelerometers and transducers are available and some of the considerations which govern their choice are:-

(1) DYNAMIC RANGE. The amplitude range over which the device is required to perform.
(2) SENSITIVITY. The severity of the vibration liable to be encountered.
(3) FREQUENCY RESPONSE. The full operating frequency range required.
(4) TEMPERATURE RANGE. The upper and lower temperature extremities to which the device will be subjected and also any heat soak conditions.

 

 

 


Related Discussions:- Static unbalance-aircraft maintenance

Architectural graphics, How to draw schiography in a perspective view of an...

How to draw schiography in a perspective view of an object

Refractory and their classification, Q. What are refractory's? How are they...

Q. What are refractory's? How are they classified? Give the essential requirements of good refractories.                                                    OR Discuss cla

Solidification of casting, Q. Describe the terms "Solids zone", "Mushy Zone...

Q. Describe the terms "Solids zone", "Mushy Zone" and "Liquid Zone" used in solidification of casting and explain directional solidification in casting. Ans. Solidificati

Budget and determining, In Corporate finance, Experts engaged in this occup...

In Corporate finance, Experts engaged in this occupation have the liability to increase the organization's revenue, shareholder's money, investment spending budget and determining

Power factor., how can decrease the power factor of any electric circuit

how can decrease the power factor of any electric circuit

sweep effects, In the previous discussion, we investigated the static aero...

In the previous discussion, we investigated the static aeroelastic behaviour of straight (unswept) wings. These wings are characterised by an effective decoupling of wing bending a

Evaporation, 2-17 Given a wind speed of 5.0 m/s at 2 m above the ground and...

2-17 Given a wind speed of 5.0 m/s at 2 m above the ground and a roughness length of 0.8 cm, compute (a) the friction velocity, in centimeters per second, and (b) the wind speed, i

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd