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 they have been superseded by the peizo electric principle.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

Interlaminar fracture tests on composite materials , Generally, there are t...

Generally, there are three modes to describe different crack surface displacement in a cracked body. Mode I is opening or tensile mode where the crack surfaces move directly ap

Linear programming, Gandhi Textile company produces shirts and pants.The sh...

Gandhi Textile company produces shirts and pants.The shirts demands for the following two months are 10 and 12 units,whereas the demand for pants are 14 and 15.The capacity for fab

Assignment #5, the date december 13, 2005. Air traffic controllers in a con...

the date december 13, 2005. Air traffic controllers in a control tower in

Quality assurance, Graduate project in the field of quality assurance

Graduate project in the field of quality assurance

Plastics, what are the key polymeric structural features to most elastomer...

what are the key polymeric structural features to most elastomeric material

AVIATION, CONSTRUCTION, OPERATION, AND MAINTENANCE OF AVIATION METAL PROPEL...

CONSTRUCTION, OPERATION, AND MAINTENANCE OF AVIATION METAL PROPELLER

Regarding my project, i want to do project in the area wing in aircraft...p...

i want to do project in the area wing in aircraft...please give some sugestions or ideas in that

Torque indication - aircraft engine, Torque indication: Turboprop and t...

Torque indication: Turboprop and turboshaft engines do not provide significant thrust through their jet pipes, so EPR would not be of any use in determining the thrust being pr

Fibre optics communications, explain the fibre optic communication system w...

explain the fibre optic communication system with block diagram

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