Causes of unbalance - aircraft design, Other Engineering

Assignment Help:

Causes of unbalance

Unbalance may be caused by a variety of factors occurring singly or in combination with others. These factors include:-

a) Eccentricity

Eccentricity exists when the geometric centreline of a part or assembly does not coincide with its axis of rotation. This may be as a result of locating features (eg. spigot location, bolt holes, splines, serration's, couplings), being eccentric to the bearing location.

1544_cause of unblance.png

b) Variation in Wall Thickness

1705_cause of unblance1.png

Variation in wall thickness may be as a result of eccentricity between an inner and outer diameter of a cylindrical type feature, or it may be as a result of a difference in thickness between a radial section of a disk type feature and the section diametrically opposite.

c) Blade Distribution

Unbalance can be caused by an unequal or unsymmetrical arrangement of a set of blades, either by reference to their mass moments or their dead weights depending on the size of the blades. This can be as a result of faulty weighting, inaccurate or illegible recording or assembly errors.

d) Unsymmetrical Features

1508_cause of unblance2.png

These may be due to manufacturing processes, such as blow holes in castings or design features such as offset holes, locating dogs, slots, keyways, etc.

e) Distortion

This can be caused by stress relieving, eg. after welding, or by unequal thermal growth during running.

f) Fits and Clearances

Clearance between mating parts allows relative movement of the parts and a consequent shift of the axis of rotation during running (or even during balancing). Joints incompletely assembled, eg. chamfers fouling radii, abutment faces not pulled together, may cause a ‘bent' rotor or an unsuitable joint, which may cause a shift during running. It is important to prevent separate locating, or fixing, features from influencing each other eg. bolt holes, spigot locations, serration's, etc. must be geometrically controlled to prevent ‘fighting' between more than one feature. See also the section on tooling, adapters, drives, dummy rotors, etc.

g) Swash

362_cause of unblance3.png

Swash is caused by out of squareness of abutment faces relative to the bearing diameter, abutment faces not being parallel across the component, eg. spacers, adjusting washers, disks, etc. It is important that the bolted joints are tightened in sequence and in increments according to the torquing instructions.

h) Miscellaneous

Foreign bodies inside assemblies, oil accumulation, carbon deposits, usually found when check balancing after running.

 


Related Discussions:- Causes of unbalance - aircraft design

Oscilloscope probes, Direct probe,isolation probe,high impedence probe,acti...

Direct probe,isolation probe,high impedence probe,active probe,current probe

Bragg''s spectrometer , It consists o a source of x ray, with a number of c...

It consists o a source of x ray, with a number of collimated slits. Crystal under investigation is mounted on a table, and the position of this table can be recorded on vernier sca

FISICA, EL DESPLAZAMEINTO DE UNA PARTICULA ESTA DADO POR S=(-2+3T)e¨-0.5t

EL DESPLAZAMEINTO DE UNA PARTICULA ESTA DADO POR S=(-2+3T)e¨-0.5t

Internal rate of return: multiple alternatives, Internal Rate of Return: Mu...

Internal Rate of Return: Multiple Alternatives To compare multiple alternatives using the IRR as measure of economic worth we must use the incremental approach. It is erroneou

.quantifying financial risk, What is the standard deviation of return if we...

What is the standard deviation of return if we have the following two possible outcomes: a rise of 8.00 per cent with 0.58 probability or a fall of -6.00 per cent?

How will you make finance forecasting ?, how will you make finance forecast...

how will you make finance forecasting ? First I will evaluation the past seasons fiscal reports to get an Idea about the economical functions. Then will talk about with the cont

Aeronautical, apply equations to solve problems for specified aerodynamic a...

apply equations to solve problems for specified aerodynamic applications. Need some inputs regarding this.

Engine speed indicators, Engine speed indicators: All engines have thei...

Engine speed indicators: All engines have their rotational speed (R.P.M.) indicated. On a twin or triple-spool engine, the high pressure assembly speed is always indicated; in

Aeroengines - cfd, Essentially, the strategy of CFD is to replace the conti...

Essentially, the strategy of CFD is to replace the continuous problem domain with a discrete domain using a grid domain with a discrete domain using a grid. In a continuous doma

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