Abradable linings-aircraft engine, Other Engineering

Assignment Help:

Abradable Linings:

Abradable Linings are usually made of a composite material which will be abraded away should the tip of a rotating blade touch the material. In flight the casings of an engine are subject to large changes in ambient temperature, so they will expand or contract. As we know the air temperature at 30,000ft is close to -50°C this would cause the casings to contract onto the rotor and the blades will then rub. To overcome this problem abrasive materials where used on early engines to wear down the tip of the blades, but this may cause balance problems. So most engines now use abradable linings that maintain minimum tip clearance but do not affect balance. They are usually found on the fan as this is the cold area of the rotating assemblies.

1842_Abradable Linings.png


Related Discussions:- Abradable linings-aircraft engine

Zener diode, easy defination of zener diode nd its application and characte...

easy defination of zener diode nd its application and characteristics ?

Electronics, explain compensated semiconductors

explain compensated semiconductors

Navigation systems , Navigation Systems  • Traditional guidance systems...

Navigation Systems  • Traditional guidance systems used mechanical gyroscopes (rate gyros) to measure the angular velocities of the vehicle or of the gimbals on which the seeke

Material science, Ask question #Minimum lkjhbi mbj jhb uy 100 words accept...

Ask question #Minimum lkjhbi mbj jhb uy 100 words accepted#

Fire safety management on railway stations, Fire safety management on railw...

Fire safety management on railway stations: Storage  tanks  are  not  allowed  above  underground  structures  or  within  a  certain distance of them. Some staff exits are

Exhaust jet mixing - aircraft design, Exhaust Jet Mixing: Figure shows ...

Exhaust Jet Mixing: Figure shows that the noise from the exhaust jet is the main contributor to the total noise generated by a low by-pass ratio turbo-fan. For a turbo-jet the

Flight control - linear system, Representations of a linear system The ...

Representations of a linear system The linear system of Section is shown in block diagram To determine the responseof the output of the system y(t) to an input u(t) the initial

Petroleum Engineering project, I need help About the project I sent and it ...

I need help About the project I sent and it is the third time I am sending so please I really want help

Thermodynamics.., Steam enters in the turbine at 6 MPa and 450 deg C and ex...

Steam enters in the turbine at 6 MPa and 450 deg C and expands at some intermediate pressure 60 % of steam is extracted and remainder expands to 10 kPa at this Investigate the effe

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