Compressor damage, Other Engineering

Assignment Help:

Compressor Damage

Foreign objects often enter engine air intakes either accidentally or through carelessness. Items such as pens, pencils cigarette lighters etc. can be drawn out of pockets and ingested by the engine. The compressor could be damaged beyond repair. Likewise, tools left in engine intakes could be drawn in causing damage. Prior to starting an engine therefore, the AME should ensure that all tools used in the vicinity of the intakes are free of any foreign objects and the area in front of intakes should be cleared of any loose stones or rubbish . Examples of the typical types of damage to be found on compressor blades is shown in Figure and possible causes of damage and the terminology used in Figure.

1613_Compressor Damage.png


Related Discussions:- Compressor damage

Airflow control system principles-aircraft engine, Airflow control system p...

Airflow control system principles: For any given engine there is only one set of conditions, mass flow, pressure ratio and rpm, at which all the compressor components are opera

Steamtables, How to draw diagrams for Rankine cycle

How to draw diagrams for Rankine cycle

Parasitic resistances, Parasitic resistances This is particularly notic...

Parasitic resistances This is particularly noticeable if the transducer is a long way from where the power supply is located and if the transducer resistance is small.

Levelling Theory and Computation, Two readings i.e., 1.64m, and 0.73m, were...

Two readings i.e., 1.64m, and 0.73m, were taken during leveling procedure to define the slope of centerline of a bridge at points A, and B. If distance AB = 50m, find the slope of

Capital budgeting process, Capital budgeting process: When investing in a l...

Capital budgeting process: When investing in a long term assets, the project has been evaluated in term of its profitability and expected cash flow in the future. The capital budge

Electro-mechanical fuel control, Electro-mechanical fuel control: The s...

Electro-mechanical fuel control: The start fuel valve and ignition are energised as soon as rotation (3%) is sensed by an Electronic Sequence Unit (ESU). At 14% and with risin

Turbine blade clearance of aircraft, Turbine Blade Clearance. Creep is ...

Turbine Blade Clearance. Creep is term used to describe the continuous and permanent stretching of turbine blades due to high temperatures and centrifugal forces acting on the

Control surfaces , Control Surfaces  As with a flight control system...

Control Surfaces  As with a flight control system, a guidance algorithm uses control surfaces to control the behaviour of an airframe.         - Rudder, ailerons, elev

#title.electronic devices., Advantages and dis advantages of a diode in ser...

Advantages and dis advantages of a diode in series /shunt

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