Engine indication systems in aircraft, Other Engineering

Assignment Help:

Engine indication systems in Aircraft:

Engine indications are very important to the crew of a powered aircraft, as they indicate one of the primary parameters needed for flight.

There are three types of indications:
1. Performance indications such as thrust (Engine Pressure Ratio EPR) and Revolutions Per Minute (RPM).
2. Operation indications such as Turbine Temperature indications, fuel flow, oil pressure and temperature.
3. Discrete indications which put ‘ON' a warning annunciator such as low oil pressure, fuel low pressure engine overspeed etc.

The engine instruments on most modern commercial aircraft will invariably be located on the main instrument panel in the centre, so that they are visible to both pilots. The instruments are laid out in a logical pattern so that the main thrust indicator is at or near the top of the indications. The indicators will be in vertical columns for each engine and like indicators in rows.

When a flight engineer is carried he will have a panel with some of the primary indications and all of the secondary and discrete indicators. He may also have a duplicate set of thrust levers so that he can trim engines when required.

Until fairly recently the majority of aircraft used analogue gauges (sometimes referred to as clockwork gauges) These had moving pointers or strips which indicated the parameter being monitored.

The modern trend is to replace the analogue instruments with electronic instruments that use LED, liquid crystal or cathode ray screens to display the engine parameters, often not displaying continuously all the information, but to highlight when a fault has occurred or when asked for by the crew. These types of instrument do not usually retain the last indication after an accident, however the electronic box powering them will inform the flight data recorder and/or retain the information in its own memory.

238_Engine indication systems in Aircraft.png


Related Discussions:- Engine indication systems in aircraft

Fire risk assessment process, Fire risk assessment process: This is th...

Fire risk assessment process: This is the main part of the FRA process.    Here we consider the risk, measure it against what we consider acceptable and, if we consider that t

Corporate Strategy, Corporate Strategy Strategy In our earlier discussion...

Corporate Strategy Strategy In our earlier discussion, we made distinctions between merger and acquisition or takeover. However, they generally involve similar analyses and evalu

Torsional divergence, Torsional Divergence Lets first try to explain a...

Torsional Divergence Lets first try to explain and interpret torsional divergence for the aerofoil structural model physically. An additional figure describing the mechanical s

Wet process of manufacturing of portland cement, What are Portland cement a...

What are Portland cement and its composition? Describe the manufacturing process of cement with diagram.  Manufacturing of Portland cement: Dry and Wet Process,  Describe the

Land serveying, list out the errors in lenier measurment

list out the errors in lenier measurment

Nash equilibrium, how to get ns2 coding for nash equilibrium

how to get ns2 coding for nash equilibrium

Actuators , Actuators  The actuator consists of the control surfaces...

Actuators  The actuator consists of the control surfaces and associated servomechanisms, and is used to change the missile attitude and trajectory or flight path.

Trusses, Analysis of truste,2D truss analysis using method of joint(cantile...

Analysis of truste,2D truss analysis using method of joint(cantilever & simply support)?

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