Engine speed indicators, Other Engineering

Assignment Help:

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 most instances, additional indicators show the speed of the low pressure and intermediate pressure assemblies. Where Engine Pressure Ratio (EPR) is not indicated then Low Pressure RPM is indicated as this can be corrected to give Thrust.

58_enigne indicator.png

Engine speed indication can be electrically transmitted from a small tacho-generator, driven by the engine, to an indicator that shows the actual revolutions per minute (r.p.m.), or a percentage of the maximum engine speed. The engine speed is often used to assess engine thrust, but it does not give an absolute indication of the thrust being produced because inlet temperature and pressure conditions affect the thrust at a given engine speed.

822_Engine speed indicators.png

The tacho-generator supplies a three phase alternating current, the frequency of which is dependent upon engine speed. The generator output frequency controls the speed of a synchronous motor in the indicator, and rotation of a magnet assembly housed in a drum or drag cup induces movement of the drum and consequent movement of the indicator pointer.Tachometer generator systems have largely been replace by speed probes. A variable-reluctance speed probe, in conjunction with a phonic wheel, is used to induce an electric current that is amplified and then transmitted to an indicator (fig. 14.5.). This method can be used to provide an indication of r.p.m. without the need for a separately driven generator, with its associated drives, thus reducing the number of components and moving parts in the engine.

2315_Engine speed indicators1.png

The speed probe can be positioned on the compressor casing in line with the phonic wheel, which can be a machined part of the compressor shaft. A gear wheel in an external gearbox can also be used. The teeth on the periphery of the wheel pass the probe once each revolution and induce an electric current by varying the magnetic flux across a coil in the probe. The magnitude of the current is governed by the rate of change of the magnetic flux and is thus directly related to engine speed.

On some engines one of the teeth is bigger than the others, and will give a bigger response. This can be used for Fan blade balancing or synchronising and/or synchrophasing.

In addition to providing an indication of rotor speed, the current induced at the speed probe can be used to illuminate a warning lamp on the instrument panel to indicate to the pilot that a rotor assembly is turning. This is particularly important at engine start, because it informs the pilot when to open the fuel cock to allow fuel to the engine. The lamp is connected into the starting circuit and is only illuminated during the starting cycle.

2361_Engine speed indicators2.png

A variation of this system uses an eddy current sensor on the fan casing that senses the fan blades rotating. Sensors similar to these can be used for active tip clearance control, where it senses the gap between the casing and the blade.

Modern speed gauges usually have an analogue type display, i.e. a pointer, and also a digital readout below the pointer axis. A target speed indicator is usually fitted which on a clockwork gauge is a pointer outside the numbers, and on an electronic gauge as a coloured marker, this usually has a digital readout of its set position within the gauge normally above the pointer axis.


Related Discussions:- Engine speed indicators

Aerodynamics-source of drage, Source of drage Total Drag on an aerofoil...

Source of drage Total Drag on an aerofoil is called profile drag - Skin friction • due to tangential force arising from friction - Pressure • Form - due to the inte

Aircraft controls, The aerodynamic flight controls of a typical aeroplane ...

The aerodynamic flight controls of a typical aeroplane include ailerons (British: ξ ("Xi"); US: da or δa), elevator (British: η ("eta"); US de or δe), and rudder (British: ζ ("zeta

Themodynamic, 1 kg of air is allowed to expand reversibly in a cylinder beh...

1 kg of air is allowed to expand reversibly in a cylinder behind a piston in such a way that the temperature remains constant at 260 degree while the volume is doubled.The piston i

Open innovation, is there any open innovation engineering web portal in ind...

is there any open innovation engineering web portal in india

Aircraft internal and external markings, AIRCRAFT INTERNAL AND EXTERNAL MAR...

AIRCRAFT INTERNAL AND EXTERNAL MARKINGS SMOKING IN AIRCRAFT - Reference: ANO Article 66 and JAR-25.791 Every aircraft registered in the U.K. must have a notice indicati

Automated Part Processing, merits of laser light curtains in terms of cost,...

merits of laser light curtains in terms of cost,ease-of-use,flexibility.

TANGENT GALVANOMETER, WHY THE NEEDLE OF TANGENT GALVANOMETER DEFLECT WITH I...

WHY THE NEEDLE OF TANGENT GALVANOMETER DEFLECT WITH INCREASING OR DECREASING CURRENT?

Various stages of creep, Q. Explain various stages of creep? Ans. CREE...

Q. Explain various stages of creep? Ans. CREEP: Creep can be defined as the process by which plastic flow occurs when a constant stress or load is applied to a material for a

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