Propeller pitch control, Other Engineering

Assignment Help:

Propeller pitch control:

Before looking at propeller pitch control an understanding of the relationship between the 'Power Lever' and the 'RPM (condition / speed) Lever' with regard to power management control, the following text is related to a 'fixed shaft', coupled turbo, propeller. 

The function of the power management system is to provide a means for controlling load and power. To do this a basic system utilising a lever to control power, and separate lever to control propeller load might be used. Moving the fuel lever alone would cause RPM to increase or decrease, but until the pitch lever is moved no real thrust would be produced. The same could be said about using the pitch lever alone. RPM fluctuations can be caused by varying propeller load, but no real operator of such a system was extremely good, both levers could be worked simultaneously. This would keep RPM constant and give useful thrust with power.

398_Propeller pitch control.png

Rather than depend on the skillful movement of two separate levers the two functions are incorporated into one lever, the Power Lever. Through a system of cams and linkages it will be rigged to give two modes of operation, 'BETA' mode and 'Prop Governing' mode.

When the power lever is moved between Flight Idle (FI) and Reverse (Rev) it will be operating in the BETA mode with the Propeller Pitch Control (PPC) directly controlling blade angle. From FI to Max. the propeller governor will adjust blade angle in response to the fuel flows demanded by the Manual Fuel Valve (MFV) situated with the Fuel Control Unit.

1307_Propeller pitch control1.png


When the power lever is advanced forward from the flight idle detent, the propeller pitch control cam will normally hold the propeller at a fixed pitch. The manual fuel valve cam will then cause fuel to increase and RPM to increase eventually giving authority to the propeller governor, see following diagram.

755_Propeller pitch control2.png

Earlier with the constant speed theory it was pointed out that the engine, with load and power equal, would operate at basically one RPM. Because of different operating conditions, such as taxiing or cruise, it becomes necessary to operate at some other RPM besides 100 percent. This is due to the need for noise reduction, fuel economy or operation at minimum load. The only function of the speed lever is to set engine operating RPM. To aid the speed lever, it is linked to the underspeed fuel governor and the propeller governor. The speed lever is used to 'calibrate' or set each governor RPM limit. With the speed lever in the low or taxi position, the underspeed governor is set to 96 percent RPM. When the speed lever is advanced to the high or takeoff position the underspeed governor is set to 97 percent RPM, the propeller governor is set to 100 percent RPM and will not be effective till this RPM is attained by forward movement of the power lever.


Related Discussions:- Propeller pitch control

Gated pattern, Gated pattern is used to produce good casting. It is esse...

Gated pattern is used to produce good casting. It is essential to make sure that full supply of molten metal flow into every part of the mould. Provision for easy passage of the

Aerofoil theory and the axial flow compressor, Aerofoil theory and the axia...

Aerofoil theory and the axial flow compressor  The blades of the axial flow compressor are aerofoils and as such behave in a similar way to aircraft mainplanes and propeller bl

Iron crabon, iron crabon diagram with reactions

iron crabon diagram with reactions

Programming, A charitable organization wants to design a special ATM machin...

A charitable organization wants to design a special ATM machine to be used by needy people. The association supplies the needy person with a pin number to be able to use the ATM

DSP HW1, With x[n] denoting the input signal and y[n] denoting the output s...

With x[n] denoting the input signal and y[n] denoting the output signal, give the difference equation relating the input signal to the output signal in the discrete-time domain, gi

Air-system in aircraft engine, Air-System in Aircraft Engine: In the wo...

Air-System in Aircraft Engine: In the working cycle and airflow section we discussed the main airflow and working cycle of a gas turbine engine and found that a major function

Variable interest rate, What is Variable Interest Rate? Interest rates whic...

What is Variable Interest Rate? Interest rates which is offered by banks or financial institutions on loans or deposits which are liable to change according to circumstances. For e

Local attraction, how can we find local attraction correction?

how can we find local attraction correction?

Engine torque, ENGINE TORQUE It is the force of rotating action about t...

ENGINE TORQUE It is the force of rotating action about the crankshaft axis at any given instant of time. It is given by,

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