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

Adder /subtractor, operation of adder/subtraction by using truthtable

operation of adder/subtraction by using truthtable

Linear integrated circuit, ac analysis for dual input unbalanced output dif...

ac analysis for dual input unbalanced output differntial amplifier

Maintenance Requirement Analysis, Ask questioA wire rope used as a crane ho...

Ask questioA wire rope used as a crane hoist rope has a mean life of 530 days. The wire rope predominantly fails in a wear-out mode caused by either corrosion, abrasive wear or fat

Seekers , Seekers   There are two main types of sensor used in autono...

Seekers   There are two main types of sensor used in autonomous vehicles (seekers and position/attitude sensors) - although not all systems have both.            - Airc

Agricultural engineering , Agricultural engineering does not easily mean on...

Agricultural engineering does not easily mean only fruits and vegetables formed from the fields. Agriculture has come up with a dissimilar  look now. When you open a paouch of chip

Fuel control in aircraft engine, Fuel control in Aircraft Engine: ...

Fuel control in Aircraft Engine: The basic fuel system is comprised of a fuel pump that receives low-pressure fuel from the aircraft fuel tank via a low pressure fuel valv

Caselet- 2, suggestion regarding credit limit. should it be approved or not...

suggestion regarding credit limit. should it be approved or not what should be the amount of

Doble titration, object:THE NORMALITY OF STANDARD FAS SOLUTION(A)N/50.find ...

object:THE NORMALITY OF STANDARD FAS SOLUTION(A)N/50.find out the strenghth and normality of fas(b) using potasium permagnettetraoxide as intermidiate compound & self indicator

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