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

Finance, Let C(K) denote a European vanilla Call option with strike price K...

Let C(K) denote a European vanilla Call option with strike price K. Assume that all options are identical except for strike price, and strike prices satisfy (K1) What are the no-

Compressor characteristics, Compressor characteristics: When a compress...

Compressor characteristics: When a compressor is designed it is essential to establish the points at which it is likely to surge. Tests are carried out to determine the relati

Corporate Governance, What is the status of corporate governance in UAE?

What is the status of corporate governance in UAE?

Financial management, I have a homework assignment with 12 present value an...

I have a homework assignment with 12 present value and future value related investment problems. Can you guys help with me these types of problems please?

KK-3 system coding, how to write code for any particle shape using KK-3 sys...

how to write code for any particle shape using KK-3 system coding in grope technology

Human Motion Kinetics, Beginning from rest when theta=10 degrees, a 30-kg c...

Beginning from rest when theta=10 degrees, a 30-kg child slides without kinetic friction down the slide which is in the shape of a 2.5 meter circular arc. Determine the child''s sp

Maintenance of aircraft under “b” conditions, Maintenance of Aircraft under...

Maintenance of Aircraft under “B” conditions:   The maintenance of aircraft flying under "B" conditions must be adequate in relation to the number and duration of the flight

Financial econometric , need solution in Financial econometric, Do you have...

need solution in Financial econometric, Do you have an expert in Financial econometric

Pitot intakes - aircraft maintenance , Pitot intakes: This intake is su...

Pitot intakes: This intake is suitable for subsonic or low supersonic speeds. Examples, 707, 747, A300B, Tristar, etc. The intake is usually short and is very efficient becau

Int. finance management, Discuss the roles of international financial syste...

Discuss the roles of international financial system in international business

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