Mailing List lml@lancaironline.net Message #48781
From: Jeffrey Liegner, MD <liegner@embarqmail.com>
Sender: <marv@lancaironline.net>
Subject: McCauley Prop Governor Unfeathering Accumulator
Date: Sun, 07 Sep 2008 18:09:01 -0400
To: <lml@lancaironline.net>
McCauley Prop Governor Unfeathering Accumulator
                                     McCauley Contact Info
Product Support:
Hal Bohannon,  Manager
Gary Peak,  Service Engineer
Chris Bell,   Service Engineer
James Williams , Technical Training Administrator
Leah Hammar, Engineering Technical Aide

Mailing Address:
McCauley Propeller Systems
PO Box 7704
Wichita, KS 67277-7704
 
Phone: 316-831-4021
Toll Free: 800-621-PROP (7767)
Fax: 316-831-3858
Support: productsupport@mccauley.textron.com


Explanation:
http://www.mccauley.textron.com/prop/prop-tech/pg02var-ptch.html
A full-feathering propeller system is normally used only on twin-engine aircraft. If one of the engines fails in flight, the propeller on the idle engine can rotate or ?windmill,? causing increased drag. To prevent this, the propeller can be ?feathered? (turned to a very high pitch), with the blades almost parallel to the airstream. This eliminates asymmetric drag forces caused by windmilling when an engine is shut down. A propeller that can be pitched to this position is called a full-feathering propeller.


http://www.mccauley.textron.com/prop/prop-tech/pg04feather.html
The unfeathering accumulator option permits a feathered propeller to be unfeathered in flight for air-starting the engine. With this option, the governor is modified to provide an external high-pressure oil outlet through a check valve, as well as a device for unseating the check valve. The external outlet is connected to an accumulator. One side of the accumulator is filled with compressed nitrogen and the other side with oil. This allows the oil to be stored under high pressure, as it is during normal flight. (Fig. 13) When the propeller is feathered, the check valve maintains oil pressure in the accumulator. (Fig. 14) When the propeller control is moved from feather to low pitch, the check valve is unseated, permitting the high-pressure oil in the accumulator to flow to the governor pilot valve. With the governor control lever and shaft in low pitch, the speeder spring forces the pilot valve down so that the oil flows to the propeller and moves the blades to low pitch. (Fig. 15)


Feathering Governors
Feathering governors were developed to maintain a constant speed on the feathering propeller as the name implies. The basic feathering governor model is identified by the alphanumeric callout of DCF290D(X)/T(X). Twin engine aircraft benefit from the safety of the use of the feathering propeller control system. The feathering governor uses oil from the engine to hydraulically maintain a given speed setting and allows the pilot to feather the propeller in the event of a loss of power or other engine problem. Feathering the propeller eliminates that would be caused by a wind-milling, non-feathered propeller. This gives the pilot the ability to fly the aircraft with one engine to the nearest airport for repairs.
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http://www.mccauley.textron.com/prop/propframese.html
Feathering Governor Options: Unfeathering
Using the basic feathering governor (DCF) many options can be added to increase safety and comfort of the passengers. Some feathering governors have been designed to include the option of unfeathering. The basic unfeathering governor model is identified by the alphanumeric callout of DCFU290D(X)/T(X). The unfeathering option allows the pilot to unfeather the propeller if desired after it has already been feathered. The unfeathering systems includes a McCauley unfeathering accumulator which provides high pressure oil to the propeller to "push" the propellers blades out of the feathered position by using stored oil to move the propeller piston.

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