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AIRCRAFT ENGINE SPEED REGULATOR MECHANISM
Upon an increase in engine speed, weights 1 of the centrifugal governor move outward and, turning about axes O, compress conical spring 2. This raises valve spool 3 and hydraulic fluid from sleeve 4 is discharged through channel 5 to the engine crankcase. As a result, the propeller pitch increases, increasing the power required to drive the propeller and, consequently, reducing the engine speed. A…
Creator
- Europeana
Type of item
- image
Creator
- Europeana
Type of item
- image
Providing institution
Aggregator
Rights statement for the media in this item (unless otherwise specified)
- http://creativecommons.org/licenses/by-nc-nd/3.0/
- http://creativecommons.org/licenses/by-nc-nd/3.0/
Rights
- http://www.dmg-lib.org/dmglib/main/portal.jsp?mainNaviState=site.oairights
Identifier
- dmg:26958023
- http://www.dmg-lib.org/dmglib/handler?image=26958023
Relations
- Ilmenau University of Technology, Germany
Providing country
- Europe
Collection name
First time published on Europeana
- 2013-11-25T17:57:15.665Z
Last time updated from providing institution
- 2013-11-25T17:57:15.665Z