Descriptive analysis and diagammatic view of pitch control gear for propeller of BMW 801 A airplane engine; mechanism comprises two separate devices, one for regular use, and other for emergency use and to stop engine that has become disabled in flight by feathering its propeller; mechanism includes speed governor, and electric hydraulic pitch changing control by which power from stationary pitch control mechanism is transmitted to pitch changing gear.
VDM propeller pitch changing mechanism
Automotive Aviation Industries
Automotive and Aviation Industries ; 8 , n 4
1943
2 pages
Article (Journal)
English
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ROTATING-BLADE PROPELLER AND MECHANISM FOR CHANGING THE PITCH OF BLADES OF A CYCLOID PROPELLER
European Patent Office | 2018
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