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Ratier Metal Propeller with Pitch Variable in FlightOne of the serious sources of difficulties in variable pitch propellers is the turning moment or torque due to the centrifugal force which tends to bring the mean plane of the blades into the plane of rotation. This moment, which is found elsewhere only in propellers with removable blades, is so great that the aerodynamic forces, as regards their effect on the torsion, become entirely negligible in comparison with it. This report presents the Ratier Company's solution to changing the pitch of airplane propellers.
Document ID
19930094855
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Leglise, Pierre
Date Acquired
September 6, 2013
Publication Date
April 1, 1930
Report/Patent Number
NACA-TM-559
Report Number: NACA-TM-559
Accession Number
93R23775
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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