A propeller blade spanning radially from a root to a tip and spanning axially from a leading edge to a trailing edge spaced from the leading edge forming an airfoil therebetween where a sweep line can be defined as a spline fitted through points which are positioned along the chord line. The propeller blade having at least one spline defining the leading edge or trailing edge.
PROPELLER ASSEMBLY
15.08.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
PROPELLER ASSEMBLY AND PROPELLER BLADE RETENTION ASSEMBLY
Europäisches Patentamt | 2018
|Propeller assembly and propeller blade retention assembly
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