摘要 |
The invention relates to a non-streamlined propeller having blades with a variable setting for a turbine engine, the blades of the propeller being rotatably mounted about the axes thereof in radial recesses (136) of a rotor element (124), and each blade being supported by a plate (144) held in a recess by a sectored ring (150), and including an inner portion (160) mounted, by interlocking, in a groove (162) of the plate, the ring sectors being inserted into the recess from the inside and locked by a nut (170) screwed onto the plate. |
申请人 |
SNECMA;BOURU, MICHEL, ANDRE;JABLONSKI, LAURENT;JOLY, PHILIPPE;BOSTON, ERIC, JACQUES |
发明人 |
BOURU, MICHEL, ANDRE;JABLONSKI, LAURENT;JOLY, PHILIPPE;BOSTON, ERIC, JACQUES |