An aeronautical thruster having a longitudinal axis and having a hub and at least two annular rows of unducted blades including an upstream annular row and a downstream annular row which are spaced apart from one another along the longitudinal axis, the upstream annular row being rotatable around the longitudinal axis, and the downstream annular row comprising a series of blades including a first blade and a second blade each extending in a radial direction from the hub to define a radial dimension between the hub and a radially outer end of the corresponding blade, wherein the radial dimension of the first blade is greater than the radial dimension of the second blade.
AERONAUTICAL THRUSTER
2024-09-19
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Emerald Group Publishing | 1988
|Engineering Index Backfile | 1929