AERONAUTICAL THRUSTER

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 th...

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Bibliographic Details
Main Authors JODET, Norman Bruno André, LEBEAULT, Eva Julie, GRUBER, Mathieu Simon Paul, DUBOIS, Adrien Clément Marcel, REGNARD, Josselin David Florian, GEA AGUILERA, Fernando, BINDER, Anthony
Format Patent
LanguageEnglish
Published 19.09.2024
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary: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.
Bibliography:Application Number: US202218577064