Power transmission gearbox presenting a modifiable speed of rotation at its outlet, and a corresponding method of operation
AssigneeEurocopter
InventorMichel Vialle
Life of this patent
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AssigneeEurocopter
InventorMichel Vialle
Estimating the term…
A power transmission gearbox for rotorcraft for transmitting rotary movement from at least two engine members to a main shaft, wherein the gearbox presents at least two transmission systems for imparting rotary movement to the main shaft, each of the transmission systems including: an inlet shaft designed to be driven in rotation by an engine member; at least two reduction stages presenting different reduction ratios; a first gearwheel connected to the inlet shaft via a declutchable freewheel, the gearwheel meshing with a first toothed wheel secured to an intermediate shaft defining at least a first reduction stage; a second gearwheel connected to the inlet shaft via a simple freewheel, the second gearwheel meshing with a second toothed wheel secured to the intermediate shaft defining the second reduction stage; a main freewheel mounted on the intermediate shaft to rotate a complementary toothed wheel secured to the main shaft; and a clutch mechanism for the declutchable freewheel.
A power transmission gearbox for rotorcraft for transmitting rotary movement from at least two engine members (MG, MD) to a main shaft (1) with determined reduction ratios, wherein the gearbox presents at least two transmission systems (G, D) for imparting rotary movement to the main shaft (1), each of the transmission systems comprising:
Dependencies are inferred from the claim text.