POWER TRANSMISSION MODULE FOR AN AIRCRAFT TURBOMACHINE

A power transmission module for an aircraft, the module including a torque input connected to a turbine shaft, a first torque output and a second torque output, the power transmission module including a mechanical reducer including a sun gear forming the torque input, and planet gears carried by a p...

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Bibliographische Detailangaben
Hauptverfasser: LEFEBVRE, Simon Loic Clement, MOULY, Guillaume Pierre, SIMON, Adrien Louis, BECK, Guillaume Julien
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:A power transmission module for an aircraft, the module including a torque input connected to a turbine shaft, a first torque output and a second torque output, the power transmission module including a mechanical reducer including a sun gear forming the torque input, and planet gears carried by a planet carrier, wherein each of the planet gears includes at least three independent toothings and further includes a first toothing meshed with the sun gear, a second toothing meshed with an element forming one of the torque outputs, and a third toothing meshed with another element