Mechanical gearbox for aircraft turbine
A technology for mechanical gearboxes and turbines, applied in mechanical equipment, machines/engines, transmission boxes, etc., can solve problems such as large axial overload size requirements, and achieve the effect of optimizing oil film thickness and optimizing lubricating oil consumption
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[0066] figure 1 A turbomachine 1 is described which generally comprises an axis of rotation X, a fan S, a low pressure compressor 1a, a high pressure compressor 1b, an annular combustor 1c, a high pressure turbine 1d, a low pressure turbine 1e and an exhaust nozzle 1h. The high-pressure compressor 1b and the high-pressure turbine 1d are connected by a high-pressure shaft 2 and together form a high-pressure (HP) body. The low-pressure compressor 1a and the low-pressure turbine 1e are connected by a low-pressure shaft 3 and together with this form a low-pressure (LP) body.
[0067] The fan S is driven by a fan shaft 4 which is driven by the LP shaft 3 by means of a gearbox 6 . The gearbox 6 is generally of the planetary or epicyclic type.
[0068] The following description refers to gearboxes of the planetary type, in which the ring gear is movable in rotation.
[0069] The gearbox 6 is positioned in the upstream part of the turbine. A fixed structure is arranged to form an ...
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