Assembly including an AGB and an oil tank
A technology for accessory devices and gearboxes, which is applied in the direction of gas turbine devices, jet propulsion devices, engine components, etc., and can solve the problems of difficult design and manufacture, difficulty in mastering, and high cost
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[0026] The invention is described in relation to a turbojet engine. The turbojet generally includes a high-pressure shaft and a low-pressure shaft, each shaft including a compressor and a turbine. An energy distribution mechanism is mounted on said high pressure shaft and drives an energy distribution shaft which is mechanically connected to an auxiliary gearbox 1 , hereinafter denoted by the English abbreviation AGB 1 . More specifically, the energy distribution shaft transmits movement from the rotational axis of the high pressure shaft to the input (or drive) shaft of the AGB 1 . The input shaft of the AGB 1 is fixed to the wall of the AGB by a connection (in this case to the figure 1 The piece 11 of the upper wall) is connected to the AGB 1. The input shaft, supported by the connection 11 , passes through the upper wall of the AGB 1 in a conventional manner.
[0027] The turbojet engine also includes a lubricating circuit comprising an oil reservoir 2, a lubricating uni...
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