Abstract: An oil tank for a turbine engine comprising a closed enclosure having the shape of an arc of circle adapted to receive oil, with the enclosure having a lower portion and an upper portion at a distance from each other, and an oil level control device in the enclosure, wherein the oil level control device comprises a first sensor positioned in the lower portion of the enclosure so as to control the oil level, and a second sensor separate from the first sensor and positioned in the upper portion of the enclosure so as to control the oil level.

Abstract: An oil tank for a turbine engine comprising a closed enclosure having the shape of an arc of circle adapted to receive oil, with the enclosure having a lower portion and an upper portion at a distance from each other, and an oil level control device in the enclosure, wherein the oil level control device comprises a first sensor positioned in the lower portion of the enclosure so as to control the oil level, and a second sensor separate from the first sensor and positioned in the upper portion of the enclosure so as to control the oil level.

Abstract: The invention provides a method of ventilating equipment of a turbojet, the turbojet (10) having a cold zone (ZF) including a fan (14) upstream from a hot zone (ZC), the turbojet equipment (32) for ventilating being arranged in a ventilation space (30) available around the hot zone between a primary air stream passage (26) and a secondary air stream passage (28) of the turbojet, the method comprising taking ventilation air from one of the air stream passages in order to convey it to the ventilation space, and providing forced flow of the ventilation air by means of at least one electric fan (36) positioned inside the ventilation space and powered electrically by at least one thermoelectric generator (38) suitable for inducing a potential difference (?V) and positioned in a wall (40) between the ventilation space and the secondary air stream passage.