초록 ▼

The invention relates to a system and to a method for controlling an aircraft engine starter-generator. The system comprises a transmission box (20) with a fixed gear ratio intended to be mechanically coupled to a turbine shaft (12) of the engine to allow the latter to be started, a gearbox (40) wit

The invention relates to a system and to a method for controlling an aircraft engine starter-generator. The system comprises a transmission box (20) with a fixed gear ratio intended to be mechanically coupled to a turbine shaft (12) of the engine to allow the latter to be started, a gearbox (40) with multiple gear ratios that is mechanically coupled to a pinion of the transmission box, a starter-generator (30) mechanically coupled to a pinion of the gearbox, and means for instigating a change in gear ratio of the gearbox according to the mode of operation of the starter-generator.

대표청구항 ▼

1. A pipe of circular overall cross section, fitted with an airflow rate regulating device comprising a circular flap with a diameter substantially corresponding to an inner diameter of the pipe, pivotably mounted around an axis substantially perpendicular to an axis of the pipe, and intended to be

1. A pipe of circular overall cross section, fitted with an airflow rate regulating device comprising a circular flap with a diameter substantially corresponding to an inner diameter of the pipe, pivotably mounted around an axis substantially perpendicular to an axis of the pipe, and intended to be actuated via a motor, wherein the airflow rate regulating device includes at least one regulating member including an outer wall having a middle zone of cylindrical overall shape bearing against an inner wall of the pipe, on either side of which first and second zones are positioned withdrawn from said inner wall of the pipe, so as to respectively form first and second lateral airflow channels, the regulating member also having an inner wall with a hollow zone designed so that, when the flap pivots, an edge of the flap is flush with or positioned near the corresponding inner wall. 2. The pipe according to claim 1, wherein the airflow rate regulating device includes first and second regulating members arranged opposing one another and generally symmetrically relative to the swivel axis of the flap. 3. The pipe according to claim 1, wherein each regulating member has, in top view, a generally triangular or trapezoidal shape, having a wide end facing the axis of rotation side of the flap and a narrower end, facing the opposite side. 4. The pipe according to claims 1, wherein the inner wall has, in the hollow zone, a shape of a sphere portion whereof a diameter substantially corresponds to the diameter of the flap. 5. The pipe according to claims 1, wherein the inner wall has, in the hollow zone, the shape of a sphere portion whereof a diameter is larger than the diameter of the flap, the flap being mobile between a first position in which it extends substantially perpendicularly to the axis of the pipe and in which the edge of the flap is flush with the inner wall, and at least one second position in which the edge of the flap is further away from the inner wall. 6. The pipe according to claim 1, wherein each regulating member includes a hollow inner space as well as at least one orifice connecting an inside of the pipe to the hollow space. 7. The pipe according to claim 6, wherein each hollow space is fitted with pressure measuring means. 8. The pipe according to claim 1, wherein a motor actuating the pivoting of the flap is housed, at least partially, in the flap, at the axis thereof. 9. The pipe according to claim 7, wherein a position of the flap is calculated according to pressure measurements obtained by the measuring means. 10. The pipe according to claim 1, wherein first and second withdrawn zones of each regulating member are formed by planar zones.