Aircraft fitted with an independent drive device
View Patent ↗An aircraft having wheels with hydraulically-actuating friction brakes and independent drives for driving the wheels in rotation and enabling the aircraft to move in stages of independent drive when engines of the aircraft are inactive. A main hydraulic circuit with a pressure source powers the brakes when the pressure source is active; with an alternative braking circuit for enabling the brake system at least when the engines of the aircraft are stopped. The alternative braking circuit includes an accumulator that is used for parking braking and is kept under pressure by the pressure source of the main circuit when the pressure source is active. An auxiliary hydraulic circuit pressurized by an auxiliary pump and power system enables the independent drives to be actuated. The auxiliary hydraulic circuit is connected to the alternative braking circuit to maintain an operating pressure in the accumulator of the alternative braking circuit.
1. An aircraft having wheels fitted with hydraulically-actuating friction brake means and also hydraulically-actuated independent drive means for driving the wheels in rotation and enabling the aircraft to move in stages of independent drive in which the engines of the aircraft are inactive, wherein the aircraft is fitted with at least:
a main hydraulic circuit including a first pressure source, activated by at least one of the main aircraft engines, that powers the brake means when the first pressure source is active;
an alternative braking circuit for enabling brake means to be actuated at least when the engines of the aircraft are stopped, the alternative braking circuit including an accumulator that is used for parking braking; and
an auxiliary hydraulic circuit pressurized by an auxiliary pump means activated by an auxiliary power unit of the aircraft to enable the independent drive means to be actuated;
the auxiliary hydraulic circuit being connected to the alternative braking circuit to maintain an operating pressure in the accumulator of the alternative braking circuit,
wherein the accumulator is kept under pressure by the first pressure source of the main circuit when the first pressure source is active; and
wherein the accumulator is kept under pressure by the auxiliary pump means when the first pressure source is inactive.
2. An aircraft according to claim 1 , wherein the auxiliary hydraulic circuit and the alternative braking circuit are connected together by means of a hydraulic connection including an expander.