Method of extending aircraft undercarriages in emergency mode
View Patent ↗A method of actuating undercarriage latching boxes and associated hatch latching boxes of an aircraft in an emergency mode, the latching boxes having at least one feed port and at least one unlatching member that is operable when the port is fed with fluid under pressure, the aircraft also being provided with a hydraulic braking circuit. The method includes connecting at least one tapping circuit to the braking circuit of the aircraft in association with an isolation valve that is kept, in a normal mode, in an isolation state and that can be controlled to be placed in an open state in which at least some of the feed ports of the latching boxes are fed by the tapping circuit connected to the braking circuit.
1. A method of actuating undercarriage latching boxes and associated hatch latching boxes of an aircraft in an emergency mode, the latching boxes having at least one feed port and at least one unlatching member that is operable when the port is fed with fluid under pressure, the aircraft also being provided with a hydraulic braking circuit, the method comprising:
connecting at least one tapping circuit to the braking circuit of the aircraft in association with an isolation valve that is kept, in a normal mode, in an isolation state, and
controlling said isolation valve to be placed in an open state in which at least some of the feed ports of the latching boxes are fed by the tapping circuit connected to the braking circuit.
2. The method according to claim 1 , wherein the isolation valve is located directly in the tapping circuit.
3. The method according to claim 1 , wherein the aircraft has a single braking circuit, and wherein the single tapping circuit that is connected thereto feeds the ports of all of the latching boxes.
4. The method according to claim 1 , in which the aircraft has two hydraulic circuits defining two braking circuits, wherein a single tapping circuit is connected to one of the braking circuits in order to feed the ports of all of the latching boxes.
5. The method according to claim 1 , in which the aircraft has two hydraulic circuits defining two braking circuits, wherein two respective tapping circuits are connected to each of the braking circuits, one of them feeding the ports of the hatch latching boxes and the other of them feeding the ports of the undercarriage latching boxes.
6. The method according to claim 1 , in which the aircraft has two hydraulic circuits defining two braking circuits, wherein two respective tapping circuits are connected to each of the braking circuits, one of them feeding the ports of the main undercarriage latching boxes and of the associated hatch latching boxes, and the other feeding the ports of the nose undercarriage latching boxes and of the associated hatch latching boxes.