Method for detecting a failure in a motive flow valve of an aircraft engine fuel circuit
View Patent ↗A method detects a failure in a fuel return valve of an aircraft engine fuel circuit. A fuel system is connected to a fuel tank of the circuit and includes a high-pressure pump delivering a flow rate to an actuating cylinder, a cutoff valve capable of feeding the actuating cylinder disposed in a feed pipe of the engine; a fuel return pipe; a fuel return valve arranged to switch between an open position and a closed position. The method includes starting the engine at an engine speed; increasing the engine speed until a flow rate reaches a predefined value sufficient for opening the cutoff valve; measuring the position of the actuating cylinder and an engine speed corresponding to the opening of said cutoff valve.
1. A method for detecting a failure of a motive flow valve of an aircraft engine fuel circuit, said fuel circuit including:
a fuel tank;
an engine fuel system connected to the fuel tank, said fuel system including a high-pressure pump delivering a flow rate Q, depending on an engine speed of said engine, to an actuating ram capable of actuating variable geometries, a cutoff valve capable of supplying the actuating ram positioned in a supply pipe of said engine;
a fuel return pipe connected downstream of the high-pressure pump and upstream of the cutoff valve and, to the fuel tank;
a motive flow valve arranged to switch between an open position and a closed position, said motive flow valve being capable of blocking, in the closed position, the fuel return pipe and, in the open position, to put into communication the fuel return pipe with the fuel tank;
the method comprising the following steps, implemented in a calculator:
starting the engine at an engine speed N0;
increasing the engine speed until the flow rate Q reaches a predetermined value Q0 sufficient for opening the cutoff valve;
measuring the position of the actuating ram and of the engine speed N corresponding to the opening of said cutoff valve; and based on the engine speed determining failure of the motive flow valve.
2. The method according to claim 1 , including a step of comparing the engine setting speed N corresponding to the opening of the valve to a predetermined threshold.
3. The method according to claim 2 , wherein, if the engine speed N thus measured is greater than the predetermined threshold, the method includes a step of detecting a failure of the motive flow valve.
4. The method according to claim 2 , wherein if the engine speed N thus measured is greater than 8% of the predetermined threshold, the method includes a step of detecting a failure of the motive flow valve.
5. The method according to claim 1 , wherein the position of the ram is measured by an LVDT type sensor.
6. The method according to claim 1 , wherein the predetermined flow rate value Q0 corresponds to a setting threshold of a spring of the cutoff valve.
7. A fuel circuit comprising:
a fuel tank;
an engine fuel system connected to the fuel tank, said fuel system including a high-pressure pump delivering a flow rate Q, depending on the engine speed of said engine, to an actuating ram capable of actuating variable geometries, a cutoff valve capable of supplying the actuating ram positioned in a supply pipe of said engine;
a fuel return pipe connected downstream of the high-pressure pump and upstream of the cutoff valve and on the other hand to the fuel tank;
a motive flow valve arranged to switch between an open position and a closed position, said motive flow valve being capable of blocking, in the closed position, the fuel return pipe and, in the open position, to put into communication the fuel return pipe with the fuel tank;
a calculator configured to implement the following steps:
starting the engine at an engine speed N0;
increasing the engine speed until the flow rate Q reaches a predetermined value Q0 sufficient for opening the cutoff valve;
measuring the position of the actuating ram and of the engine speed N corresponding to the opening of said cutoff valve; and based on the engine speed determining failure of the motive flow valve.
8. The fuel circuit according to claim 7 , wherein the high-pressure pump is a positive displacement pump.
9. An aircraft including an engine supplied with fuel by a fuel circuit according to claim 7 .