Fuel System
A fuel system includes a centrifugal pump which pressurizes and delivers fuel that is supplied to an aircraft engine, and a transmission which connects the engine and the centrifugal pump to each other, is able to regulate a gear ratio and which modifies and transmits a rotational speed of rotational power that is output from the engine to the centrifugal pump.
1. A fuel system comprising:
a centrifugal pump which pressurizes and delivers fuel that is supplied to an aircraft engine;
a transmission which connects the engine and the centrifugal pump to each other, is able to regulate a gear ratio and modifies and transmits a rotational speed of a rotational power that is output from the engine to the centrifugal pump;
a metering valve which regulates a flow amount of the fuel that is discharged from the centrifugal pump;
a throttling valve which is provided downstream of the metering valve and regulates pressure of the fuel that passes through the metering valve; and
a transmission controller that controls the gear ratio in the transmission such that a difference of the pressure of the fuel upstream of the metering valve and the pressure of the fuel downstream of the throttling valve is constant.
2. The fuel system according to claim 1 , further comprising:
an inducer which is disposed on the upstream of the centrifugal pump and drives proportionally to the rotational power which is output from the engine.
3. A fuel system comprising:
a centrifugal pump which pressurizes and delivers fuel that is supplied to an aircraft engine;
a transmission which connects the engine and the centrifugal pump to each other, is able to regulate a gear ratio and modifies and transmits a rotational speed of a rotational power that is output from the engine to the centrifugal pump;
a metering valve which regulates a flow amount of the fuel that is discharged from the centrifugal pump;
a throttling valve which is provided downstream of the metering valve and regulates pressure of the fuel that passes through the metering valve;
a pressure difference sensor which measures a difference between the pressure of the fuel upstream of the metering valve and the pressure of the fuel downstream of the throttling valve;
an arithmetic control member which compares a setting value and the measurement result of the pressure difference sensor; and
a transmission controller that controls the gear ratio in the transmission based on the comparison result of the arithmetic control member in accordance with the difference of the pressure of the fuel upstream of the metering valve and the pressure of the fuel downstream of the throttling valve.
4. The fuel system according to claim 3 , further comprising:
an inducer which is disposed on the upstream of the centrifugal pump and drives proportionally to the rotational power which is output from the engine.
5. A fuel system comprising:
a centrifugal pump which pressurizes and delivers fuel that is supplied to an aircraft engine;
a transmission which connects the engine and the centrifugal pump to each other, is able to regulate a gear ratio and modifies and transmits a rotational speed of a rotational power that is output from the engine to the centrifugal pump;
a metering valve which regulates a flow amount of the fuel that is discharged from the centrifugal pump;
a throttling valve which is provided downstream of the metering valve and regulates pressure of the fuel that passes through the metering valve;
a pressure difference sensor which measures a difference between the pressure of the fuel upstream of the metering valve and the pressure of the fuel downstream of the throttling valve, and a difference between the pressure of the fuel upstream of the metering valve and the pressure of the fuel between the metering valve and the throttling valve;
an arithmetic control member which compares a setting value to the measurement result of the pressure difference sensor and controls an opening area of the throttling valve; and
a transmission controller that controls the gear ratio in the transmission based on the comparison result of the arithmetic control member such that the difference between the pressure of the fuel upstream of the metering valve and the pressure of the fuel downstream of the throttling valve, and the difference between the pressure of the fuel upstream of the metering valve and the pressure of the fuel between the metering valve and the throttling valve are respectively constant.
6. The fuel system according to claim 5 , further comprising:
an inducer which is disposed on the upstream of the centrifugal pump and drives proportionally to the rotational power which is output from the engine.