Oil pipe assembly
An oil pipe assembly for a gas turbine engine. The oil pipe assembly includes a first pipe that defines a first fluid passage between an oil supply and a bearing chamber, and a second pipe that houses the first pipe and defines a second fluid passage between the first pipe and the second pipe that is supplied with cooling air. The oil pipe assembly also includes a restrictor that extends from the second pipe and restricts the passage of fluid from the second fluid passage before it flows into a breather. Pressure and temperature sensors) are located adjacent the restrictor to detect and measure changes in air pressure and air temperature adjacent the restrictor from which a controller identifies whether a leak has occurred in the first pipe or the second pipe. A method for detecting a leak in the oil pipe assembly, and a gas turbine are also described.
1. An oil pipe assembly comprising:
a first pipe configured to define a first fluid passage between an oil supply and a bearing chamber of a gas turbine engine;
a second pipe that houses the first pipe and is configured to define a second fluid passage between the first pipe and the second pipe that is supplied with cooling air;
a restrictor that extends from the second pipe and is configured to restrict the passage of fluid from the second fluid passage before it flows into a breather of the gas turbine engine;
a pressure sensor and a temperature sensor which are located adjacent the restrictor to detect and measure changes in air pressure and air temperature adjacent the restrictor; and
a controller that signals that a leak has occurred in the first pipe or the second pipe when the pressure sensor and the temperature sensor detect an increase in air pressure and air temperature adjacent the restrictor.
2. The oil pipe assembly of claim 1 , wherein the oil pipe assembly is configured so that if the first pipe leaks, oil from the first pipe is directed to flow into a cavity so that the oil can be recovered and fed back into an oil system of the gas turbine engine.
3. The oil pipe assembly of claim 1 , wherein the oil pipe assembly is configured so that if the second pipe leaks, air from the second pipe is directed to flow into the breather so that the air can be vented overboard.
4. The oil pipe assembly of claim 1 , wherein the restrictor is an elongate element that includes a restrictor fluid passage where the average diameter of the restrictor fluid passage is smaller than the average diameter of the second fluid passage.
5. A method for detecting a leak in an oil pipe of a gas turbine engine, the method comprising the steps of:
(a) providing the oil pipe assembly of claim 1 ;
(b) detecting and measuring any changes in air pressure and air temperature adjacent the restrictor of the oil pipe assembly; and
(c) signalling that a leak has occurred in the first pipe or the second pipe of the oil pipe assembly when the pressure sensor and the temperature sensor of the oil pipe assembly detect an increase in air pressure and air temperature adjacent the restrictor.
6. The method of claim 5 , further comprising identifying from the pressure and air temperature measurements whether a leak has occurred in the first pipe or the second pipe.
7. A gas turbine engine that includes the oil pipe assembly of claim 1 .
8. The gas turbine engine of claim 7 wherein the gas engine comprises:
an engine core comprising a turbine, a compressor, and a core shaft connecting the turbine to the compressor;
a fan located upstream of the engine core, the fan comprising a plurality of fan blades; and
a gearbox that receives an input from the core shaft and outputs drive to the fan so as to drive the fan at a lower rotational speed than the core shaft.