Propulsion system including a turbine engine
A propulsion system and a method of operating the propulsion system. The propulsion system includes a first turbine engine, a second turbine engine, and a lubrication system. The lubrication system supplies a lubricant to the first turbine engine and the second turbine engine. The lubrication system includes one or more first lubricant sensors that sense information about the lubricant to the first turbine engine and one or more second lubricant sensors that sense information about the lubricant to the second turbine engine. The first controller and the second controller receive the information of the lubricant from the first lubricant sensors and the second lubricant sensors. The first controller controls the lubrication system to supply the lubricant to the second turbine engine based on the sensed information about the lubricant in the second turbine engine received at the first controller when the second turbine engine is shut down.
1 . A propulsion system comprising:
a first turbine engine comprising:
a first turbo-engine;
a first propulsor that is drivingly coupled to the first turbo-engine;
a first electric machine configured to power the first propulsor when the first turbo-engine is shut down; and
a first controller configured to control the first turbine engine;
a second turbine engine comprising:
a second turbo-engine;
a second propulsor that is drivingly coupled to the second turbo-engine;
a second electric machine configured to power the second propulsor when the second turbo-engine is shut down; and
a second controller configured to control the second turbine engine; and
a lubrication system configured to supply a lubricant to the first turbine engine and the second turbine engine, the lubrication system including a plurality of lubricant sensors including one or more first lubricant sensors that are configured to sense information about the lubricant to the first turbine engine and one or more second lubricant sensors that are configured to sense information about the lubricant to the second turbine engine,
wherein the first controller and the second controller are configured receive the information of the lubricant from the one or more first lubricant sensors and the one or more second lubricant sensors, and the first controller is configured to control the lubrication system to supply the lubricant to the second turbine engine based on the sensed information about the lubricant in the second turbine engine received at the first controller when the second turbine engine is shut down.
2 . The propulsion system of claim 1 , wherein each of the plurality of lubricant sensors includes redundant sensing elements and discrete outputs that are electrically isolated from each other.
3 . The propulsion system of claim 1 , wherein each of the plurality of lubricant sensors includes a chip detector that is configured to detect failures of components in the lubrication system.
4 . The propulsion system of claim 1 , wherein the one or more first lubricant sensors each includes four communication outputs including two communication outputs to the first controller and two communication outputs to the second controller for sending the information about the lubricant in the first turbine engine to the first controller and the second controller.
5 . The propulsion system of claim 4 , wherein the one or more second lubricant sensors each includes four communication outputs including two communication outputs to the second controller and two communication outputs to the first controller for sending the information about the lubricant in the second turbine engine to the second controller and the first controller.
6 . The propulsion system of claim 1 , further comprising an auxiliary lubrication system that is configured to supply the lubricant to at least one of the first turbine engine or the second turbine engine when a failure occurs in the lubrication system.
7 . The propulsion system of claim 6 , wherein the auxiliary lubrication system includes an auxiliary pump and an auxiliary lubricant valve, the auxiliary lubricant valve is configured to open and the auxiliary pump is configured to pump the lubricant through the auxiliary lubricant valve to the at least one of the first turbine engine or the second turbine engine when the failure occurs in the lubrication system.
8 . The propulsion system of claim 1 , wherein the one or more first lubricant sensors each includes two communication outputs to the first controller for sending the information about the lubricant in the first turbine engine to the first controller.
9 . The propulsion system of claim 8 , wherein the one or more second lubricant sensors each includes two communication outputs to the second controller for sending the information about the lubricant in the second turbine engine to the second controller.
10 . The propulsion system of claim 9 , further including a data communication bus that is configured to provide data communication between the first controller and the second controller, the first controller is configured to send the information about the lubricant in the first turbine engine to the second controller.
11 . A method of operating a propulsion system including a first turbine engine, a second turbine engine, and a lubrication system, the method comprising:
operating the first turbine engine, the first turbine engine comprising a first turbo-engine, a first propulsor, a first electric machine, and a first controller;
operating the second turbine engine, the second turbine engine comprising a second turbo-engine, a second propulsor, a second electric machine, and a second controller;
powering the first propulsor with the first electric machine when the first turbo-engine is shut down;
powering the second propulsor with the second electric machine when the second turbo-engine is shut down;
supplying a lubricant to the first turbine engine and the second turbine engine with the lubrication system, the lubrication system including one or more first lubricant sensors and one or more second lubricant sensors;
sensing information about the lubricant in the first turbine engine with the one or more first lubricant sensors;
receiving the information about the lubricant in the first turbine engine at the first controller;
sensing information about the lubricant in the second turbine engine with the one or more second lubricant sensors;
receiving the information about the lubricant in the second turbine engine at the second controller; and
controlling the lubrication system with the first controller to supply the lubricant to the second turbine engine based on the sensed information about the lubricant in the second turbine engine received at the first controller when the second turbine engine is shut down.
12 . The method of claim 11 , wherein each of the one or more first lubricant sensors and the one or more second lubricant sensors includes redundant sensing elements and discrete outputs that are electrically isolated from each other.
13 . The method of claim 11 , further comprising detecting failures of components in the lubrication system with a chip detector of each of the one or more first lubricant sensors and the one or more second lubricant sensors.
14 . The method of claim 11 , wherein the one or more first lubricant sensors each includes four communication outputs including two communication outputs to the first controller and two communication outputs to the second controller, the method further comprising sending the information about the lubricant in the first turbine engine to the first controller and the second controller.
15 . The method of claim 14 , wherein the one or more second lubricant sensors each includes four communication outputs including two communication outputs to the second controller and two communication outputs to the first controller, the method further comprising sending the information about the lubricant in the second turbine engine to the second controller and the first controller.
16 . The method of claim 11 , further comprising supplying the lubricant with an auxiliary lubrication system of the lubrication system to at least one of the first turbine engine or the second turbine engine when a failure occurs in the lubrication system.
17 . The method of claim 16 , further comprising opening an auxiliary lubricant valve of the auxiliary lubrication system, and pumping the lubricant with an auxiliary pump of the auxiliary lubrication system through the auxiliary lubricant valve to the at least one of the first turbine engine or the second turbine engine when the failure occurs in the lubrication system.
18 . The method of claim 11 , wherein the one or more first lubricant sensors each includes two communication outputs to the first controller, the method further comprising sending the information about the lubricant in the first turbine engine to the first controller via the two communication outputs.
19 . The method of claim 18 , wherein the one or more second lubricant sensors each includes two communication outputs to the second controller, the method further comprising sending the information about the lubricant in the second turbine engine to the second controller via the two communication outputs.
20 . The method of claim 19 , further including a data communication bus that provides data communication between the first controller and the second controller, the method further comprising sending the information about the lubricant in the first turbine engine from the first controller to the second controller.