Pre-start motoring synchronization for multiple engines
An aspect includes a system for pre-start motoring control for multiple engines of an aircraft. The system includes a first engine starting system of a first engine and a controller. The controller is operable to control a motoring time of the first engine starting system relative to one or more other engine starting systems of one or more other engines of the aircraft by adjusting the motoring time of the first engine starting system within a tolerance of the motoring time of the one or more other engine starting systems in a pre-start motoring sequence.
1. A system for pre-start motoring control for multiple engines of an aircraft, the system comprising:
a first engine starting system of a first engine; and
a controller operable to control a motoring time of the first engine starting system relative to one or more other engine starting systems of one or more other engines of the aircraft by adjusting the motoring time of the first engine starting system within a tolerance of a motoring time of the one or more other engine starting systems in a pre-start motoring sequence based on comparing the motoring time of the first engine starting system with the motoring time of the one or more other engine starting systems.
2. The system as in claim 1 , wherein the motoring time of the first engine starting system is controlled relative to the one or more other engine starting systems by comparing a first value of the motoring time of the first engine starting system with a first value of the motoring time of the one or more other engine starting systems and selecting larger value as the motoring time for the first engine starting system and the one or more other engine starting systems.
3. The system as in claim 2 , wherein the controller provides the first value of the motoring time of the first engine starting system to one or more other controllers and receives the first value of the motoring time of the one or more other engine starting systems from the one or more other controllers.
4. The system as in claim 2 , wherein the controller maintains the motoring time of the first engine starting system as the first value of the motoring time of the first engine starting system based on determining that the first value of the motoring time of the first engine starting system is greater than or equal to the first value of the motoring time of the one or more other engine starting systems.
5. The system as in claim 1 , wherein the pre-start motoring sequence comprises simultaneous motoring of the first engine and the one or more other engines.
6. The system as is claim 1 , wherein the pre-start motoring sequence comprises sequential motoring of the first engine and the one or more other engines.
7. The system as in claim 1 , wherein the controller is operable to control the first engine starting system to maintain a starting spool speed of the first engine below a resonance speed during the motoring time of the first engine starting system.
8. The system as in claim 1 , wherein the controller is further operable to validate the motoring time of the one or more other engine starting systems and range limit the motoring time of the first engine starting system prior to performing motoring of the first engine during the pre-start motoring sequence.
9. A system of an aircraft, the system comprising:
a first engine system comprising a first gas turbine engine, a first starter, and a first controller operable to control the first starter to perform motoring of the first gas turbine engine in a pre-start motoring sequence; and
a second engine system comprising a second gas turbine engine, a second starter, and a second controller operable to control the second starter to perform motoring of the second gas turbine engine in the pre-start motoring sequence, wherein a motoring time of the first gas turbine engine is controlled within a tolerance of a motoring time of the second gas turbine engine by adjusting the motoring time of the first gas turbine engine relative to the motoring time of the second gas turbine engine based on comparing the motoring time of the first gas turbine engine with the motoring time of the second gas turbine engine.
10. The system of claim 9 , wherein at least one engine control interface coordinates the motoring time of the first gas turbine engine relative to the motoring time of the second gas turbine engine.
11. The system of claim 9 , wherein the first controller and the second controller exchange first values of the motoring time of the first gas turbine engine and the motoring time of the second gas turbine engine and select a larger value as the motoring time of the first gas turbine engine and the motoring time of the second gas turbine engine.
12. The system of claim 9 , wherein the pre-start motoring sequence comprises simultaneous motoring of the first gas turbine engine and the second gas turbine engine.
13. The system of claim 9 , wherein the pre-start motoring sequence comprises sequential motoring of the first gas turbine engine and the second gas turbine engine.
14. The system of claim 9 , wherein the motoring time of the first gas turbine engine and the motoring time of the second gas turbine engine are validated and range limited prior to performing motoring of the first gas turbine engine and the second gas turbine engine during the pre-start motoring sequence.
15. A method for pre-start motoring control for multiple engines of an aircraft, the method comprising:
determining, by a controller, a motoring time of a first engine starting system of a first engine;
comparing, by the controller, the motoring time of the first engine starting system with a motoring time of one or more other engine starting systems of one or more other engines of the aircraft; and
controlling the motoring time of the first engine starting system relative to a tolerance of the motoring time of the one or more other engine starting systems by adjusting the motoring time of the first engine starting system relative to the one or more other engine starting systems in a pre-start motoring sequence based on comparing the motoring time of the first engine starting system with the motoring time of the one or more other engine starting systems.
16. The method as in claim 15 , wherein the controller maintains the motoring time of the first engine starting system as a first value of the motoring time of the first engine starting system based on determining that the first value of the motoring time of the first engine starting system is greater than or equal to a first value of the motoring time of the one or more other engine starting systems.
17. The method as in claim 15 , wherein the pre-start motoring sequence comprises simultaneous motoring of the first engine and the one or more other engines.
18. The method as in claim 15 , wherein the pre-start motoring sequence comprises sequential motoring of the first engine and the one or more other engines.
19. The method as in claim 15 , further comprising controlling the first engine starting system to maintain a starting spool speed of the first engine below a resonance speed during the motoring time of the first engine starting system, and the motoring time of the first engine starting system is determined by the controller using a bowed rotor start risk model based on a target speed, a temperature at shutdown, a time of engine shutdown, a current engine temperature, and an ambient temperature.
20. The method as in claim 15 , further comprising:
validating the motoring time of the one or more other engine starting systems; and
range limiting the motoring time of the first engine starting system prior to performing motoring of the first engine during the pre-start motoring sequence.