| 摘要 |
A gas turbine engine (20) is provided having a control and health monitoring system (240) that includes an engine control module (200). At least one electronic component electronically coupled to the engine control module (200). The at least one electronic component includes an electronic module (232). The system further includes an isolation rail (230) extending through the gas turbine engine (20). The at least one control component (204) is electronically coupled to the engine control module (200) through the isolation rail (230). The electronic module (232) is in thermal communication with isolation rail (230). |
