| 摘要 |
The present invention relates to a method and to apparatus (9) for controlling and regulating a rotorcraft turbine engine (1) provided with an electronic control and regulation computer (3) that receives signals relating to monitored parameters of said turbine engine (1). The apparatus is remarkable in that it is provided alarm means (4) controlled by said electronic computer (3) via an analog connection (8) to operate whenever an event occurs that might diminish the safety of said rotorcraft.
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