| 摘要 |
An arrangement for monitoring engine parameters in gas-turbine-driven helicopters, having in each case at least one display instrument, one device for producing a warning signal and one computer. The computer has inputs for the engine parameters to be monitored and has outputs for the limit display means and for at least one device for producing a warning signal. The displays for the instantaneous values and limit values are combined on one display instrument and consist of a pointer for a value which is proportional to the instantaneously emitted overall power from the engines and/or for the most critical instantaneous value of the engine parameters, of a pointer-like mask for the absolute limits, and of a flat mask for the limits which may be exceeded for only a limited time. |
