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74 Gas Turbine Handbook: Principles and Practices<br />

Figure 5-2. Temperature-power-speed interrelationships.<br />

From the turn of the century through the late 1970s, control<br />

systems operated only in real time with no ability to store or retrieve<br />

data. Hydromechanical controls had to be calibrated frequently<br />

(weekly in some applications) and were subject to contamination and<br />

deterioration due to wear. A requirement for multiple outputs (i.e.,<br />

fuel flow control and compressor bleed-air flow-control) required completely<br />

independent control loops. Coordinating the output of multiple<br />

loops, through cascade control, was a difficult task and often resulted<br />

in a compromise between accuracy and response time. In addition,<br />

many of the tasks had to be performed manually. For example, station<br />

valves, prelube pumps, and cooling water pumps were manually<br />

placed into the running position prior to starting the gas generator.<br />

Also protection devices were limited. The margin between temperature<br />

control set points and safe operating turbine temperatures was<br />

necessarily large because the hydromechanical controls could not react<br />

quick enough to limit high turbine temperatures, or to shutdown<br />

the gas generator, before damage would occur.

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