Development of a Component Head Injury Criteria (HIC ... - FAA
Development of a Component Head Injury Criteria (HIC ... - FAA
Development of a Component Head Injury Criteria (HIC ... - FAA
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Figure 8. Pressure Sensor<br />
Once the accumulator is filled to the desired pressure, the system is ready to be activated via the<br />
computer. Doing so initiates a 5-second countdown and automatic triggering <strong>of</strong> the camera and<br />
data acquisition system. The system then triggers the solid-state relays, which open the main<br />
supply valve from the accumulator to the actuator, thus driving the pendulum arm into the test<br />
article. A sensor mounted on the pendulum arm base measures angular position from which the<br />
computer calculates both peak velocity and peak time (figure 9).<br />
Figure 9. Computer Screen With Posttest Data<br />
5. PRELIMINARY EVALUATION OF THE NHCT AT NIAR.<br />
A preliminary evaluation <strong>of</strong> the NHCT was conducted at NIAR [11]. The NHCT had been<br />
previously calibrated and evaluated for a setback distance <strong>of</strong> 35 inches. Although this is the<br />
most common seating configuration, other distances related to various cabin class configurations<br />
7