Features of the Aircraft Design Essay Example | Topics and Well Written Essays - 2250 words

Features of the Aircraft Design - Essay ExampleAlthough composite materials weigh little than aluminum and have more corrosion resistance, which will lower maintenance, composite materials also have more failure characteristics in high-energy crashes (Langevin, 2003). Composite materials atomic number 18 brittle, and lack plasticity following an impact, so that a change in configuration may be needed in an aircraft design to ensure that crashworthiness criteria are met. There are load-limiting devices that preempt be implemented so that the oodles transmitted to passengers during a crash will be minimized. The structural assembly can also be modified to decrease transmitted loads. Aircraft subfloor systems can be developed with high-strength materials that hold the passenger seats during impact, and also contain a crushable forge that will absorb energy. The crushable layer is most important in the vertical direction, for improving human tolerance of the impact. This subfloor p latform will also distribute loads across the fuselage evenly. Energy absorbing seats are also effective at reducing loads transmitted to passengers. A comparison of two comparable real-life crash events shows that energy absorbing seats and restraint systems can mean the difference between walking away and not surviving (Langevin, 2003). Another outlook of an aircraft designs crashworthiness is its ditchability, or its ability to emergency land in water. There is usually a great loss of life in ditching all the same statistics show a 60% survivability during ditching (Kebabjian, 2006) - some sources list a much higher survivability rate. Intentional ditching of commercial aircraft is rare and often occurs after fuel enervation small aircraft ditching is much more common. As far as aircraft design considerations go, large underwing turbofans have been seen as having problematic ditchability (Fall-back System..., 1999). In our aircraft design, engines mount above or on the wing, a nd there shouldnt be the same ditchability problem.