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Pages 53-77

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From page 53...
... 53 A P P E N D I X F Study on Emergency Evacuation Challenges on Large Transport Aircraft
From page 54...
... 54 Executive Summary The purpose of this study was to investigate emergency evacuations challenges from large transport aircraft. The world's largest commercial aircraft, the Airbus A380, is considered as a very large transport aircraft (VLTA)
From page 55...
... 55 Background 1. Large Aircraft The Boeing 747, which has been in use since 1970, features a partial upper deck, but does not contain as many passengers as the A380 will on the upper deck.
From page 56...
... 56 2. Emergency Evacuation Inflatable Slides As dictated by Code of Federal Regulations (14CFR & 25.810)
From page 57...
... 57 a. Airbus A380 Slide Characteristics Figure 2 shows the evacuation slides of the Airbus A380.
From page 58...
... 58 presented at the International Aircraft Fire and Cabin Safety Research Conference in Atlantic City in 2001. He developed a model to analyze how factors such as slide design, visibility and passenger safety instruction would influence an individual's performance and observed the reactions to different situations.
From page 59...
... 59 3 . Figure 4: Unit normal and unit tangent vectors at point (x,y)
From page 60...
... 60 These unit directional vectors can be written as: j ds dy i ds dx T ˆ ˆ (unit tangent) j ds dx i ds dy N ˆ ˆ (unit normal)
From page 61...
... 61 Then, using the relation: dt ds v or v dsdt , we obtain that: ds vd ds dv v vds dv dt dv )
From page 62...
... 62 Then, by applying Euler-Lagrange equation: 0) '( FyFy dx d , we obtain a second order differential equation.
From page 63...
... 63 theorem, the x component has then a maximum value of 5 .
From page 64...
... 64 results are the coefficient of friction and initial velocity of an individual at the top of an evacuation slide. Figure 6 shows an optimal shape of the A380 upper and lower deck slides as well as of a B747 upper decks slide.
From page 65...
... 65 0 1 2 3 4 5 6 7 8 9 10 11 0 0.5 1 1.5 2 2.5 Time (seconds)
From page 66...
... 66 0 1 2 3 4 5 6 7 8 9 10 11 0 0.5 1 1.5 2 2.5 Time (seconds)
From page 67...
... 67 0 1 2 3 4 5 6 7 8 9 10 0 0.5 1 1.5 2 2.5 Time (seconds)
From page 68...
... 68 One event occurred on August 19, 2005 in Agana, Guam. A Boeing 747-200 landed with its nose gear retracted and an emergency evacuation was initiated.
From page 69...
... 69 Figure 10: Slide emergency evacuation of a Boeing 747-438 (Sydney, Australia, The most serious injury occurred to one woman while she was on an over wing slide at the time it deflated. She got a fractured vertebra that required surgery as she landed heavily on the tarmac.
From page 70...
... 70 2. Airbus A380 Certification As mentioned, any new aircraft to enter service must pass the certification test.
From page 71...
... 71 Figure 11: Airbus A380 Certification Test (Source: http://www.airporttech.tc.faa.gov/safety/patterson1.asp) Importance, Relevance, and Potential Impact of the Study Safety standards have been maintained throughout the years in order to provide safe and efficient passenger evacuations.
From page 72...
... 72 A number of factors affect the safe evacuation of passengers. As mentioned, passenger's reactions and decisions will have an effect on the overall process.
From page 73...
... 73 lift and therefore improved fuel economy. Passenger's flights on blended wing aircraft will be able to carry 800 passengers in a double-deck cabin.
From page 74...
... 74 Eelman, S., Schmitt, D., Becker, A., Granzeier, W., "Future Requirements and Concepts for Cabins of Blended Wing Body Configurations – A scenario approach". Journal of Air Transportation, Vol.
From page 75...
... 75 Wallace, James, "Aerospace Notebook: This is only a test with 850 passengers", 2 February 2005, http://seattlepi.nwsource.com/business/210321_air02.html Appendix A- Airbus A380 Slides Lengths and Angles Source: A380 Cabin Evacuation System (Jean-Michel GOVAERE, A380 Chief Airworthiness Engineer, AIRBUS SAS) Appendix B - Matlab Code % Maryline Rassi, 07/31/2007 clear all; close all; clc; % 1.
From page 77...
... 77 plot(y,v) xlabel('y [m]

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