Emergency exit system
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[0047] exist Figures 1a to 1e , figure 2 , Figure 3a and 3b , Figures 5a to 5c as well as Figure 9 Various embodiments of an emergency exit system 10 suitable for use in an aircraft are shown in . The emergency exit system 10 can be used as an overwing exit in Figure 10 Aircraft 100 is shown for use.
[0048] The emergency exit system will be explained in detail below Figures 1a to 1e The first embodiment shown in . The emergency system 10 includes a first primary structural frame 12 and a second primary structural frame 14 extending substantially parallel to the first primary structural frame 12, see especially Figure 1b . The two primary structural frames 12, 14 of the emergency exit system 10 are configured for use in the state in which the emergency exit system 10 is assembled in the aircraft 100 (such as Figures 1a to 1e ) form part of the main structure of the aircraft 100 .
[0049] A door opening 16 is disposed between the first primary structural fram...
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