Emergency egress in a blended wing body aircraft
Technologies for providing emergency egress routes for a blended wing body aircraft are described herein. In some examples, the emergency egress routes are through a side cabin bulkhead and aft one or more cargo holds. In some examples, the blended wing body aircraft has wings that are high geometry wings. In these examples, the emergency egress routes do not penetrate an aft spar, reducing weight and increasing the integrity of the aircraft.
1. A blended wing body (BWB) aircraft comprising:
a main cabin configured to hold passengers during flight;
at least one cargo hold located outboard of the main cabin; and
at least one egress route through a side cabin bulkhead;
wherein the side cabin bulkhead is located aft of the at least one cargo hold, at least a portion of the side cabin bulkhead is located forward a trailing edge of at least a wing, and the at least one egress route does not penetrate a rear spar of the aircraft.
2. The BWB aircraft of claim 1 , wherein the at least one egress route comprises a first door between the main cabin and the at least one cargo hold and a second door at a tunnel exit on an outer lower surface of the at least a wing of the BWB aircraft.
3. The BWB aircraft of claim 2 , wherein the second door, when opened for egress from the BWB aircraft, has a ramp suitable for passenger travel.
4. The BWB aircraft of claim 2 , further comprising an inflatable slide proximate to the second door, wherein the inflatable slide is used to facilitate travel of passengers from the BWB aircraft.
5. The BWB aircraft of claim 1 , further comprising a second egress route through the side cabin bulkhead forward of the at least one cargo hold.
6. The BWB aircraft of claim 2 , wherein the at least one cargo hold is pressurized.
7. The BWB aircraft of claim 2 , wherein the BWB aircraft is a single deck BWB aircraft.
8. The BWB aircraft of claim 1 , wherein the at least one cargo hold has a height substantially no less than the main cabin.
9. The BWB aircraft of claim 1 , further comprising at least one wing continuously coupled to a nose of the BWB aircraft, the at least one wing having a high wing geometry located above a center of height of the BWB aircraft.