AIRCRAFT FUSELAGES

摘要

Aircraft fuselages are disclosed herein. An example apparatus includes a fuselage of an aircraft having a first section and a second section to which a tail assembly is to be coupled. The second section is aft of the first section and is to extend to at least a trailing edge of a horizontal stabilizer of the tail assembly. A first width of the first section decreases from a front to a rear of the first section, and a second width of the second section is substantially constant.

主权项

1. An aircraft comprising:
a tail portion of a fuselage, the tail portion including a first section, a second section aft of the first section, and a third section aft of the second section, a first width of the first section decreasing from a front to a rear of the first section, a second width of the second section being substantially constant, and a third width of the third section decreasing from a front to a rear of the third section; and a horizontal stabilizer extending from the tail portion such that a trailing edge of the horizontal stabilizer extends from the tail portion at or fore an intersection of the second section and the third section and a leading edge of the horizontal stabilizer extends from the tail portion along the first section.