ELEVON DESIGN FOR ALL-AXIS CONTROL IN A BLENDED WING BODY AIRCRAFT
Aspects relate to airplanes having a blended wing body. A blended wing body may include a fuselage and a port wing and a starboard wing continuously coupled to the fuselage and a nose section. A midship control surface may be disposed on a trailing edge of the blended wing body and centered between the port wing and the starboard wing.
1 . An aircraft comprising:
a blended wing body, wherein the blended wing body comprises:
a fuselage;
a port wing and a starboard wing continuously coupled to the fuselage and a nose section; and
a midship control surface disposed on a trailing edge of the fuselage, centered between the port wing and the starboard wing, wherein the entirety of the trailing edge of the fuselage is substantially at the same height.
2 . The aircraft of claim 1 , wherein the midship control surface is the aftmost control surface on the fuselage.
3 . The aircraft of claim 2 , wherein no other control surface on the fuselage is in line with the midship control surface.
4 . The aircraft of claim 1 , wherein the trailing edge of the fuselage is convex.
5 . The aircraft of claim 1 , wherein there are no vertical stabilizers on the fuselage.
6 . The aircraft of claim 1 , wherein the blended wing body has no clear demarcation between the wings and fuselage along a trailing edge of the aircraft.
7 . The aircraft of claim 1 , wherein the midship control surface is aft of a rear pressure bulkhead of the aircraft.
8 . The aircraft of claim 1 , wherein there is no aft door through a rear pressure bulkhead of the aircraft.
9 . The aircraft of claim 1 , wherein the chord length of the midship control surface is between 3.1% and 3.5% of the centerbody chord length.
10 . The aircraft of claim 1 , wherein the midship control surface has elevator functionality.
11 . The aircraft of claim 1 , wherein the midship control surface has braking functionality.
12 . The aircraft of claim 1 , further comprising an inboard port control surface on the trailing edge of the port side of the fuselage, further comprising an inboard starboard control surface on the trailing edge of the starboard side of the fuselage.
13 . The aircraft of claim 12 , wherein the blended wing body has no clear demarcation between the wings and fuselage along a trailing edge of the aircraft, wherein the inboard port control surface on the trailing edge of the port side of the fuselage is in a transition region between the fuselage and the port wing, and wherein the inboard starboard control surface on the trailing edge of the starboard side of the fuselage is in a transition region between the fuselage and the starboard wing.
14 . The aircraft of claim 12 , wherein the inboard port control surface is a control surface doublet, and wherein the inboard starboard control surface is a starboard control surface doublet.
15 . The aircraft of claim 12 , wherein the inboard port and starboard control surfaces have elevator functionality.
16 . The aircraft of claim 12 , wherein the inboard port and starboard control surfaces have aileron functionality.
17 . The aircraft of claim 1 , further comprising an outboard port control surface on the trailing edge of the port wing, further comprising an outboard starboard control surface on the trailing edge of the starboard wing.
18 . The aircraft of claim 16 , wherein the outboard port control surface is a control surface triplet, and wherein the outboard starboard control surface is a control surface triplet.
19 . The aircraft of claim 18 , wherein the outboard port control surface and the outboard starboard control surface each comprise a first triangular shaped control surface, a quadrilateral shaped control surface, and a second triangular shaped control surface.
20 . The aircraft of claim 19 , wherein the first triangular shaped control surface, the quadrilateral shaped control surface, and the second triangular shaped control surface of each of the outboard port control surface and the outboard starboard control surface are positioned such that a side of the first triangular control surface is adjacent to and parallel to a first side of the quadrilateral control surface, and a side of the second triangular control surface is adjacent to and parallel to a second side of the quadrilateral control surface, wherein the first side of the quadrilateral control surface and the second side of the quadrilateral control surface are not adjacent sides.