Vertical takeoff and landing aircraft

1. An aircraft defining a vertical direction and a longitudinal direction, the aircraft comprising:

a fuselage;

a propulsion system comprising a power source and a vertical thrust electric fan oriented to generate thrust along the vertical direction and powered by the power source; and

a wing extending from the fuselage and including the vertical thrust electric fan positioned at least partially therein, the wing comprising a variable geometry assembly having partial wing assembly, the partial wing assembly comprising a frame and a first member, the partial wing assembly moveable generally along the longitudinal direction when the variable geometry assembly is moved between a forward thrust position and a vertical thrust position, the first member moveable relative to the frame to form an exhaust path for the vertical thrust electric fan.

2. The aircraft of claim 1 ,

wherein the partial wing assembly is a forward partial wing assembly, and

wherein the variable geometry assembly further comprises an aft partial wing assembly,

wherein the aft partial wing assembly is also moveable generally along the longitudinal direction when the variable geometry assembly is moved between the forward thrust position and the vertical thrust position.

3. The aircraft of claim 2 ,

wherein the vertical thrust electric fan is substantially completely enclosed within the wing when the variable geometry assembly is in the forward thrust position, and

wherein the vertical thrust electric fan is substantially completely exposed when the variable geometry assembly is in the vertical thrust position.

4. The aircraft of claim 2 , wherein the aft partial wing assembly comprises a frame and a first member movable relative to the frame to form at least in part the exhaust path for the vertical thrust electric fan.

5. The aircraft of claim 1 , wherein the first member is configured to pivot downwardly along the vertical direction when the variable geometry assembly is moved to the vertical thrust position.

6. The aircraft of claim 1 ,

wherein the vertical thrust electric fan defines a fan axis,

wherein the first member of the partial wing assembly of the wing defines a first angle with the fan axis when the variable geometry assembly is in the forward thrust position and a second angle with the fan axis when the variable geometry assembly is in the vertical thrust position, and

wherein the first angle is greater than the second angle.

7. The aircraft of claim 6 ,

wherein the first angle is between about 75 degrees and about 105 degrees, and

wherein second angle is between about −30 degrees and 75 degrees.

8. The aircraft of claim 1 ,

wherein the partial wing assembly further comprises a second member,

wherein the first member is a bottom member and wherein the second member is a top member,

wherein the top member is movable relative to the frame of the partial wing assembly to at least partially form an inlet path for the vertical thrust electric fan.

9. The aircraft of claim 8 , wherein the top member is configured to pivot upwardly along the vertical direction when the variable geometry assembly is moved to the vertical thrust position.

10. The aircraft of claim 9 ,

wherein the vertical thrust electric fan defines a fan axis,

wherein the second member of the partial wing assembly defines a first angle with the fan axis when the variable geometry assembly is in the forward thrust position and a second angle with the fan axis when the variable geometry assembly is in the vertical thrust position, and

wherein the first angle is between about 75 degrees and about 105 degrees, and

wherein second angle is between about 120 degrees and about 180 degrees.

11. The aircraft of claim 1 ,

wherein the first member of the partial wing assembly defines a length,

wherein the vertical thrust electric fan defines a fan diameter, and

wherein the length is at least about 75 percent of the fan diameter.

12. The aircraft of claim 1 ,

wherein the vertical thrust electric fan is a first vertical thrust electric fan of a plurality of vertical thrust electric fans of the propulsion system,

wherein the variable geometry assembly substantially completely encloses the plurality of vertical thrust electric fans when in the forward thrust position, and

wherein the variable geometry assembly substantially completely exposes the plurality of vertical thrust electric fans when in the vertical thrust position.

13. The aircraft of claim 1 ,

wherein the wing comprises a rail and an actuator, and

wherein the frame of the partial wing assembly is movable along the rail by the actuator.

14. The aircraft of claim 1 ,

wherein the partial wing assembly comprises an actuator, and

wherein the actuator is configured to move the first member downwardly along the vertical direction when the variable geometry assembly is moved to the vertical thrust position.

15. The aircraft of claim 1 ,

wherein the wing is an aft wing,

wherein the vertical thrust electric fan is a first vertical thrust electric fan, and

wherein the aircraft further comprises:

a second wing coupled to and extending from the fuselage,

wherein the propulsion system further comprises a second vertical thrust electric fan integrated into the second wing and oriented to generate thrust along the vertical direction, the second wing comprising a variable geometry assembly having a partial wing assembly, the partial wing assembly comprising a frame and a first member, the partial wing assembly of the second wing moveable generally along the longitudinal direction when the variable geometry assembly of the second wing is moved between a forward thrust position and a vertical thrust position, the first member moveable relative to the frame to form at least in part an exhaust path for the second vertical thrust electric fan.

16. The aircraft of claim 1 ,

wherein the vertical thrust electric fan is a first vertical thrust electric fan of a plurality of vertical thrust electric fans of the propulsion system, and

wherein the plurality of vertical thrust electric fans are arranged along a length of the wing.

17. The aircraft of claim 16 , wherein each of the plurality of electric fans are fixed in orientation within the wing.

18. The aircraft of claim 1 ,

wherein the hybrid electric propulsion system further comprises a combustion engine and a forward thrust propulsor,

wherein an electric power source is an electric machine driven by the combustion engine, and

wherein the forward thrust propulsor is selectively or permanently mechanically coupled to the combustion engine.

19. A wing for an aircraft including a fuselage and a propulsion system and defining a vertical direction and a longitudinal direction, the wing comprising:

a plurality of vertical thrust electric fans positioned at least partially within the wing and arranged along a length of the wing; and

a variable geometry assembly having partial wing assembly, the partial wing assembly comprising a frame and a first member, the partial wing assembly moveable generally along the longitudinal direction when the variable geometry assembly is moved between a forward thrust position and a vertical thrust position, the first member moveable relative to the frame to form an exhaust path for at least one of the plurality of vertical thrust electric fans.

20. The wing of claim 19 ,

wherein the partial wing assembly is a forward partial wing assembly, and

wherein the variable geometry assembly further comprises an aft partial wing assembly,

wherein the aft partial wing assembly is also moveable generally along the longitudinal direction when the variable geometry assembly is moved between the forward thrust position and the vertical thrust position, and

wherein the aft partial wing assembly comprises a frame and a first member movable relative to the frame to form at least in part the exhaust path for the at least one of the plurality of vertical thrust electric fans.