Vertical takeoff and landing aircraft
A method for operating a vertical takeoff and landing aircraft includes modifying a first variable component of a wing associated with a first portion of the plurality of vertical thrust electric fans relative to a second variable component of the wing associated with a second portion of the plurality of vertical thrust electric fans to adjust an exposure ratio of the first portion of the plurality of vertical thrust electric fans relative to the second portion of the plurality of vertical thrust electric fans.
1. A method for operating a vertical takeoff and landing aircraft, the aircraft comprising a fuselage, a wing extending from the fuselage, and a propulsion system having a plurality of vertical thrust electric fans arranged along the wing, the method comprising:
modifying a first variable component of the wing associated with a first portion of the plurality of vertical thrust electric fans relative to a second variable component of the wing associated with a second portion of the plurality of vertical thrust electric fans to adjust an exposure ratio of the first portion of the plurality of vertical thrust electric fans relative to the second portion of the plurality of vertical thrust electric fans, wherein the first variable component and the second variable component each include first and second partial wing assemblies that translate in opposing directions to define a respective exposure area therebetween.
2. The method of claim 1 , wherein modifying the first variable component relative to the second variable component comprises positioning the first variable component in a forward thrust position.
3. The method of claim 2 , wherein positioning the first variable component in the forward thrust position comprises substantially completely enclosing the first portion of the plurality of vertical thrust electric fans.
4. The method of claim 2 , wherein modifying the first variable component relative to the second variable component further comprises positioning the second variable component in a vertical thrust position to define a diffusion area ratio, wherein the diffusion area ratio is greater than 1:1.
5. The method of claim 4 , wherein positioning the second variable component in the vertical thrust position comprises substantially completely exposing the second portion of the plurality of vertical thrust electric fans in the wing.
6. The method of claim 4 , further comprising:
providing the first portion of the plurality of vertical thrust electric fans with a first amount of electrical power and providing the second portion of the plurality of vertical thrust electric fans with a second amount of electrical power, and wherein the first amount of electrical power is less than the second amount of electrical power.
7. The method of claim 1 , wherein modifying the first variable component relative to the second variable component comprises positioning the first variable component in a middle position, and wherein positioning the first variable component in the middle position comprises partially exposing the first portion of the plurality of vertical thrust electric fans and partially enclosing the first portion of the plurality of vertical thrust electric fans.
8. The method of claim 1 , wherein the first variable component is spaced from the second variable component along a length of the wing.
9. The method of claim 1 , wherein each of the plurality of vertical thrust electric fans are fixed in orientation within the wing and arranged substantially linearly along the length of the wing.
10. The method of claim 1 , wherein the first variable component of the wing is a first partial wing assembly, wherein the second variable component of the wing is a second partial wing assembly.
11. The method of claim 1 , wherein the wing is a starboard wing, wherein the plurality of vertical thrust electric fans is a first plurality of vertical thrust electric fans, wherein the aircraft further comprises a port wing extending from the fuselage, wherein the propulsion system includes a second plurality of vertical thrust electric fans arranged along the port wing, and wherein the method further comprises:
modifying a first variable component of the port wing associated with a first portion of the second plurality of vertical thrust electric fans relative to a second variable component of the port wing associated with a second portion of the second plurality of vertical thrust electric fans to adjust an exposure ratio of the first portion of the second plurality of vertical thrust electric fans relative to the second portion of the second plurality of vertical thrust electric fans.
12. A method for operating a vertical takeoff and landing aircraft, the aircraft comprising a fuselage, a wing extending from the fuselage, and a propulsion system having a plurality of vertical thrust electric fans arranged along the wing, the method comprising:
modifying a first diffusion assembly of the wing associated with a first portion of the plurality of vertical thrust electric fans relative to a second diffusion assembly of the wing associated with a second portion of the plurality of vertical thrust electric fans to adjust an effective thrust profile of the first portion of the plurality of vertical thrust electric fans relative to an effective thrust profile of the second portion of the plurality of vertical thrust electric fans, wherein modifying the first variable component relative to the second variable component comprises positioning the first diffusion assembly in an extended position to define a diffusion area ratio is greater than 1:1.
13. The method of claim 12 , wherein modifying the first diffusion assembly relative to the second diffusion assembly further comprises positioning the second diffusion assembly in a retracted position.
14. The method of claim 12 , wherein modifying the first diffusion assembly relative to the second diffusion assembly comprises modifying a diffusion area ratio of the first diffusion assembly relative to a diffusion area ratio of the second diffusion assembly.
15. The method of claim 12 , wherein the first variable component is spaced from the second variable component along a length of the wing.
16. The method of claim 12 , wherein each of the plurality of vertical thrust electric fans are fixed in orientation within the wing and arranged substantially linearly along the length of the wing.
17. The method of claim 12 , wherein the first variable component of the wing is a first partial wing assembly, wherein the second variable component of the wing is a second partial wing assembly.
18. An aircraft defining a vertical direction comprising:
a fuselage;
a propulsion system comprising a power source, a first pair of vertical thrust electric fans driven by the power source, and a second pair of vertical thrust electric fans driven by the power source;
a port wing extending from the fuselage, the first pair of vertical thrust electric fans arranged along a length of the port wing, the port wing comprising a first variable component including a forward partial wing assembly and aft partial wing assembly extending over each of the first pair of vertical thrust electric fans; and
a starboard wing extending from the fuselage, the second pair of vertical thrust electric fans arranged along a length of the starboard wing, the port starboard comprising a second variable component including a forward partial wing assembly and aft partial wing assembly extending over each of second pair of vertical thrust electric fans; the first variable component moveable relative to the second variable component to adjust an exposure ratio of the first portion of the plurality of vertical thrust electric fans relative to the second portion of the plurality of vertical thrust electric fans.