Vertical takeoff and landing aircraft having a diffusion assembly for lift fan(s)

Patent metadata

Field	Value
Publication number	US-11124307-B2
Application number	US-201816042403-A
Country	US
Kind code	B2
Filing date	Jul 23, 2018
Priority date	Jul 21, 2017
Publication date	Sep 21, 2021
Grant date	Sep 21, 2021

Abstract

An aircraft includes a fuselage; a propulsion system including a power source and a plurality of vertical thrust electric fans driven by the power source; and a wing extending from the fuselage. The plurality of vertical thrust electric fans are arranged along the wing, the wing including one or more components being moveable to selectively expose the plurality of vertical thrust electric fans, the wing further including a diffusion assembly positioned downstream of at least one vertical thrust electric fan of the plurality of vertical thrust electric fans, the diffusion assembly defining a diffusion area ratio greater than 1:1 and less than about 2:1.

First claim

What is claimed is:

1. An aircraft defining a vertical direction, the aircraft comprising:
a fuselage;
a propulsion system comprising a power source and a plurality of vertical thrust electric fans driven by the power source; and
a wing extending from the fuselage, the plurality of vertical thrust electric fans arranged along the wing, the wing comprising:
a variable geometry assembly being moveable to selectively expose the plurality of vertical thrust electric fans, the variable geometry assembly including a forward partial wing assembly generally linearly movable between a forward thrust position and a vertical thrust position and an aft partial wing assembly generally linearly movable between the forward thrust position and the vertical thrust position; and
a diffusion assembly positioned downstream of at least one vertical thrust electric fan of the plurality of vertical thrust electric fans, the diffusion assembly having a first member of the forward partial wing assembly and a first member of the aft partial wing assembly, wherein the first member of the forward partial wing assembly moves with the forward partial wing assembly and rotates about a first joint from a forward thrust position to a vertical thrust position and the first member of the aft partial wing assembly moves with the aft partial wing assembly and rotates about a second joint from a forward thrust position to a vertical thrust position, and wherein the diffusion assembly defines a diffusion area ratio greater than 1:1 and less than about 2:1.

2. The aircraft of claim 1 , wherein the diffusion area ratio defined by the diffusion assembly of the wing is greater than about 1.15:1 and less than about 1.85:1.

3. The aircraft of claim 1 , wherein the at least one vertical thrust electric fan defines a power loading during vertical thrust operations greater than about 3 pounds per horsepower and less than about 15 pounds per horsepower.

4. The aircraft of claim 1 , wherein the at least one vertical thrust electric fan defines a power loading during vertical thrust operations greater than about 4 pounds per horsepower and less than about 10 pounds per horsepower.

5. The aircraft of claim 1 , wherein the diffusion assembly is positioned downstream of each of the plurality of vertical thrust electric fans, and wherein the diffusion area ratio is defined relative to each of the plurality of vertical thrust electric fans.

6. The aircraft of claim 1 , wherein the plurality of vertical thrust electric fans are fixed in orientation for providing thrust generally along the vertical direction.

7. The aircraft of claim 1 , wherein the plurality of vertical thrust electric fans are integrated into the wing and arranged substantially linearly along a length of the wing.

8. The aircraft of claim 1 , wherein the wing defines an aspect ratio greater than about 3:1.

9. The aircraft of claim 1 , wherein the diffusion assembly includes a plurality of diffusion assemblies, wherein each diffusion assembly is associated with one of the vertical thrust electric fans of the plurality of vertical thrust electric fans.

10. The aircraft of claim 1 , wherein the diffusion assembly is positioned downstream of two or more of the plurality of vertical thrust electric fans.

11. The aircraft of claim 1 , wherein the diffusion assembly is a fixed diffusion assembly positioned within the wing of the aircraft.

12. The aircraft of claim 1 , wherein the diffusion assembly comprises one or more movable components movable to a vertical thrust position to define the diffusion area ratio.

13. The aircraft of claim 1 , further comprising:
a first member actuator operably coupled with the first member of the forward partial wing assembly, wherein the first member actuator is positioned between the first member of the forward partial wing assembly and the forward partial wing assembly in the forward thrust position and forward of the first member of the forward partial wing assembly in a longitudinal direction in the vertical thrust position.

14. An aircraft defining a vertical direction, the aircraft comprising:
a fuselage;
an electric or hybrid-electric propulsion system, the propulsion system comprising a power source and a plurality of vertical thrust electric fans driven by the power source; and
a wing extending from the fuselage, the plurality of vertical thrust electric fans arranged along the wing, the wing comprising:
a variable geometry assembly moveable to selectively expose the plurality of vertical thrust electric fans, the variable geometry assembly including a forward partial wing assembly and an aft partial wing assembly; and
a diffusion assembly positioned downstream of at least one vertical thrust electric fan of the plurality of vertical thrust electric fans, the diffusion assembly including a first member that is rotatable between a forward thrust position and a vertical thrust position about a joint, the joint slidable along a longitudinal direction with the forward partial wing assembly, wherein the at least one vertical thrust electric defines a power loading during vertical thrust operations greater than about 3 pounds per horsepower and less than about 15 pounds per horsepower.

15. The aircraft of claim 14 , wherein the at least one vertical thrust electric fan defines a power loading during vertical thrust operations greater than about 4 pounds per horsepower and less than about 10 pounds per horsepower.

16. The aircraft of claim 14 , wherein the diffusion assembly defines a diffusion area ratio greater than 1:1 and less than about 2:1.

17. The aircraft of claim 16 , wherein the diffusion area ratio defined by the diffusion assembly of the wing is greater than about 1.15:1 and less than about 1.85:1.

18. The aircraft of claim 14 , wherein the diffusion assembly is a fixed diffusion assembly positioned within the wing of the aircraft.

19. The aircraft of claim 14 , further comprising:
a first member actuator operably coupled with the first member of the forward partial wing assembly, wherein the first member actuator is positioned between the first member of the forward partial wing assembly and the forward partial wing assembly in the forward thrust position and forward of the first member of the forward partial wing assembly in a longitudinal direction in the vertical thrust position.

20. An aircraft defining a vertical direction, the aircraft comprising:
a fuselage;
a propulsion system comprising a power source and a plurality of vertical thrust electric fans driven by the power source; and
a wing extending from the fuselage, the plurality of vertical thrust electric fans arranged along the wing, the wing comprising a variable geometry assembly being moveable to selectively expose the plurality of vertical thrust electric fans, the wing further comprising a diffusion assembly positioned downstream of at least one vertical thrust electric fan of the plurality of vertical thrust electric fans and operably coupled with the variable geometry assembly such that the diffusion assembly translates with the variable geometry assembly between a forward thrust position and a vertical thrust position, the diffusion assembly having a member that is rotatable between forward thrust position and a vertical thrust position when the variable geometry assembly is in the vertical thrust position.

Assignees

• Gen Electric

Inventors

• Murrow Kurt David
• Breeze-Stringfellow Andrew
• Zatorski Darek Tomasz
• Barone Dominic

Classifications

• B64D27/31

  within, or attached to, wings · CPC title

• B64D35/023

  of series-parallel type · CPC title

• B64D27/357

  using batteries · CPC title

• B64D27/33

  Hybrid electric aircraft · CPC title

• B64D27/406

  Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links · CPC title