Ducted fan assembly for an aircraft

Patent metadata

Field	Value
Publication number	US-11634216-B2
Application number	US-202017036798-A
Country	US
Kind code	B2
Filing date	Sep 29, 2020
Priority date	Sep 29, 2020
Publication date	Apr 25, 2023
Grant date	Apr 25, 2023

Abstract

In an embodiment, a ducted fan assembly includes a housing that further includes a rotor. The ducted fan assembly also includes a plurality of stators that extend outward from the housing. The ducted fan assembly also includes a control vane pivotally attached to at least one of the plurality of stators. The ducted fan assembly also includes a rim that extends around at least a portion of a perimeter of the ducted fan assembly and is supported by the plurality of stators and the control vane, where the rim defines an opening surrounding at least a portion of the housing.

First claim

What is claimed is:

1. A ducted fan assembly comprising:
a housing comprising a rotor;
a plurality of stators that extend outward from the housing;
a control vane pivotally attached to at least one of the plurality of stators;
a rim that extends around at least a portion of a perimeter of the ducted fan assembly and is supported by the plurality of stators and the control vane, wherein the rim defines an opening surrounding at least a portion of the housing;
wherein the control vane is positioned aft of the rim;
wherein an outer edge of the control vane is coextensive with the rim in a direction perpendicular to a rotational plane of the rotor; and
a leading-edge bladder comprising a carcass and that is attached to the rim and extends around the at least a portion of a perimeter of the ducted fan assembly to form a leading edge of the ducted fan assembly, the leading-edge bladder configured to be filled with a gas;
wherein the carcass comprises a weakened section configured to bleed off pressure resulting from impact with a foreign object.

2. The ducted fan assembly of claim 1 , wherein the rim has greater rigidity than the leading-edge bladder.

3. The ducted fan assembly of claim 1 , wherein:
the rim comprises a frame made from at least one of a metal and a composite; and
the leading-edge bladder comprises a rubber polymer.

4. The ducted fan assembly of claim 3 , wherein the rubber polymer is reinforced with a fiber.

5. The ducted fan assembly of claim 1 , comprising a trailing-edge bladder that is attached to the ducted fan assembly on a side thereof opposite the rim such that the trailing-edge bladder forms a trailing edge of the ducted fan assembly, the trailing-edge bladder configured to be filled with a gas.

6. The ducted fan assembly of claim 5 , comprising a middle section that joins the leading-edge bladder and the trailing-edge bladder.

7. The ducted fan assembly of claim 1 , wherein the leading-edge bladder comprises a blow-off valve configured to bleed off pressure resulting from impact with a foreign object.

8. The ducted fan assembly of claim 1 , wherein the leading-edge bladder comprises a plurality of bladders that together extend around the at least a portion of a perimeter of the ducted fan assembly.

9. The ducted fan assembly of claim 1 , wherein the leading-edge bladder comprises a single contiguous bladder that extends around the at least a portion of a perimeter of the ducted fan assembly.

10. The ducted fan assembly of claim 1 , comprising a fan positioned over the housing and attached to the rotor, wherein the fan is adjacent to the rim such that the opening defined by the rim surrounds the fan.

11. The ducted fan assembly of claim 10 , wherein the fan comprises a plurality of blades that are each spaced from the rim such that, for each blade of the plurality of blades, a space between the blade and the rim is less than or equal to 0.25 inches.

12. A rotorcraft comprising a plurality of fan assemblies, each fan assembly comprising:
a housing comprising a rotor;
a plurality of stators that extend outward from the housing;
a control vane pivotally attached to at least one of the plurality of stators;
a rim that extends around at least a portion of a perimeter of the fan assembly and is supported by the plurality of stators and the control vane, wherein the rim defines an opening surrounding at least a portion of the housing;
a leading-edge bladder comprising a carcass and that is attached to the rim and extends around the at least a portion of a perimeter of the fan assembly to form a leading edge of the fan assembly, the leading-edge bladder configured to be filled with a gas;
wherein the control vane is positioned aft of the rim;
wherein an outer edge of the control vane is coextensive with the rim in a direction perpendicular to a rotational plane of the rotor; and
wherein the carcass comprises a weakened section configured to bleed off pressure resulting from impact with a foreign object.

13. The rotorcraft of claim 12 , wherein, for at least one fan assembly of the plurality of fan assemblies, the rim has greater rigidity than the leading-edge bladder.

14. The rotorcraft of claim 12 , wherein, for at least one fan assembly of the plurality of fan assemblies:
the rim comprises a frame made from at least one of a metal and a composite; and
the leading-edge bladder comprises a rubber polymer.

15. The rotorcraft of claim 12 , wherein each fan assembly of the plurality of fan assemblies comprises a trailing-edge bladder that is attached to the fan assembly on a side thereof opposite the rim such that the trailing-edge bladder forms a trailing edge of the fan assembly, the trailing-edge bladder configured to be filled with a gas.

16. The rotorcraft of claim 12 , wherein each fan assembly of the plurality of fan assemblies comprises a fan positioned over the housing and attached to the rotor, and wherein the fan is adjacent to the rim such that the opening defined by the rim surrounds the fan.

17. The rotorcraft of claim 16 , wherein, for each fan assembly of the plurality of fan assemblies, the fan comprises a plurality of blades that are each spaced from the rim such that, for each blade of the plurality of blades, a space between the blade and the rim is less than or equal to 0.25 inches.

18. The rotorcraft of claim 12 , wherein, for at least one fan assembly of the plurality of fan assemblies, the leading-edge bladder comprises a single contiguous bladder that extends around the at least a portion of a perimeter of the fan assembly.

19. The rotorcraft of claim 12 , at least one fan assembly of the plurality of fan assemblies comprising a trailing-edge bladder that is attached to the at least one fan assembly on a side thereof opposite the rim such that the trailing-edge bladder forms a trailing edge of the at least one fan assembly, the trailing-edge bladder configured to be filled with a gas.

Assignees

• Bell Textron Inc
• Textron Innovations Inc

Inventors

• Amante William Anthony
• Carr Timothy Brian

Classifications

• B64C27/20

  Rotorcraft characterised by having shrouded rotors, e.g. flying platforms · CPC title

• B64C11/001

  Shrouded propellers · CPC title

• B64C29/0033 Primary

  the propellers being tiltable relative to the fuselage · CPC title