Tail sitter vehicle with aerial and ground refueling system

Patent metadata

Field	Value
Publication number	US-10106274-B2
Application number	US-201615070599-A
Country	US
Kind code	B2
Filing date	Mar 15, 2016
Priority date	Mar 30, 2015
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

An aircraft is provided and includes a fuselage, first and second wings extending outwardly from opposite sides of the fuselage, proprotors operably disposed on each of the first and second wings to drive vertical take-off and landing aircraft operations and horizontal flight aircraft operations and a refueling system including at least one fuel tank disposed in at least one or more of the fuselage, the first wing or the second wing and a refueling apparatus. The refueling apparatus is coupled to the at least one fuel tank such that fuel is movable with respect to the at least one fuel tank during aircraft ground and aerial operations.

First claim

What is claimed is:

1. An aircraft, comprising:
a fuselage;
first and second wings extending outwardly from opposite sides of the fuselage;
proprotors operably disposed on each of the first and second wings to drive vertical take-off and landing aircraft operations and horizontal flight aircraft operations;
alighting elements disposed at a trailing side of the first and second wings for aircraft support during the ground operations; and
a refueling system including at least one fuel tank disposed in at least one or more of the fuselage, the first wing or the second wing and a refueling apparatus,
the refueling apparatus being coupled to the at least one fuel tank such that fuel is movable with respect to the at least one fuel tank during aircraft ground and aerial operations.

2. The aircraft according to claim 1 , wherein each of the first and second wings comprises:
a main wing;
a winglet coupled to a distal end of the main wing; and
a hinge by which the winglet is pivotable about the distal end of the main wing.

3. The aircraft according to claim 1 , wherein the proprotors comprise foldable rotor blades.

4. The aircraft according to claim 1 , wherein the fuselage comprises:
a wing section disposed along a plane of the first and second wings; and
a bulged section disposed to extend away from the plane.

5. The aircraft according to claim 4 , wherein the fuselage further comprises:
a stores support coupled to the wing section; and
an external tank element coupled to a distal end of the stores support.

6. The aircraft according to claim 5 , wherein the fuselage comprises a plurality of stores supports and a corresponding number of external tank elements.

7. The aircraft according to claim 6 , wherein the plurality of the stores supports and the corresponding number of the external tank elements are arrayed on opposite sides of the plane.

8. The aircraft according to claim 4 , wherein the refueling apparatus comprises an inlet fluidly communicative with the at least one fuel tank.

9. The aircraft according to claim 4 , wherein the refueling apparatus comprises a hose and drogue system fluidly communicative with the at least one fuel tank.

10. The aircraft according to claim 9 , wherein the hose and drogue system is housed in or on the fuselage.

11. The aircraft according to claim 1 , further comprising an auxiliary power unit configured to power a fuel transfer between the at least one fuel tank and the refueling apparatus.

12. An aircraft, comprising:
a fuselage;
first and second wings extending outwardly from opposite sides of the fuselage;
proprotors operably disposed on each of the first and second wings to drive vertical take-off and landing aircraft operations and horizontal flight aircraft operations;
alighting elements disposed at a trailing side of the first and second wings for aircraft support during the ground operations; and
a refueling system including at least one fuel tank disposed in at least one or more of the fuselage, the first wing or the second wing and a refueling apparatus,
the refueling apparatus being coupled to the at least one fuel tank such that fuel is movable with respect to the at least one fuel tank during aircraft ground and aerial operations and comprising:
an inlet fluidly communicative with the at least one fuel tank; and
a hose and drogue system fluidly communicative with the at least one fuel tank.

13. The aircraft according to claim 12 , wherein the fuselage comprises:
a wing section disposed along a plane of the first and second wings;
a bulged section disposed to extend away from the plane;
a plurality of stores supports coupled to opposite sides of the wing section; and
a plurality of external tank elements respectively coupled to respectively distal ends of each of the stores supports.

14. The aircraft according to claim 12 , wherein the hose and drogue system is housed in or on the fuselage.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Alber Mark R
• Gayagoy Charles
• Parkhurst Jeffrey
• Tiongson Glenn D

Classifications

• B64C2201/108

  Operations & Transport · mapped topic

• B64C2201/104

  Operations & Transport · mapped topic

• B64C23/072

  the wing tip airfoil devices being moveable in their entirety · CPC title

• B64D39/00

  Refuelling during flight · CPC title

• B64D37/16

  Filling systems (ground installations for fuelling aircraft B64F1/28) · CPC title