Air vehicle having strakes

• US 9,132,904 B2
• Filed: 07/17/2013
• Issued: 09/15/2015
• Est. Priority Date: 07/18/2012
• Status: Active Grant

• Current Assignee: Hybrid Air Vehicles Limited
• Original Assignee: Hybrid Air Vehicles Limited
• Inventors: Durham, Michael
• Primary Examiner(s): Dinh, Tien
• Assistant Examiner(s): Giczy, Alexander V
• Application Number:
  US13/944,141
• Publication Number:
  US 20140021298A1
• Time in Patent Office: 790 Days
• Field of Search: 244/30, 244/123.11
• US Class Current: 1/1
• CPC Class Codes: B64B 1/02 Non-rigid airships B64B1/58 takes precedence; balloons B64B1/40
• CPC Class Codes: B64B 1/20 provided with wings or stabilising surfaces tail unit construction B64B1/10; movable control surfaces B64B1/12
• CPC Class Codes: B64B 2201/00 Hybrid airships, i.e. airships where lift is generated aerodynamically and statically

Abstract

An air vehicle has a gas-filled hull of a flexible sheet material. Strakes extend along an exterior of the hull, each strake comprising a gas-filled tube of a sheet of a flexible sheet material. A rigid board extends outwardly from the gas-filled tube and away from the vehicle. A further sheet of a flexible sheet material extends from one side of the strake over the board to another side of the strake, to provide a strake that is generally triangular in cross section.

Claims

1. An air vehicle having a gas-filled hull of a first flexible sheet, wherein a plurality of strakes extend along an exterior of the hull, each strake comprising:

a gas-filled tube of a further flexible sheet,

a rigid board, projecting outwardly from the gas-filled tube and away from the air vehicle, and

an outer flexible sheet extending from one side of the gas-filled tube over the board to another side of the gas-filled tube,

wherein each strake has a generally triangular cross section.

2. An air vehicle according to claim 1, wherein the tube is filled with air.

3. An air vehicle according to claim 1, wherein a part of a periphery of the gas-filled tube is provided by the first flexible sheet of the hull of the air vehicle.

4. An air vehicle according to claim 1, wherein the hull is contoured and flattened, and includes a pair of longitudinally extending side lobes defining, on an underside of the hull, a longitudinally extending central recess.

5. An air vehicle according to claim 1, wherein each strake extends from a vicinity behind a forward motor of the air vehicle to a vicinity a forward edge of a stabilizing fin of the air vehicle.

17. An air vehicle according to claim 4, further including:

a payload module or a fuel module or both a payload module and a fuel module disposed in the central recess.

6. An air vehicle comprising:

a gas-filled hull formed of a first flexible sheet,

first and second strakes extending along opposite sides of an exterior of the hull,

each strake comprising;

an elongated gas-filled tube of a further flexible sheet adjacent the hull of the air vehicle,

a rigid board abutting and projecting outwardly from the gas-filled tube and away from the hull of the air vehicle, and

an outer flexible sheet extending from one side of the_elongated gas-filled tube over an edge of the rigid board to another side of the elongated gas-filled tube, thereby to define each strake as having a generally triangular cross section.

7. An air vehicle according to claim 6, wherein the first flexible sheet, the further flexible sheet and the outer flexible sheet include a reinforced sheet material, a high strength laminated fabric, or both reinforced sheet material and high strength laminated fabric.

8. An air vehicle according to claim 6, wherein each strake extends rearwardly on the air vehicle from a forward motor of the air vehicle to a vicinity of a forward edge of a stabilizing fin of the air vehicle.

9. An air vehicle according to claim 6, wherein the first flexible sheet of the hull of the air vehicle provides part of a periphery of the elongated gas-filled tube of the strake.

10. An air vehicle according to claim 6, wherein the hull is contoured and flattened so as to have a width and to have a height that is less than the width, the hull including a pair of elongated side lobes extending longitudinally along the hull to define, on an underside of the hull, a longitudinally extending central recess between the side lobes.

18. An air vehicle according to claim 10, further including:

a payload module or a fuel module or both a payload module and a fuel module disposed in the central recess.

11. An air vehicle comprising:

a gas-filled hull formed of a first flexible sheet,

first and second strakes extending along opposite sides of an exterior of the hull,

each strake comprising;

an elongated gas-filled tube of a further flexible sheet adjacent the hull of the air vehicle,

a rigid board having first and second opposing edges, with the first edge of the rigid board disposed abutting and projecting outwardly from the gas-filled tube and away from the hull of the air vehicle, and

an outer flexible sheet extending from one side of the elongated gas-filled tube over the second edge of the rigid board to another side of the elongated gas-filled tube, thereby to define each strake as having a generally triangular cross section,

wherein the rigid board is in compression and the outer flexible sheet is in tension when the hull and the elongated tube are filled with gas.

12. An air vehicle according to claim 11, wherein the first flexible sheet, the further flexible sheet and the outer flexible sheet include a reinforced sheet material, a high strength laminated fabric, or both reinforced sheet material and high strength laminated fabric.

13. An air vehicle according to claim 11, wherein each of the first and second strakes extends rearwardly on the hull of the air vehicle from a forward motor of the air vehicle to a vicinity of a forward edge of a stabilizing fin of the air vehicle.

14. An air vehicle according to claim 11, wherein the flexible sheet material of the hull of the air vehicle provides part of a periphery of the elongated gas-filled tube of the strake.

15. An air vehicle according to claim 11, wherein the hull is contoured and flattened so as to have a width and to have a height that is less than the width, the hull including a pair of elongated side lobes extending longitudinally along the hull to define, on an underside of the hull, a longitudinally extending central recess between the side lobes.

16. An air vehicle according to claim 15, further including:

a payload module or a fuel module or both a payload module and a fuel module disposed in the central recess.