MODULAR ARTICULATED-WING AIRCRAFT

• US 20100193625A1
• Filed: 06/27/2006
• Published: 08/05/2010
• Est. Priority Date: 07/07/2005
• Status: Active Grant

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: Geoffrey S. Sommer
• Inventors: Sommer, Geoffrey S.
• Granted Patent: US 7,789,339 B2
• Time in Patent Office: Days
• US Class Current: 244/2
• CPC Class Codes: B64C 37/02 Flying units formed by separate aircraft towing B64D3/00; aircraft transported by aircraft B64D5/00; air-refuelling B64D39/00
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 20/40 Modular UAVs
• CPC Class Codes: B64U 20/50 Foldable or collapsible UAVs with frangible components B64U20/30
• CPC Class Codes: B64U 2201/102 adapted for flying in formations
• CPC Class Codes: B64U 50/13 using external fans or propellers
• CPC Class Codes: B64U 50/31 generated by photovoltaics
• CPC Class Codes: B64U 60/40 foldable or retractable
• CPC Class Codes: B64U 70/20 for releasing or capturing UAVs in flight by another aircraft
• CPC Class Codes: B64U 70/60 Take-off or landing of UAVs from a runway using their own power
• CPC Class Codes: B64U 80/82 Airborne vehicles

Abstract

Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

Claims

1. An autonomous modular flyer operable to loiter over an area of interest at a first high altitude, comprising:

an airborne object having two wings, each wing having a wingtip, the wingtips being operably joinable to at least one other autonomous modular flyer'"'"'s wingtips to form an aggregation when a first predetermined condition is met, and being operably disaggregable from the at least one other autonomous modular flyer'"'"'s wingtips when a second predetermined condition is met;

wherein each said autonomous modular flyer includes first and second side-force controllers being respectively located on the bottom of the port and starboard wings, the side-force controllers being configured to impart selective aerodynamic forces along a lateral axis of the flyer resulting in lateral translation during flyer aggregation, each side-force controller being in line with the center of gravity of the flyer,

wherein the aggregation forms a multiple-articulated flying system having a high aspect ratio wing platform, operable to loiter over the area of interest at an altitude at least as high as the first high altitude, and

wherein, when changing directions, the autonomous modular flyers in the aggregation are operable to disaggregate prior to, and re-aggregate once, each autonomous modular flyer in the aggregation has individually changed directions.

2. The autonomous modular flyer of claim 1, being further operable to match its airspeed with a prevailing headwind so as to loiter over the area of interest.

3. The autonomous modular flyer of claim 1, wherein the autonomous modular flyer has both an altitude ceiling high in Earth'"'"'s stratosphere and structural robustness in Earth'"'"'s troposphere.

4. The autonomous modular flyer of claim 1, further comprising a wingtip hinge on at least one wingtip allowing two operably joined modular flyers to flap about the wingtip hinge with respect to each other.

5. The autonomous modular flyer of claim 1, wherein aggregations of larger numbers of modular flyers occur at sequentially higher altitudes.

6. The autonomous modular flyer of claim 1, wherein the second predetermined condition includes one or more of:

a loading event above a given load threshold, a gust above a gust threshold, a turn of the multiple-articulated flying system, a span shear above a span shear threshold, an instruction for at least one of the modular flyers to undertake a remote surveillance activity, and an instruction for at least one of the modular flyers to move closer to the area of interest.

7. The autonomous modular flyer of claim 1, wherein the multiple-articulated flying surface of claim 1 is operable to reaggregate based at least on a third predetermined condition.

8. The autonomous modular flyer of claim 7, wherein the third predetermined condition includes one or more of:

a second predetermined condition that previously was met no longer is met, and at least one modular flyer being destroyed, recalled, and/or no longer functional.

9. The autonomous modular flyer of claim 1, further comprising insolation circuitry to power each modular element and/or the multiple-articulated flying system.

10. The autonomous modular flyer of claim 9, wherein the insolation circuitry comprises a photovoltaic array, an electronic controller to condition and manage the power, and an electrical energy storage mechanism.

11. The autonomous modular flyer of claim 1, further comprising a flight controller operable to calculate an equilibrium ceiling altitude and to instruct the autonomous modular flyer to climb or descend to the equilibrium ceiling altitude.

12. The autonomous modular flyer of claim 1, further comprising a sensor operable to gather data relating to the area of interest.

13. The autonomous modular flyer of claim 12, wherein the sensor is further operable to work as an element in a sensor array when a multiple-articulated flying system is formed, each element in the sensor array working in synchrony with each other element in the sensor array.

24. The autonomous modular flyer of claim 1, wherein each wingtip has a pitch freedom selected to enable span-wise wing twist of the autonomous modular flyer to be changeable based on operating conditions.

25. The autonomous modular flyer of claim 1, wherein the autonomous modular flyer is configured to store and operate on different types and/or quantities of batteries, the type and/or quantity of battery being selected based on seasonal changes, and

wherein the autonomous modular flyer is further configured to disaggregate from an aggregation, if formed, to obtain a new battery pack, and then re-form the aggregation.

14. A method of forming a multiple-articulated flying system having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude, the method comprising:

providing at least two autonomous modular flyers, each having two wings with wingtips thereon;

joining the wingtips of the at least two autonomous modular flyers when a first predetermined condition is met to form an aggregation; and

disaggregating the wingtips of the at least two autonomous modular flyers when a second predetermined condition is met,

wherein each said autonomous modular flyer includes first and second side-force controllers being respectively located on the bottom of the port and starboard wings, the side-force controllers being configured to impart selective aerodynamic forces along a lateral axis of the flyer resulting in lateral translation during flyer aggregation, each side-force controller being in line with the center of gravity of the flyer, and

wherein, when changing directions, the autonomous modular flyers in the aggregation are operable to disaggregate prior to, and re-aggregate once, each autonomous modular flyer in the aggregation has individually changed directions.

16. The method of claim 14, further comprising matching the multiple-articulated flying system'"'"'s airspeed with a prevailing headwind and/or making large orbits in order to loiter over the area of interest.

17. The method of claim 14, further comprising allowing joined wingtips to flap about wingtip hinges attached to the wingtips.

19. The method of claim 14, further comprising powering the autonomous modular flyers and/or the multiple-articulated flying system by using solar-electric energy.

20. The method of claim 14, further comprising calculating an equilibrium ceiling altitude for the autonomous modular flyer, and altering the autonomous modular flyer'"'"'s altitude to the equilibrium ceiling altitude.

15. (canceled)

18. The method of claim 15, further comprising re-aggregating disaggregated autonomous modular flyers.

21. (canceled)

22. (canceled)

23. (canceled)

26. (canceled)