In-flight loadable and refuelable unmanned aircraft system for continuous flight
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64D-037/00
B64C-001/22
출원번호
US-0738227
(2000-12-15)
발명자
/ 주소
Henderson, J. Kirston
출원인 / 주소
Lockheed Martin Corporation
대리인 / 주소
Jackson Walker LLP
인용정보
피인용 횟수 :
14인용 특허 :
3
초록▼
A method for refueling and reloading an unmanned aircraft for continuous flight is disclosed herein wherein the unmanned aircraft is maintained and supported by a support aircraft. Both aircraft maintain cargo bays and in-flight operable doors located on the underside of each aircraft for the purpos
A method for refueling and reloading an unmanned aircraft for continuous flight is disclosed herein wherein the unmanned aircraft is maintained and supported by a support aircraft. Both aircraft maintain cargo bays and in-flight operable doors located on the underside of each aircraft for the purposes of docking and exchanging goods. Preferably the goods comprise loadable cartridges and may contain such items as weapons, cargo, or fuel for example. In one embodiment, when both aircraft are in a docked configuration for exchange of goods during flight, the in-flight operable doors open and the support aircraft is capable of loading such cartridges aboard the unmanned aircraft. When necessary the support aircraft may load gear for the purposes of landing the unmanned aircraft. Alternate methods of reloading an unmanned aircraft for continuous flight is disclosed wherein the unmanned aircraft does not have cargo bay doors and the aircraft is supported by a support aircraft.
대표청구항▼
1. A method of refueling an unmanned continuous flight aircraft, said unmanned aircraft comprising: an aircraft capable of multiple missions via continuous flight configured to dock to a support aircraft, both maintaining a payload bay on the bottom side of the aircraft; comprising the step of:
1. A method of refueling an unmanned continuous flight aircraft, said unmanned aircraft comprising: an aircraft capable of multiple missions via continuous flight configured to dock to a support aircraft, both maintaining a payload bay on the bottom side of the aircraft; comprising the step of: maintaining said unmanned aircraft in an inverted flight pattern; docking both said aircraft in a configuration for refueling via a docking means; and exchanging fuel via both said payload bays. 2. The method of refueling an unmanned aircraft of claim 1, wherein said cargo bay of the continuous flight aircraft is located at the aircraft center of mass. 3. The method of refueling an unmanned aircraft of claim 2, wherein said cargo bay of the continuous flight aircraft is capable of dropping or exchanging weapons. 4. The method of refueling an unmanned aircraft of claim 2, wherein said cargo bay of the continuous flight aircraft is capable of dropping or exchanging cargo. 5. The method of refueling an unmanned aircraft of claim 4, wherein said cargo is in the form of a cartridge. 6. The method of refueling an unmanned aircraft of claim 5, wherein said cartridges comprise either one of the following: weapons, fuel, cargo, electronic equipment, sensors, take-off or landing gear. 7. The method of refueling an unmanned aircraft of claim 2, wherein said cargo bay maintains in flight operable doors. 8. The method of refueling an unmanned aircraft of claim 1, wherein said docking means is capable of configuring the aircraft to fly as a single aircraft. 9. The method of refueling an unmanned aircraft of claim 1, wherein said docking means is capable of launching said continuous flight aircraft. 10. The method of refueling an unmanned aircraft of claim 1, wherein the support aircraft is also unmanned. 11. A method of reloading an unmanned continuous flight aircraft, said unmanned aircraft comprising: an aircraft capable of multiple missions via continuous flight configured to dock to a support aircraft, both maintaining a payload bay on the bottom side of the aircraft; comprising the step of: maintaining said unmanned aircraft in an inverted flight pattern; docking both said aircraft in a configuration for reloading via a docking means; and exchanging cargo via both said payload bays. 12. The method of reloading an unmanned aircraft of claim 11, wherein said cargo bay of the continuous flight aircraft is located at the aircraft center of mass. 13. The method of reloading an unmanned aircraft of claim 12, wherein said cargo bay of the continuous flight aircraft is capable of dropping or exchanging weapons. 14. The method of reloading an unmanned aircraft of claim 12, wherein said cargo bay of the continuous flight aircraft is capable of dropping or exchanging cargo. 15. The method of reloading an unmanned aircraft of claim 14, wherein said cargo is in the form of a cartridge. 16. The method of reloading an unmanned aircraft of claim 15, wherein said cartridges comprise either one of the following: weapons, fuel, cargo, electronic equipment, sensors, take-off or landing gear. 17. The method of reloading an unmanned aircraft of claim 12, wherein said cargo bay maintains in flight operable doors. 18. The method of reloading an unmanned aircraft of claim 11, wherein said docking means is capable of configuring the aircraft to fly as a single aircraft. 19. The method of reloading an unmanned aircraft of claim 11, wherein said docking means is capable of launching said continuous flight aircraft. 20. The method of reloading an unmanned aircraft of claim 11, wherein the support aircraft is also unmanned.
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이 특허에 인용된 특허 (3)
Minovitch Michael A. (2832 St. George St. #6 Los Angeles CA 90027), Ammunition reloading system and operating method.
Pongratz, Hans Wolfgang; Hiebl, Manfred, Air-to-surface surveillance and/or weapons system and method for air-based inspection and/or engagement of objects on land or sea.
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