A morphing aircraft that is achieves multi-modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage Th
A morphing aircraft that is achieves multi-modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.
대표청구항▼
1. A morphing rotary-wing unmanned aerial vehicle that transforms from a beverage container to an aircraft, comprising: a substantially cylindrical fuselage comprising a shape configured, dimensioned, and sized as a hand-held beverage container with a first end and a second end, the beverage contain
1. A morphing rotary-wing unmanned aerial vehicle that transforms from a beverage container to an aircraft, comprising: a substantially cylindrical fuselage comprising a shape configured, dimensioned, and sized as a hand-held beverage container with a first end and a second end, the beverage container with an outer surface containing color, trade dress, and lettering substantially identical to a given consumer brand of a beverage, thereby appearing substantially identical to the beverage container when not in flight;at least one rotor coupled to the first end, the at least one rotor comprising a first position where the at least one rotor is extended outwards using at least one mechanical drive mechanism from the fuselage and a second position where the at least one rotor is retracted inwards using the mechanical drive mechanism towards the fuselage, wherein in the second position, the rotor is completely inside the beverage container, thereby appearing only as the beverage container; andat least one of an electric-power engine, a gas-powered engine, and a jet-powered engine mechanically coupled to the at least one rotor, wherein the engine is enclosed within the fuselage and rotates the at least one rotor relative to the cylindrical fuselage in order to provide lift and propulsion. 2. The rotary-wing unmanned aerial vehicle of claim 1, wherein the at least one rotor is retracted inwards into an inner portion of the fuselage. 3. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage is formed from the beverage container. 4. The rotary-wing unmanned aerial vehicle of claim 1, wherein the at least one rotor comprises plurality of members, wherein at least one of the plurality of members is pivotably coupled to at least one other of the plurality of members. 5. The rotary-wing unmanned aerial vehicle of claim 1, wherein the beverage container is a soft drink container. 6. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises external trade dress and lettering substantially similar to a given consumer brand of beverage. 7. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a camera coupled thereto. 8. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a microphone coupled thereto. 9. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a chemical sensor coupled thereto. 10. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a biological sensor coupled thereto. 11. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a heat sensor coupled thereto. 12. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises an explosive device coupled thereto. 13. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a positioning device coupled thereto. 14. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises at least one flare coupled thereto. 15. The rotary-wing unmanned aerial vehicle of claim 1, wherein the fuselage comprises a smoke generator coupled thereto. 16. The rotary-wing unmanned aerial vehicle of claim 1, wherein the at least one rotor is made of resilient material so as to be bendable in order to fit inside the fuselage. 17. A morphing rotary-wing unmanned aerial vehicle that transforms from a consumer packaging container to an aircraft, comprising: a fuselage comprising a shape configured and sized as a consumer packaging container with a first end and a second end, the consumer packaging container with an outer surface containing color, trade dress and lettering substantially identical to a given consumer brand of a food packaging;at least one rotor coupled to the first end, the at least one rotor comprising a first position where the at least one rotor is extended outwards using at least one mechanical drive mechanism from the fuselage and a second position where the at least one rotor is retracted inwards using the mechanical drive mechanism towards the fuselage, wherein in the second position, the rotor is completely inside the consumer packaging container, thereby appearing only as the consumer packaging container; andat least one of an electric-power engine, a gas-powered engine, and a jet-powered engine mechanically coupled to the at least one rotor, wherein the engine is enclosed within the fuselage and rotates the at least one rotor relative to the fuselage in order to provide lift and propulsion. 18. The rotary-wing unmanned aerial vehicle of claim 17, wherein the at least one rotor is retracted inwards into an inner portion of the fuselage. 19. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage is formed from the consumer packaging container. 20. The rotary-wing unmanned aerial vehicle of claim 17, wherein the consumer packaging container is a soft drink container. 21. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises external trade dress and lettering substantially similar to a given consumer brand of beverage. 22. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises a camera coupled thereto. 23. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises a microphone coupled thereto. 24. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises a chemical sensor coupled thereto. 25. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises at least one of a biological sensor and a heat sensor coupled thereto. 26. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises a positioning device coupled thereto. 27. The rotary-wing unmanned aerial vehicle of claim 17, wherein the fuselage comprises at least one of an explosive device, a flare, and a smoke generator coupled thereto. 28. The rotary-wing unmanned aerial vehicle of claim 17, wherein the at least one rotor is made of resilient material so as to be bendable in order to fit inside the fuselage.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (3)
Eickmann Karl (2420 Isshiki Hayama-machi ; Kanagawa-ken JPX), Aircraft with a retractable variable pitch propeller or a fluid motor driven multi propeller aircraft.
Neal, III, David Anthony; Ehlmann, Kevin Marlan; Gressick, William Thomas; Bateman, Alec Jacob Devine; Horneman, Kenneth Richard, Systems, devices, and/or methods for managing targeted payload descent.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.