[특허]Boundary layer propulsion airship with related system and method

StratoComm Corporation

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Boundary layer propulsion airship with related system and method

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64B-001/30 B64B-001/24 B64C-021/00 B64C-021/10 B64C-011/00
미국특허분류(USC)	244/029; 244/030; 244/200; 244/200.1; 244/204; 244/204.1; 244/096; 244/055; 244/065
출원번호	US-0068667 (2008-02-08)
등록번호	US-8286909 (2012-10-16)
발명자 / 주소	Lee, Yee-Chun
출원인 / 주소	StratoComm Corporation
대리인 / 주소	Breneman & Georges
인용정보	피인용 횟수 : 10 인용 특허 : 18

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Systems, method, devices and apparatus are provided for reducing drag and increasing the flight efficiency characteristics of aircraft and airships including hybrid aircraft utilizing distributed boundary layer control and propulsion devices. Boundary layer control includes passive systems such as riblet films and boundary layer propulsion devices having a divided and distributed propulsion system disposed in the curved aft sections of aircraft and airships including hybrid aircraft susceptible to boundary layer drag due to degree of curvatures, speed and density of the surrounding air. Distributed propulsion devices include constructing propellers and riblets from shape memory alloys, piezoelectric materials and electroactive polymer (EAP) materials to change the shape and length of the distributed propulsion device.

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1. A boundary layer propelled airship comprising: (a) a curved airship skin having a fore section and a curved aft section; and(b) a distributed boundary layer propulsion means disposed in said curved aft section having at least one member of said distributed boundary layer propulsion means disposed inside a boundary layer separation area said distributed boundary layer propulsion means selected from the group consisting of: a plurality of micropropellers having a diameter less than the thickness of a boundary layer;a plurality of piezoelectric biomorph fins;a plurality of electroactive polymer propellers having a diameter less than the thickness of the boundary layer; anda plurality of electroactive polymer riblets. 2. The boundary layer propelled airship of claim 1 further comprising a passive riblet film disposed on said curved airship skin. 3. The boundary layer propelled airship of claim 1 further comprising a passive riblet film is disposed on said curved aft section of the airship skin. 4. The boundary layered propelled airship of claim 3 wherein said boundary layer propulsion means is disposed aft of said passive riblet film. 5. The boundary layer propelled airship of claim 3 wherein said boundary layer propulsion means is said plurality of electroactive polymer riblets disposed aft of said passive riblet film. 6. The boundary layer propelled airship of claim 5 wherein said boundary layer propulsion means further comprises said plurality of electroactive polymer propellers disposed aft of said plurality of electroactive polymer riblets. 7. The boundary layer propelled airship of claim 6 wherein said aft section terminates in a propeller. 8. The boundary layer propelled airship of claim 6 wherein said aft section terminates in a blunt end. 9. An airship having a boundary layer assisted propulsion system comprising: (a) an elongated airship having a skin with a frontal area and a rearward area;(b) a passive drag reducing film disposed on said skin between said frontal area and said rearward area;(c) a propulsion area having an electroactive polymer propulsion device disposed inside a boundary layer separation area on said skin between said passive drag reducing film and said rearward area; and(d) electrical contacts connecting said electroactive polymer to an electric propulsion system. 10. The airship of claim 9 further comprising an electroactive polymer controller connected to said electrical contacts through said skin. 11. The airship of claim 10 further comprising an electroactive polymer power supply and control circuit connected to said electrical contacts. 12. The airship of claim 9 wherein said electroactive polymer includes a plurality of electroactive polymer micropropellers. 13. The airship of claim 12 wherein said electrical contacts are composed of an elastomeric material containing graphite powder. 14. The airship of claim 9 further comprising an electroactive polymer pressure/stress sensing layer disposed on said skin. 15. The airship of claim 9 wherein said electroactive polymer is an electroactive polymer fin. 16. The airship of claim 9 wherein said electroactive polymer is an electroactive polymer riblet. 17. The airship of claim 9 wherein said electroactive polymer is a propeller. 18. The airship of claim 17 wherein said electroactive polymer includes a polymer pressure/stress sensing layer disposed on said propeller. 19. A high altitude dirigible having reduced drag comprising: (a) an elongated dirigible body having a curved skin with a fore section and an aft section;(b) a passive riblet film disposed between said fore section and said aft section of said curved skin;(c) an electroactive polymer propulsion device disposed inside a boundary layer between said passive riblet film and said aft section of said curved skin; and(d) a computer to control the operation of said electroactive polymer area. 20. The dirigible of claim 19 further comprising a layer of solar cells to provide electrical power for said electroactive polymer propulsion device. 21. The dirigible of claim 20 wherein said electroactive polymer device is the plurality of small propellers with a diameter of about 2 to 15 centimeters. 22. The dirigible of claim 20 wherein said electroactive polymer device is the plurality of piezoelectric biomorph fins. 23. The dirigible of claim 20 wherein said electroactive polymer device is the plurality of electroactive polymer propellers. 24. The dirigible of claim 20 wherein said electroactive polymer device is the plurality of electroactive riblets.

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Boundary layer propulsion airship with related system and method

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이 특허에 인용된 특허 (18)

이 특허를 인용한 특허 피인용횟수: 10

IPC 상위 출원인

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IPC 상세정보(version : 201201)

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