Vehicle comprising a bifunctional structural part
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B60L-011/18
H01M-004/46
H01M-002/10
B64C-001/12
B64C-039/02
H01G-011/22
H01G-011/66
H01G-011/04
H01M-012/04
H01G-011/08
H01G-011/82
B64C-001/00
출원번호
US-0344547
(2016-11-06)
등록번호
US-10046666
(2018-08-14)
발명자
/ 주소
Wei, Xibo
Li, Yuanyuan
Wei, Jingjing
출원인 / 주소
Ningbo Wise Digital Technology Co., Ltd
대리인 / 주소
Wang, Guosheng
인용정보
피인용 횟수 :
0인용 특허 :
7
초록▼
The present invention provides a vehicle comprising a power source such as a primary battery, a secondary battery, and a supercapacitor. The power source includes a plurality of components. At least one of the plurality of components serves as at least a portion of the structural part of the vehicle
The present invention provides a vehicle comprising a power source such as a primary battery, a secondary battery, and a supercapacitor. The power source includes a plurality of components. At least one of the plurality of components serves as at least a portion of the structural part of the vehicle. The power source is integrated with the structure of the vehicle, and improves the endurance of the vehicle.
대표청구항▼
1. A vehicle comprising a power source and a structural part, wherein the power source includes a plurality of components, and at least one of the plurality of components serves as at least a portion of the structural part, wherein the power source comprises a metal-air battery including a metal ano
1. A vehicle comprising a power source and a structural part, wherein the power source includes a plurality of components, and at least one of the plurality of components serves as at least a portion of the structural part, wherein the power source comprises a metal-air battery including a metal anode or an alloy anode, wherein said anode serves as said at least a portion of the structural part, and wherein the structural part is non-essential for the vehicle's mobility and is replaceable between trips of the vehicle,wherein said anode is oxidized or consumed during a trip of the vehicle,wherein said vehicle is selected from an aircraft, an unmanned aerial vehicle (UAV), a spacecraft, a watercraft including sub-surface watercraft, and a land vehicle e.g. an electrical car or truck, andwherein the non-essential part is selected from aircraft fuselage, aircraft skin, watercraft hull, car floor, car roof, car fender, car bumper, car decklid, car rocker, car door, vehicle window frame, vehicle door frame, main hatch, under the hatch before, quadrotor frame, camera mounting frame, landing bar, and landing gear. 2. The vehicle according to claim 1, wherein said power source further comprises a primary battery, a secondary battery, a film capacitor, or a supercapacitor. 3. The vehicle according to claim 2, wherein said at least one of the plurality of components in the power source comprises an electrode, an anode, a cathode, a current collector, a wire, a housing, a bipolar plate, a negative plate, a positive plate, or any combination thereof; and wherein the structural part is selected from aircraft wings, aircraft fuselages, aircraft skin, valve body, watercraft hull, connecting rod, car floor, car roof, car fender, car bumper, car decklid, car rocker, car door, vehicle window frame, vehicle door frame, pipe, rod, car chassis, wheel spacer, main hatch, under the hatch before, tail pipe, horizontal tail, vertical tail, quadrotor frame, camera mounting frame, landing bar, and landing gear. 4. The vehicle according to claim 3, wherein said at least one of the plurality of components is made of a metal, an alloy, a conductive polymer, a conductive composite material, a carbon fiber or graphite reinforced polymer (CFRP), graphene, carbon nanotube reinforced polymer (CNRP), or any combination thereof. 5. The vehicle according to claim 4, wherein the metal or the alloy comprises Aluminum, Iron, Lithium, Magnesium, Manganese, Copper, Zinc, Zirconium, Chromium, Titanium, Scandium, Silicon, Germanium, Calcium, Potassium, Sodium, Tin, or any combination thereof. 6. The vehicle according to claim 1, wherein the metal-air battery is aluminum-air (Al-air) battery. 7. The vehicle according to claim 1, wherein the metal-air battery includes an air cathode having a current collector, and said current collector serves as said at least a portion of the structural part. 8. The vehicle according to claim 2, wherein the secondary battery includes an electrode made of an aluminum alloy, and said electrode serves as said at least a portion of the structural part. 9. The vehicle according to claim 8, wherein said aluminum alloy comprises 0.1%˜0.5% (by weight) of scandium, and the electrode functions as the skin of an airplane. 10. The vehicle according to claim 8, wherein said aluminum alloy comprises zinc (7.3˜8.3% by weight), magnesium (2.2˜3.0% by weight), copper (1.6˜2.4% by weight), zirconium (0.05˜0.15% by weight), silicon, iron, manganese, chromium, and titanium, and the electrode functions as a valve body or connecting rod in the vehicle. 11. The vehicle according to claim 8, wherein said aluminum alloy comprises by weight 5.6˜6.1% zinc, 2.1˜2.5% magnesium, 1.2˜1.6% copper, and less than 0.5% of silicon, iron, manganese, titanium and chromium; and the electrode functions as the skin of an airplane. 12. The vehicle according to claim 8, wherein said aluminum alloy comprises lithium; and the electrode functions as the wings and fuselages of an aircraft. 13. The vehicle according, to claim 8, wherein said aluminum alloy comprises by weight 0.2˜0.6% silicon, 0˜0.35% iron, 0˜0.10% copper, 0˜0.10% manganese, 0.45˜0.9% magnesium, 0˜0.10% chromium, 0˜0.10% zinc, and 0˜0.10% titanium; and the electrode functions as window frame and door frame in a vehicle. 14. The vehicle according to claim 8, wherein said aluminum alloy comprises copper or lithium; and the electrode functions as the wings and fuselages of an aircraft. 15. The vehicle according to claim 8, wherein said aluminum alloy comprises by weight 0.4˜0.8% silicon, 0˜0.7% iron, 0.15˜0.4% copper, 0˜0.15% manganese, 0.8˜1.2% magnesium, 0.04˜0.35% chromium, 0˜0.25% zinc, and 0˜0.15% titanium; and the electrode functions as the wings and fuselages of an aircraft, or the wheel spacer of a land vehicle. 16. The vehicle according to claim 2, wherein said film capacitor includes electrodes made of a metal or alloy such as aluminum or zinc, and an insulating, plastic dielectric film 78 selected from polypropylene (PP), polyester, polyethylene terephthalate (PET), polyethylene naphthalate (PEN), polyphenylene sulfide (PPS), polytetrafluoroethylene (PTFE), polystyrene (PS), and polycarbonate (PC). 17. The vehicle according to claim 2, wherein said supercapacitor utilizes electrostatic double-layer capacitance, electrochemical pseudocapacitance, or a hybrid of the both. 18. The vehicle according to claim 17, wherein activated carbon electrodes are used for electrostatic double-layer capacitance, wherein transition metal oxide and conducting polymer electrodes are used for electrochemical pseudocapacitance, and wherein current collectors of said supercapacitor serve as said at least a portion of the structural part.
연구과제 타임라인
LOADING...
LOADING...
LOADING...
LOADING...
LOADING...
이 특허에 인용된 특허 (7)
Hibbs Bart D. ; Lissaman Peter B. S. ; Morgan Walter R. ; Radkey Robert L., Aircraft.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.