KR20210021327A - 풍력발전기능의 하이브리드식의 전기비행기 - Google Patents
풍력발전기능의 하이브리드식의 전기비행기 Download PDFInfo
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- KR20210021327A KR20210021327A KR1020210014344A KR20210014344A KR20210021327A KR 20210021327 A KR20210021327 A KR 20210021327A KR 1020210014344 A KR1020210014344 A KR 1020210014344A KR 20210014344 A KR20210014344 A KR 20210014344A KR 20210021327 A KR20210021327 A KR 20210021327A
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- 238000010248 power generation Methods 0.000 title claims abstract description 11
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000001257 hydrogen Substances 0.000 claims abstract description 19
- 229910052739 hydrogen Inorganic materials 0.000 claims abstract description 19
- 239000000446 fuel Substances 0.000 claims abstract description 12
- 230000005611 electricity Effects 0.000 claims description 10
- 238000013473 artificial intelligence Methods 0.000 claims description 9
- 239000007789 gas Substances 0.000 claims description 7
- 238000006243 chemical reaction Methods 0.000 claims description 2
- 238000005259 measurement Methods 0.000 claims description 2
- 150000002431 hydrogen Chemical class 0.000 claims 2
- 239000011248 coating agent Substances 0.000 claims 1
- 238000000576 coating method Methods 0.000 claims 1
- 210000001061 forehead Anatomy 0.000 claims 1
- 230000002265 prevention Effects 0.000 abstract 1
- 241000282373 Panthera pardus Species 0.000 description 1
- 241000282376 Panthera tigris Species 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
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Abstract
본 발명의 풍력발전기능의 비행기는 풍력발전기와 태양광발전기 수소가스 열병합발전기가 설치되어 있고 동력으로는 수소연료로 작동되는 수소엔진과 가솔린엔진의 하이브리드 방식의 엔진과 전기모타의 2개의 방식이며 화재시 인공지능마이컴장치기가 작동되어 자동으로 스스로 작동되는 소화기기능과 비행기 추락시 추락방지용 구난장치인 비행기 낙하산 개폐장치가 작동되여 3개의 낙하산이 펼쳐져서 비행기자체를 안전하게 땅에 낙하시켜 주는 사고방지용비행기이다.
Description
본 발명 풍력발전기능의 비행기는 모든 비행기 종류의 전체 기체표면에 태양광패널을 형성시켜서 태양광발전을 하는 태양광 발전기 기능을 부여시키고 휘발유로 작동되는 엔진과 더불어서 전기로 작동되는 전기모타를 형성하여 하이브리드식으로 된 휘발유와 수소연료로 가는 수소가스 열병합발전기와 전기겸용의 전기모터식의 전기비행기이다
.
본 발명의 풍력발전기능의 전기비행기는 비행기 기체 전체의 모든 부분에 태양광패널을 설치해서 형성시키고 앞날개 전면부 일측에 작은 풍력기를 복수로 설치 형성하여 착륙시나 운행시 바람의 힘으로 돌아가는 풍력발전기를 통해서 그기서 발생된 전기에너지를 2차전지에 충전시켜 전기모터를 작동시켜 사용하는 전기비행기이다 그리고 휘발유로 된 가솔린엔진과 수소연료로 가는 수소엔진과 수소열병합발전기로 형성된 하이브리드식 비행기이다.
본 발명의 풍력발전기능의 하이브리드 전기비행기는 비행기 전체부분의 기체에 태양광패널을 형성시키고 패널에서 발생된 전기에너지를 2차전지에 충전시켜 전기모타를 구동시키고 앞날개 전면부 일측에 풍력발전기를 형성시켜 발생된 풍력의 변환된 전기에너지를 2차전지에 충전시켜 전기모터를 작동시킨다 그리고 하이브리드식 수소엔진과 가솔린엔진이 형성된다. 수소열병합발전기와 그 전기로 작동되는 전기모터를 형성시킨다
본 발명의 풍력발전기능의 비행기는 일반비행기의 운행시 발생되는 비행기 휘발유가 엄청난 연료비와 함께 지구를 오염시키는 폐단이 많고 친환경의 반대되므로 지구 환경에 막대한 손실을 끼치지만 본 발명의 비행기는 연료가 작게 들고 친환경수소연료로 작동되고 가는 수소엔진과 더불어 전기모타까지 작동되고 수소가스로 작동되는 열병합발전기가 형성된 하이브리드라는 좋은 기능이 업그레이드된 관계로 지구친화적인비행기이며 그기다가 "금상첨화"인 기체 전체표면이 태양광패널로 되어 있어 마치 "호랑이나 표범처럼" 몸에 나있는 전체무늬처럼 태양광 패널이 기체표면에 수놓아 있듯이 형성된 관계로 비행기가 착륙중이거나 운행, 주행중에도 계속해서 햇빛을 받아 계속적으로 24시간 고마운 전기발생을 해서 2차전지에 충전해서 전기힘으로도 미국까지 날아갈 수도 있기 때문에 큰 연료비가 들지 않고 공짜로도 날아갈 수도 있는 지구친환경의 엔진과 전기모타로 2개의 동력 발생되는 겸용 하이브리드식의 비행기이다 그리고 전기량이 일정수준 미달시는 가솔린엔진과 수소동력엔진이 인공지능마이컴장치기에 의해서 자동구동, 작동되고 수소가스 열병합발전기도 작동되는 하이브리드 기능이 설치 형성되어 있다
도1은 본 발명 비행기의 사시도이며 대표도이고 도2는 본 발명 비행기의 낙하산 작동예시도이다
본 발명의 하이브리드식 풍력발전기능의 전기비행기(1)는 기체(2)의 전체표면(3)의 일측에 태양광패널(4)을 코팅형성시키고 패널(4)에서 그기서 발생된 전기를 전기충전2차전지(5)에 충전하여 전기모터(6)를 구동시킨다 그리고 기체(2)의 앞날개(7) 일측에 풍력발전기(8, 9, 10, 11)를 형성하고 2차전지(5)의 전기량이 일정수준이하가 될 때 인공지능마이컴장치기(12) 측정센스(16)가 작동되어 즉시로 하이브리드기능(13)이 작동되어 휘발유로 작동되는 엔진(14)과 수소연료로 작동되는 엔진(14')과 수소가스 열병합발전기(14")로 작동되고 수소가스통(14"')과 인공지능마이컴기(14"")가 작동되는 기능으로 자동변환 장치기(15)가 기체내 일측에 형성된다
그리고 비상사태시 인공지능컴장치기(12)가 인지하여 소화기(17) 작동센스(18)를 작동시키고 비행기(1) 앞머리와 중간부분과 꼬리날개 일측에 있는 낙화산스프링(21)을 작동시켜 낙화산장치기(19, 19', 19")의 문(22)을 여는 낙화산개폐장치기(19, 19', 19")를 작동시켜 대형으로 된 3개의 낙하산을 튀어나오게 하여 추락하는 비행기로부터 안전하게 비행기를 땅에 안착시켜 준다.
본 발명의 하이브리드식 풍력발전기능의 전기비행기(1)는 기체(2)의 전체표면(3)의 일측에 태양광패널(4)을 코팅형성시키고 패널(4)에서 그기서 발생된 전기를 전기충전2차전지(5)에 충전하여 전기모터(6)를 구동시킨다 그리고 기체(2)의 앞날개(7) 일측에 풍력발전기(8, 9, 10, 11)를 형성하고 2차전지(5)의 전기량이 일정수준이하가 될 때 인공지능마이컴장치기(12) 측정센스(16)가 작동되어 즉시로 하이브리드기능(13)이 작동되어 휘발유로 작동되는 엔진(14)과 수소연료로 작동되는 엔진(14')과 수소가스 열병합발전기(14")로 작동되고 수소가스통(14"')과 인공지능마이컴기(14"")가 작동되는 기능으로 자동변환 장치기(15)가 기체내 일측에 형성된다
그리고 비상사태시 인공지능컴장치기(12)가 인지하여 소화기(17) 작동센스(18)를 작동시키고 비행기(1) 앞머리와 중간부분과 꼬리날개 일측에 있는 낙화산스프링(21)을 작동시켜 낙화산장치기(19, 19', 19")의 문(22)을 여는 낙화산개폐장치기(19, 19', 19")를 작동시켜 대형으로 된 3개의 낙하산을 튀어나오게 하여 추락하는 비행기로부터 안전하게 비행기를 땅에 안착시켜 준다.
본 발명의 풍력발전기능의 비행기는 가솔린엔진과 수소엔진과 전기모타로 구동되는 하이브리드 방식이므로 인공지능마이컴장치를 형성하여 전기잔량이 수준이하로 미달될 때는 인공지능마이컴칩장치기가 작동되어 즉시로 명령하달되어 가솔린과 수소 열병합발전기와 엔진작동이 시작된다. 그리고 사고발생시 비상시도 즉시로 인공지능마이컴장치기가 명령을 내려 기체외부와 내부에 설치된 화재진압하는 소화기작동과 비행기앞머리와 중간등부분과 꼬리날개부분의 낙하산이 튀어나와 펼쳐져 비행기를 안전하게 낙하시킨다 이렇게 하는 것은 인공지능감지센스가 전기적인 신호로 명령을 비행기 낙하산 개폐장치에 신호명령을 내려서 실시실행시킨다.
Claims (1)
- 본 발명의 풍력발전기능의 하이브리드식의 전기비행기(1)는 기체(2)의 전체표면(3)의 일측에 태양광패널(4)을 코팅시켜 형성시키고 패널(4)에서 발생된 전기를 2차전지(5)에 충전하여 구동하는 전기모터(6)를 기체(2) 내부일측에 형성하는 단계와 기체(2) 앞날개(7) 일측에 풍력발전기(8, 9, 10, 11)를 설치 형성하는 단계와 2차전지(5)의 전기량이 일정이하의 수준이 될 때 비행기의 모든 기능을 제어하는 인공지능마이컴장치(12)의 측정센스(12')가 작동되어 즉시로 하이브리드기능(13)이 작동되어 전기모타(6)에서 변환되어 가솔린엔진(14')과 수소연료엔진(14)동력으로 바뀌게 해주는 자동변환장치기(15)를 기체내부일측에 설치형성시키는 단계와 하이브리드시스템으로 작동되는 엔진(14)의 연료로는 휘발유(14')탱크(14")와 수소(14"')탱크(14"")가 기체(2) 일측에 설치형성되는 단계와 수소(14"') 연료로 발전되는 수소가스 열병합발전기(14')와 수소연료(14"')를 직접 연소시켜 작동되는 엔진(14')을 휘발유(14')용 엔진과 같이 비행기(1) 내부기체(2) 일측에 형성하는 단계와를 기체(2) 내부 일측에 형성시키는 단계와 수소가스 열병합발전기(14')가 기체(2)내부 일측에 형성되어 있는 단계와 비상시 소화기센스(18)를 작동시키고 비행기(2)의 앞머리와 중간부분과 꼬리날개부분에 있는 안전 낙화산개폐센스(19"')장치기(19, 19', 19")를 비행기 일측에 형성시키는 단계와 휘발유와 수소를 연료로 하는 수소충전엔진과 태양광과 풍력과 수소에너지로 구동되는 엔진과 수소가스 열병합발전기로 작동되는 전기모터의 4개의 하이브리드 동력으로 작동되는 풍력발전기능의 하이브리드식의 전기비행기
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CN114109726B (zh) * | 2021-11-24 | 2024-04-30 | 重庆交通大学绿色航空技术研究院 | 利用太阳能与风能发电的飞行装置、发电系统及发电方法 |
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