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KR20110087661A - Green Energy Hybrid Helicopter - Google Patents

Green Energy Hybrid Helicopter
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Publication number
KR20110087661A
KR20110087661AKR1020100007181AKR20100007181AKR20110087661AKR 20110087661 AKR20110087661 AKR 20110087661AKR 1020100007181 AKR1020100007181 AKR 1020100007181AKR 20100007181 AKR20100007181 AKR 20100007181AKR 20110087661 AKR20110087661 AKR 20110087661A
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KR
South Korea
Prior art keywords
energy
helicopter
present
propeller
lot
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Ceased
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KR1020100007181A
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Korean (ko)
Inventor
박경섭
정재원
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박경섭
정재원
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Publication date
Application filed by 박경섭, 정재원filedCritical박경섭
Priority to KR1020100007181ApriorityCriticalpatent/KR20110087661A/en
Publication of KR20110087661ApublicationCriticalpatent/KR20110087661A/en
Ceasedlegal-statusCriticalCurrent

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Abstract

Translated fromKorean

(가) 기술분야
본 발명은 헬리콥터 프로펠러의 회전 에너지를 전기에너지로 변환하기 위하여 고안된 발명이다.
전기에너지는 충전지로 충전되어 다시 헬리콥터의 프로펠러를 회전시키다.
그린에너지 기술의 한 분야로 보면 된다.
이것은 에너지 효율을 높인 하이브리드의 한 방법이다.
(나) 해결하고자 하는 과제
본 발명은 기존 헬리콥터가 날아다니는데 많은 연료 에너지를 소비하는 것을 해결하려고 한다.
(다) 과제의 해결 수단
기존의 헬리콥터는 많은 에너지로 짧은 시간 떠있었다.
이것은 많은 에너지 소비를 발생시켰다.
기존의 헬리콥터의 에너지의 과소비를 막는 본 발명은 하이브리드 헬리콥터의 회전 운동에너지를 이용하여 충전지를 충전시킨다.
따라서 적은 에너지로 많은 체공시간을 가질 수 있다.
(라) 효과
본 발명은 회전 운동에너지를 모터를 이용하여 전기에너지로 전환 시켜서 기존 헬리콥터보다 에너지 효율을 높이는 효과가 있다.
이것은 그린에너지 기술분야 중에 하나인 하이브리드 방식을 사용한 것이다.
(A) Technical field
The present invention is an invention designed to convert the rotational energy of the helicopter propeller into electrical energy.
The electrical energy is charged with a rechargeable battery, which in turn rotates the helicopter's propeller.
It's a field of green energy technology.
This is a hybrid method of energy efficiency.
(B) Challenges to be solved
The present invention seeks to address the consumption of a lot of fuel energy for existing helicopters to fly.
(C) Solution to the problem
Conventional helicopters were floating for a short time with a lot of energy.
This caused a lot of energy consumption.
The present invention, which prevents excessive consumption of energy of a conventional helicopter, charges a rechargeable battery using rotational kinetic energy of a hybrid helicopter.
Therefore, you can have more flight time with less energy.
(D) effect
The present invention has the effect of increasing the energy efficiency than the existing helicopter by converting the rotational kinetic energy into electrical energy using a motor.
This is a hybrid approach, one of the green energy technologies.

Description

Translated fromKorean
그린에너지 하이브리드 헬리콥터{Green Energy hybrid helicopter}Green Energy Hybrid Helicopter

본 발명은 헬리콥터 프로펠러의 회전 에너지를 전기에너지로 변환하기 위하여 고안된 발명이다.The present invention is an invention designed to convert the rotational energy of the helicopter propeller into electrical energy.

전기에너지는 충전지로 충전되어 다시 헬리콥터의 프로펠러를 회전한다.The electrical energy is charged with a rechargeable battery, which in turn rotates the helicopter's propeller.

하이브리드 자동차Hybrid car

IPC 코드B60K 6/02IPC Code B60K 6/02

출원번호1019990004610 (1999.02.10)Application number1019990004610 (1999.02.10)

공개번호1020000055787 (2000.09.15)Publication No. 1020000055787 (2000.09.15)

출원인현대자동차 주식회사Applicant Hyundai Motor Company

발명자/고안자이충섭Inventor / Designer

대리인송만호 | 오원석Representative Song Man-ho | Oh Won Seok

(검색일 2010. 1. 27.)(Date of search January 27, 2010)

기존에 사용중이던 하이브리드 자동차의 전기에너지 충전 방식을 약간 변형 시켜서 헬리콥터에 적용하여 사용Slightly modify the electric energy charging method of the existing hybrid car and apply it to the helicopter

본 발명은 기존 헬리콥터가 날아다니는데 많은 연료 에너지를 소비하는 것을 해결하려고 한다.The present invention seeks to address the consumption of a lot of fuel energy for existing helicopters to fly.

기존의 헬리콥터는 많은 에너지로 짧은 시간 떠있었다.Conventional helicopters were floating for a short time with a lot of energy.

이것은 많은 에너지 소비를 발생시켰다.This caused a lot of energy consumption.

기존의 헬리콥터의 에너지의 과소비를 막는 본 발명은 하이브리드 헬리콥터의 회전 운동에너지를 이용하여 충전지를 충전시킨다.The present invention, which prevents excessive consumption of energy of the conventional helicopter, charges the rechargeable battery using the rotational kinetic energy of the hybrid helicopter.

따라서 적은 에너지로 많은 체공시간을 가질 수 있다.
Therefore, you can have more flight time with less energy.

본 발명은 회전 운동에너지를 모터를 이용하여 전기에너지로 전환 시켜서 기존 헬리콥터보다 에너지 효율을 높이는 효과가 있다.The present invention has the effect of increasing the energy efficiency than the existing helicopter by converting the rotational kinetic energy into electrical energy using a motor.

이것은 그린에너지 기술분야 중에 하나인 하이브리드 방식을 사용한 것이다.
This is a hybrid approach, one of the green energy technologies.

[도면1]은 부품 전체를 조립한 3차원 입체도[Figure 1] is a three-dimensional three-dimensional view of the entire assembly

본 발명은 연료를 이용한 프로펠러 구동모터(②)가 회전해서 프로펠러의 회전축 ③을 돌리고 프로펠러 회전축(③)는 프로펠러(①)을 돌려서 회전 운동을 한다.In the present invention, the propeller drive motor (②) using fuel rotates to rotate thepropeller rotating shaft ③ and thepropeller rotating shaft ③ rotates the propeller (①) to perform a rotary motion.

프로펠러(①)의 회전 운동에너지를 회전축(③)을 통하여 전기 모터(④)를 회전 시킨다.Rotate the kinetic energy of the propeller (①) to rotate the electric motor (④) through the rotating shaft (③).

전기 모터(④)에서 회전 운동에너지는 전기에너지로 전환되어 충전지에 전기에너지가 저장된다.In theelectric motor ④, the rotational kinetic energy is converted into electrical energy and stored in the rechargeable battery.

① 헬리콥터의 운행을 담당하며 회전 운동을 하는 프로펠러
② 연료를 이용하여 회전 운동에너지를 발생시키는 모터이다.
전기로 프로펠러를 동작시에는 클러치가 떨어져서 모터에 직접적인 영향을 끼치지 않는다.
③ 프로펠러의 회전 운동에너지를 전기에너지로 전환 시키며 연료에너지를 사용하지 않을 때는 전기에너지로 프로펠러를 회전시킨다.
④ 전기 모터와 연료 모터의 회전에너지를 프로펠러의 회전 운동에너지로 전달하는 회전축이다.
① Propeller that rotates and handles helicopter operation
② It is a motor that generates rotational kinetic energy using fuel.
When operating the electric propeller, the clutch drops and does not directly affect the motor.
③ It converts the rotational kinetic energy of propeller into electric energy and rotates the propeller with electric energy when fuel energy is not used.
④ It is a rotating shaft that transmits rotational energy of electric motor and fuel motor as rotational kinetic energy of propeller.

Claims (1)

Translated fromKorean
프로펠러의 회전 운동에너지를 전기에너지로 전환하여 에너지 효율을 높인 특징을 가진 하이브리드 헬리콥터.Hybrid helicopter with energy efficiency by converting rotational kinetic energy of propeller into electric energy.
KR1020100007181A2010-01-272010-01-27 Green Energy Hybrid HelicopterCeasedKR20110087661A (en)

Priority Applications (1)

Application NumberPriority DateFiling DateTitle
KR1020100007181AKR20110087661A (en)2010-01-272010-01-27 Green Energy Hybrid Helicopter

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
KR1020100007181AKR20110087661A (en)2010-01-272010-01-27 Green Energy Hybrid Helicopter

Publications (1)

Publication NumberPublication Date
KR20110087661Atrue KR20110087661A (en)2011-08-03

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Family Applications (1)

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KR1020100007181ACeasedKR20110087661A (en)2010-01-272010-01-27 Green Energy Hybrid Helicopter

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KR (1)KR20110087661A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB2489311A (en)*2011-03-212012-09-26Tecniq S LtdCharging unit for hybrid electrically powered aircraft
US11486472B2 (en)2020-04-162022-11-01United Technologies Advanced Projects Inc.Gear sytems with variable speed drive
US11535392B2 (en)2019-03-182022-12-27Pratt & Whitney Canada Corp.Architectures for hybrid-electric propulsion
US11628942B2 (en)2019-03-012023-04-18Pratt & Whitney Canada Corp.Torque ripple control for an aircraft power train
US11697505B2 (en)2019-03-012023-07-11Pratt & Whitney Canada Corp.Distributed propulsion configurations for aircraft having mixed drive systems
US11732639B2 (en)2019-03-012023-08-22Pratt & Whitney Canada Corp.Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
US11738874B2 (en)2019-03-012023-08-29Hamilton Sundstrand CorporationAircraft having hybrid-electric propulsion system with electric storage located in fuselage
US11855301B2 (en)2019-09-302023-12-26Hamilton Sundstrand CorporationSystems and methods for battery ventilation
US12240619B2 (en)2019-03-012025-03-04Pratt & Whitney Canada Corp.Torque balancing for hybrid electric propulsion systems and aircraft utilizing hybrid electric propulsion systems

Cited By (11)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB2489311A (en)*2011-03-212012-09-26Tecniq S LtdCharging unit for hybrid electrically powered aircraft
US11628942B2 (en)2019-03-012023-04-18Pratt & Whitney Canada Corp.Torque ripple control for an aircraft power train
US11697505B2 (en)2019-03-012023-07-11Pratt & Whitney Canada Corp.Distributed propulsion configurations for aircraft having mixed drive systems
US11732639B2 (en)2019-03-012023-08-22Pratt & Whitney Canada Corp.Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
US11738874B2 (en)2019-03-012023-08-29Hamilton Sundstrand CorporationAircraft having hybrid-electric propulsion system with electric storage located in fuselage
US12240619B2 (en)2019-03-012025-03-04Pratt & Whitney Canada Corp.Torque balancing for hybrid electric propulsion systems and aircraft utilizing hybrid electric propulsion systems
US11535392B2 (en)2019-03-182022-12-27Pratt & Whitney Canada Corp.Architectures for hybrid-electric propulsion
US12071256B2 (en)2019-03-182024-08-27Pratt & Whitney Canada Corp.Architectures for hybrid-electric propulsion
US11855301B2 (en)2019-09-302023-12-26Hamilton Sundstrand CorporationSystems and methods for battery ventilation
US11486472B2 (en)2020-04-162022-11-01United Technologies Advanced Projects Inc.Gear sytems with variable speed drive
US12066083B2 (en)2020-04-162024-08-20Pratt & Whitney Canada Corp.Gear systems with variable speed drive

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