KR20220093292A - Drone helicopter - Google Patents

Drone helicopter Download PDF

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Publication number
KR20220093292A
KR20220093292A KR1020200184059A KR20200184059A KR20220093292A KR 20220093292 A KR20220093292 A KR 20220093292A KR 1020200184059 A KR1020200184059 A KR 1020200184059A KR 20200184059 A KR20200184059 A KR 20200184059A KR 20220093292 A KR20220093292 A KR 20220093292A
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KR
South Korea
Prior art keywords
battery
present
balance
drone
flying
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Application number
KR1020200184059A
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Korean (ko)
Inventor
박성호
Original Assignee
박성호
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Priority to KR1020200184059A priority Critical patent/KR20220093292A/en
Publication of KR20220093292A publication Critical patent/KR20220093292A/en

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/08—Helicopters with two or more rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B64C2201/024—
    • B64C2201/042—
    • B64C2201/108—
    • B64C2201/165—
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Remote Sensing (AREA)
  • Toys (AREA)

Abstract

The present invention relates to a drone helicopter intended to solve the problems of unstable balance and small battery capacity, which can only be used for 30 minutes, by allowing energy to be stored by the battery. In other words, the drone helicopter of the present invention, a manned drone, is composed of batteries divided into two for the center of gravity to store energy, and four propellers arranged in a diamond shape to adjust the balance while flying in the sky. Therefore, the present invention has the effect of solving the existing problems of unstable balance and small battery capacity that can be used for only 30 minutes by allowing energy to be stored in the battery.

Description

드론헬기 {Drone helicopter}Drone helicopter}

본 발명은 드론헬기에 관한 것으로서,The present invention relates to a drone helicopter,

더욱 상세하게는 드론헬기에 있어서,More specifically, in the drone helicopter,

에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 배터리, 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 프로펠러으로 구성 하여서,The battery is divided into two for the center of gravity to store energy, and the battery is located at the front and the back, and it is composed of a propeller with four propellers arranged in a diamond shape to control the balance while flying in the sky.

배터리에 의하여 에너지를 저장할 수 있게 함으로써 균형이 불안정하고 배터리가 작아 30분 밖에 사용할 수 없는 문제점을 해소하도록 함을 목적으로 한 것이다.By enabling the battery to store energy, the purpose is to solve the problem that the balance is unstable and the battery is small and can only be used for 30 minutes.

일반적으로유인드론는 이동 교통수단으로 사용하는 것이다.In general, manned drones are used as a means of transportation.

상기한 바와 같이 유인드론는 배터리, 모터, 프로펠러, 의자, 안전장치로 구성된 것이다.As described above, the manned drone is composed of a battery, a motor, a propeller, a chair, and a safety device.

이상과 같은 유인드론는 프로펠러가 움직여 하늘을 날아서 이동하는 것이다.The manned drones as described above fly in the sky by moving the propellers.

그러나 상기한 바와 같은 종래의 유인드론는 균형이 불안정하고 배터리가 작아 30분 밖에 사용할 수 없는 문제점이 있었다.However, the conventional manned drone as described above has a problem in that the balance is unstable and the battery is small, so that it can be used only for 30 minutes.

대한민국 특허 공개 제 1020190018514호Korean Patent Publication No. 1020190018514

이에 본 발명은 종래의 유인드론가 균형이 불안정하고 배터리가 작아 30분 밖에 사용할 수 없는 문제점을 해결하기 위한 것이다.Accordingly, the present invention is to solve the problem that the balance of the conventional manned drone is unstable and the battery is small and can only be used for 30 minutes.

즉, 본 발명은 에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 배터리, 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 프로펠러으로 구성한 것이다.That is, the present invention consists of a battery divided into two for the center of gravity so as to store energy and located in the front and rear, and a propeller in which four propellers are arranged in a rhombus shape so that the balance can be adjusted while flying in the sky.

따라서, 본 발명은 에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 배터리, 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 프로펠러으로 구성 함으로써, 배터리에 의하여 에너지를 저장할 수 있게 함으로써 균형이 불안정하고 배터리가 작아 30분 밖에 사용할 수 없는 문제점을 해소하도록 한 효과를 갖는 것이다.Therefore, the present invention is divided into two for the center of gravity so as to store energy, and the battery is located at the front and rear, and the propeller with four propellers arranged in a rhombus shape so that the balance can be adjusted while flying in the sky. By allowing it to be stored, it has the effect of solving the problem that the balance is unstable and the battery is small and can only be used for 30 minutes.

도 1 : 본 발명의 고안도Figure 1: Design of the present invention

즉, 본 발명은 에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 (101)배터리, 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 (102)프로펠러으로 구성 된 것이다.That is, the present invention consists of a (101) battery located at the front and back, divided into two for the center of gravity to store energy, and a (102) propeller with four propellers arranged in a rhombus shape to control the balance while flying in the sky. will be.

여기서, (101)배터리는 에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 것이다.Here, the (101) battery is divided into two for the center of gravity to store energy, and is located at the front and back.

여기서, (102)프로펠러는하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 것이다.Here, the (102) propeller is arranged in a rhombus shape so that the balance can be adjusted while flying in the sky.

이하, 본 발명의 사용과정에 대하여 설명하면 다음과 같다.Hereinafter, the process of using the present invention will be described as follows.

상기한 바와 같이 본 발명은 유인드론에 있어서에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 (101)배터리, 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 (102)프로펠러으로 구성된 본 발명을 적용하여 실시하게 되면, 균형이 불안정하고 배터리가 작아 30분 밖에 사용할 수 없는 문제점을 해소하도록 한 것이다.As described above, the present invention is a (101) battery located at the front and back, divided into two for the center of gravity to store energy in the manned drone, and four propellers arranged in a rhombus shape to control the balance while flying in the sky ( 102) When the present invention composed of a propeller is applied and implemented, it is intended to solve the problem that the balance is unstable and the battery is small and can only be used for 30 minutes.

또한 본 발명의 실시에 있어, 무게중심을 위해 2개로 나누어 앞뒤에 위치한 (101)배터리로 구성한 본 발명을 적용하여 실시하게 되면, 에너지를 저장할 수 있게 될 것이다.In addition, in the practice of the present invention, if the present invention is implemented by applying the present invention composed of (101) batteries located in the front and rear divided into two for the center of gravity, energy can be stored.

또한 본 발명의 실시에 있어, 4개의 프로펠러를 마름모 모양으로 배치한 (102)프로펠러로 구성한 본 발명을 적용하여 실시하게 되면, 하늘을 날면서 균형조절을 할 수 있게 될 것이다.In addition, in the practice of the present invention, if the present invention consisting of (102) propellers arranged in a rhombus shape is applied and implemented by applying the present invention, it will be possible to adjust the balance while flying in the sky.

101 : 배터리, 102 : 프로펠러101: battery, 102: propeller

Claims (3)

드론헬기에 있어서,
에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치한 (101)배터리, 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치한 (102)프로펠러.In a drone helicopter,
A (101) battery located at the front and back divided into two for the center of gravity to store energy, and a (102) propeller with four propellers arranged in a diamond shape to control the balance while flying. 제 1항에 있어서,
(101)배터리를 통하여 에너지를 저장할 수 있게 무게중심을 위해 2개로 나누어 앞뒤에 위치함을 특징으로 하는 배터리.The method of claim 1,
(101) A battery, characterized in that it is divided into two for the center of gravity so that energy can be stored through the battery and located at the front and back. 제 1항에 있어서,
(102)프로펠러를 통하여 하늘을 날면서 균형조절을 할 수 있게 4개의 프로펠러를 마름모 모양으로 배치함을 특징으로 하는 프로펠러.The method of claim 1,
(102) A propeller, characterized in that by arranging four propellers in a rhombus shape so that the balance can be adjusted while flying through the propeller.
KR1020200184059A 2020-12-27 2020-12-27 Drone helicopter KR20220093292A (en)

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Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20190018514A (en) 2016-07-08 2019-02-22 탈레스 유에스에이, 인크. Triggering the identification signal broadcast of the first navigation auxiliary equipment

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20190018514A (en) 2016-07-08 2019-02-22 탈레스 유에스에이, 인크. Triggering the identification signal broadcast of the first navigation auxiliary equipment

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