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KR20180096455A - Triangle jet airplane - Google Patents

Triangle jet airplane Download PDF

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Publication number
KR20180096455A
KR20180096455A KR1020170023782A KR20170023782A KR20180096455A KR 20180096455 A KR20180096455 A KR 20180096455A KR 1020170023782 A KR1020170023782 A KR 1020170023782A KR 20170023782 A KR20170023782 A KR 20170023782A KR 20180096455 A KR20180096455 A KR 20180096455A
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KR
South Korea
Prior art keywords
jet engine
jet
flying
landing
present
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
KR1020170023782A
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Korean (ko)
Inventor
조효석
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조효석
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Priority to KR1020170023782A priority Critical patent/KR20180096455A/en
Publication of KR20180096455A publication Critical patent/KR20180096455A/en
Withdrawn legal-status Critical Current

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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
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/02—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded
    • B64C29/04—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded characterised by jet-reaction propulsion
    • 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • 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
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/296—Rotors with variable spatial positions relative to the UAV body
    • B64U30/297—Tilting rotors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
    • B64C2201/02—
    • B64C2201/048—
    • B64C2201/10—
    • B64C2201/16—
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/022—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising bird or foreign object protections
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0273—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for jet engines
    • B64D2700/62754—

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

Abstract

본 발명은 비행체에 관한 것으로, 정삼각형 구조에 비행체 몸체의 삼각형 꼭지점 부위 세곳에 제트엔진(2)을 각각 1개씩 설치하고, 제트엔진(2)을 방향전환(11) 하여 제트개스(7) 토출을 수직, 수평으로 270도 방향전환 조정 분출(11)하여 비행, 이,착륙하고, 전진, 후진으로 비행하며 고정익 주익(3)으로 날개로 수평비행하며, 고속비행 및 수직 이,착륙 하는 구조로써, 제트엔진(2) 상부에 공기걸음 그물망돔(4)을 설치하여 이,착륙시 제트개스(7)에 의해서 지면에서 비상하는 이물질이 제트엔진(2) 속으로 빨려 들어가서 제트엔진(2)이 손상되거나 사고가 발생하는 것을 방지하는 것이 특징인 구조로 된 제트엔진(2)으로 운행하는 비행체이다.The present invention relates to a flying body, wherein one jet engine (2) is installed at each triangular vertex portion of a flight body in a regular triangle structure, and the jet engine (2) is redirected (11) It is a structure in which a high-speed flight and a vertical landing are carried out by flying a wing with a wing wing (3), flying in a vertical, horizontal direction, The airflow net dome 4 is installed on the upper part of the jet engine 2 so that the jet engine 7 sucks foreign matter flying from the ground on the ground into the jet engine 2, (2) which is structured so as to prevent the occurrence of an accident or the occurrence of an accident.

Description

삼각제트비행체{ Triangle jet airplane }Triangle jet airplane

본 발명은 제트엔진으로 운행하는 드론(Drone) 비행체에 관한 것이다.The present invention relates to a dragon air vehicle which runs on a jet engine.

일반적으로 드론은 프로펠러 구조를 배터리 전기로 운행하는 구조로 배터리 용량 부족으로 장시간 체공 비행 할 수 없는 구조이고, 제트엔진으로 운행하는 구조는 이,착륙시 지면에서 비산하는 이물질이 제트엔진 속으로 빨려 들어가서 제트엔진이 손상되거나 사고가 발생하여 일반적으로는 제트엔진을 수직 이,착륙 구조로 드론에 사용 할 수 없는 현실이다..Generally, a dron is a structure in which a propeller structure is driven by a battery electric system and can not fly for a long time due to insufficient battery capacity. The structure of a jet engine is such that foreign substances scattered from the ground are sucked into the jet engine In general, the jet engine can not be used for vertical or landing drones due to damage to the jet engine or accidents.

본 발명은 일반적으로 프로펠러와 전기배터리 구조로 된 드론이 장시간 채공 비행이 어렵고 장거리 비행시 비행속도가 느려 장거리 비행용으로 부적합 함을 개선하고자 함이다.The present invention is intended to improve the drones of a propeller and an electric battery structure, which are difficult to carry out for a long time, and which are not suitable for long-distance flying due to a slow flight speed in long-distance flying.

본 발명은 일반적인 드론을 구성함에 있어 제트엔진(2)을 설치하여 항공유를 연료로 사용하여 장시간 채공 비행이 가능하도록 하고, 이,착륙시 비산 이물질로부터 제트엔진(2) 손상이나 사고를 방지하기 위하여 제트엔진(2) 전면 공기흡입부에 공기걸음 그물망돔(Dome)(4)을 설치한 것이 특징이다.In order to prevent damages and accidents of the jet engine 2 from foreign matter scattered during landing, it is necessary to use a jet engine 2 as a fuel to constitute a general drones, And a pneumatic mesh dome (4) is installed in the front air intake portion of the jet engine (2).

본 발명은 일반적으로 프로펠러와 전기배터리로 운행하는 드론 보다 장시간 채공 비행이 가능하고 장거리 비행 운행시 제트엔진을 수평으로 전개하고 비행체 고정 주익(3)에 의한 양력으로 비행하여 적은 연료로 장시간 채공 고속비행 하는 뛰어난 효과가 있다.The present invention is generally applicable to a drone that is operated by a propeller and an electric battery for a long period of time, and the jet engine is horizontally deployed in a long distance flight, and is fly by lift by a fixed wing 3, There is an excellent effect.

도1은 본 발명의 비행체 수직 이,착륙 상태 실시 사시도 이고
도2는 본 발명의 비행체 수직 이,착륙 상태 정면도 이고
도3은 본 발명의 비행체 전진 수평비행 상태 실시 사시도 이고
도4는 본 발명의 비행체 전진 수평비행 상태 측면도 이고
도5는 본 발명의 비행체 후진 수평비행 상태 실시 사시도 이고
도6은 본 발명의 비행체 분해 사시도 이고
도7은 본 발명의 비행체 그물망돔 사시도 이고
도8은 본 발명의 비행체 그물망돔 A-A'선 횡단면 확대도 이다.
*부호의 설명*
1.비행체몸체 2.제트엔진 3.주익 4.그물망돔 5.탑승부 6.제트개스 방향전환각 조정부 7.제트개스 8.적재물 연결부 9.착륙다리 10.지상 이동바퀴 11.제트엔진 방향전환 각 표시Fig. 1 is a perspective view of the airplane vertical landing according to the present invention
FIG. 2 is a front view of the aircraft vertical, landing state of the present invention
FIG. 3 is a perspective view illustrating the flight forward horizontal flight state of the present invention
4 is a side view of the flight forward horizontal flight state of the present invention
FIG. 5 is a perspective view of the flight backward horizontal flight state of the present invention
6 is an exploded perspective view of the air vehicle of the present invention
Fig. 7 is a perspective view of a dome of a network of the present invention
8 is an enlarged cross-sectional view of the aircraft network dome A-A 'of the present invention.
* Explanation of symbols *
1. Aircraft body 2. Jet engine 3. Wing 4. Net dome 5. Boarding section 6. Jet gas direction change angle control 7. Jet gas 8. Load connection 9. Landing bridge 10. Ground movement wheel 11. Jet engine redirect Each mark

본 발명을 첨부된 도면을 참조하여 상세히 설명하면 다음과 같다,The present invention will now be described in detail with reference to the accompanying drawings,

일반적인 비행체을 구성함에 있어 도1과 같이 정삼각형 구조의 비행몸체(1)로 삼각형 꼭지점 부위에 각각 1개씩 3개의 제트엔진(2)을 설치하고 제트엔진(2)를 270도(11) 방향전환 구조(6)로 토출하고, 수직방향으로 제트개스(7)를 분출하여 수직 이,착륙(도1)을 하고, 제트개스(7)를 수평으로 전개 분출하여 전진 및 후진 수평비행 하며, 고정 주익(3)의 날개양력으로 수평비행을 하며, 이,착륙시 지면에서 비상하는 이물질이 제트엔진(2) 속으로 빨려 들어가서 엔진이 손상 되거나 사고가 발생하는 것을 방지하기 위하여 제트엔진(2) 전면 공기흡임부에 공기걸음 그물망돔(4)을 설치한 것이 특징인 구조이다.As shown in FIG. 1, three jet engines 2 are installed at each of the triangular vertex portions of the flight body 1 having a regular triangle structure, and the jet engine 2 is rotated at 270 degrees (11) 6), vertically jetting the jetting gas 7 in the vertical direction, landing (Fig. 1), horizontally expanding and jetting the jetting gas 7, advancing and backward horizontally, The air is sucked into the jet engine 2 in order to prevent the engine from being damaged or an accident from occurring when the air is sucked into the jet engine 2, And a pneumatic mesh dome (4) is provided on the pneumatic tire.

Claims (2)

비행체를 구성함에 있어 삼각형 구조의 비행몸체의 삼각형 꼭지점 부위에 제트엔진(2)을
각각 1개씩 설치하고 제트개스(11)를 방향전환 구조(6)로 분출각을 조정하여 수직 이,착륙 및 전진, 후진 수평비행을 하고, 고정주익(3) 양력으로 수평비행 하며, 수직 이,착륙시 지면에서 비상하는 이물질로 인한 제트엔진(2)의 손상과 사고를 방지하기 위하여 제트엔진(2) 전면 공기 흡입부에 공기걸음 그물망돔(4)을 설치한 구조가 특징인 비행체.In constructing the aircraft, a jet engine (2) is mounted on the vertex of the triangle of the flying body of the triangular structure
(1), and the vertical direction, landing, forward, and backward horizontal flight are adjusted by adjusting the jet angle of the jet gas (11) to the direction switching structure (6) (4) is installed in the air intake part at the front of the jet engine (2) in order to prevent damage and accident of the jet engine (2) due to foreign matter flying on the ground when landing. 제1항에 있어서 제트엔진 전면부 공기흡입부에 공기걸음 그물망돔을 장착한 제트엔진을 설치한 구조.The structure according to claim 1, wherein a jet engine having an air walking net dome mounted on the front air intake portion of the jet engine is installed.
KR1020170023782A 2017-02-21 2017-02-21 Triangle jet airplane Withdrawn KR20180096455A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020170023782A KR20180096455A (en) 2017-02-21 2017-02-21 Triangle jet airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020170023782A KR20180096455A (en) 2017-02-21 2017-02-21 Triangle jet airplane

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KR20180096455A true KR20180096455A (en) 2018-08-29

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021064499A1 (en) * 2019-10-03 2021-04-08 Tran Vo Trung Automatic flying delivery drone in precalculated flight routes and method for delivering merchandises
CN113277079A (en) * 2021-05-12 2021-08-20 上海工程技术大学 Jet-propelled vertical take-off and landing unmanned aerial vehicle capable of realizing thrust vector control
KR102385180B1 (en) * 2020-12-21 2022-04-08 이정용 Multi-directional jet propulsion drone

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021064499A1 (en) * 2019-10-03 2021-04-08 Tran Vo Trung Automatic flying delivery drone in precalculated flight routes and method for delivering merchandises
KR102385180B1 (en) * 2020-12-21 2022-04-08 이정용 Multi-directional jet propulsion drone
CN113277079A (en) * 2021-05-12 2021-08-20 上海工程技术大学 Jet-propelled vertical take-off and landing unmanned aerial vehicle capable of realizing thrust vector control

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Patent event code: PA01091R01D

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Patent event date: 20170221

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