KR20020017542A - Vertical takeoff and landing small plane - Google Patents

Vertical takeoff and landing small plane Download PDF

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Publication number
KR20020017542A
KR20020017542A KR1020000050940A KR20000050940A KR20020017542A KR 20020017542 A KR20020017542 A KR 20020017542A KR 1020000050940 A KR1020000050940 A KR 1020000050940A KR 20000050940 A KR20000050940 A KR 20000050940A KR 20020017542 A KR20020017542 A KR 20020017542A
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South Korea
Prior art keywords
engine
airplane
dongchae
landing
engines
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KR1020000050940A
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Korean (ko)
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임두남
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임두남
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Priority to KR1020000050940A priority Critical patent/KR20020017542A/en
Publication of KR20020017542A publication Critical patent/KR20020017542A/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/02Gyroplanes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Emergency Lowering Means (AREA)

Abstract

PURPOSE: A vertical takeoff and landing airplane is provided to fly safely by driving vertically, and to keep the balance of the fuselage by distributing plural engines in the body of the multipurpose airplane. CONSTITUTION: A small airplane is vertically taken off and landed without a landing strip, and moved left and right, and up and down. A fuselage of the airplane is formed with trapezoid structures(1,2) with a column(3). A rafter(4) is installed in the upper part to insert conveniently, and an engine(8) for moving forward, left or right, and up and down is installed in the front of the body of the airplane. The upper opening part except for the engine installation space is covered with fabric cloth to operate as wings of the airplane. A small engine(5) is installed in the column, and a propeller is mounted in a driving unit in the roof, and the engine is mounted in an engine installation board(10). The airplane flies forward, and turns up and down, and left and right with operating levers(9). The load is distributed with arranging engines evenly, and the stability is improved with vertically flying in an emergency.

Description

수직 이착륙 소형비행기{.}Vertical takeoff and landing small plane {.}

본 발명은 대소 몇종의 소형 엔진을 다수 이용한 수직 이착륙 및 상하 좌우를 자유롭게 비행하며 그리고 특별한 훈련없이 단시간에 조종을 습득 할 수 있음을 목적으로 하는 수직이착륙 소형 비행기에 관한 것을 목적으로 한다.The present invention aims at a vertical take-off and landing small plane using a large number of small and small engines, and freely flying vertically, landing, vertically and horizontally, and gaining control in a short time without special training.

종래에는 이러한 형의 소형 비행기는 없는 것으로 사료됨.Conventionally, there is no such small airplane.

본 발명은 수직 이착륙 비행기를 제작함에 안전하고 저렴한 생산비와 손쉽게 조종할 수 있는 비행기의 구조이다.The present invention is a safe and low cost of manufacturing a vertical take-off and landing airplane structure of the airplane that can be easily controlled.

제 1 도는 본 발명의 사시도1 is a perspective view of the present invention

제 2 도는 본 발명의 전진 및 좌우상하로 진로를 바꿀때 사용되는 엔진2 is an engine used to advance the course of the present invention and to change course from side to side

(1 도 8)을 설치한 설치대의 확대도Enlarged view of the mounting table (1 FIG. 8)

* 도면의 주요부분에 대한 부호 설명 *Explanation of symbols on the main parts of the drawings

1 도 1,2 : 동채의 간골인 상하 사다리꼴의 구조물1 and 1: 1: structure of the upper and lower trapezoid which is the bone of Dongchae

1 도 3 : 동채의 사다리꼴이 상하 간골을 잇는 기둥1 Fig.: A pillar in which the trapezoid of the Dongchae connects the upper and lower stems

1 도 4 : 동채의 좌우로 연설한 서까래로서 발취와 삽설이 용이함.1 Fig. 4: A rafter that speaks from the left and right of the dongchae as easy to extract and insert.

1 도 5 : 기둥 옆에 장치한 양력용 소엔진1 FIG. 5: Lifting Small Engine Installed Beside a Column

1 도 6 : 엔진에 착설된 프로펠러1 Fig. 6: Propeller mounted on the engine

1 도 7 : 와이어로 엮어 만든 동채의 바닥1 Fig.: Bottom of copper foil made of wire

1 도 8 : 비행용 큰엔진1 Fig. 8: Large engine for flight

1 도 9 : 엔진의 조종용 손잡이 1 도 10 : 엔진을 장치한 엔진 설치대1 Fig. 9: Control knob of the engine 1 Fig. 10: Engine mounting table equipped with the engine

1 도 11 : 엔진 설치대(1 도 10)와 가동파이프(2 도 3)와 연결 고정된 톱니판으로 엔진(1 도 8)을 상하로 각도 변경 고정할 시 사용됨.1 Fig. 11: Used to fix the engine (1 Fig. 8) by changing the angle up and down with the tooth plate fixed to the engine mount (1 Fig. 10) and the movable pipe (2 Fig. 3).

1 도 12 : 상하 각도 고정용 톱니(1 도 11)를 고정하는 핀으로서 스프링 장치가 되어 있어 당겼다 각도를 변경후 다시 놓으면 톱니에 끼워져 고정이 된다.1 Fig. 12: Pins for fixing the up and down angle fixing teeth (1 Fig. 11), which are spring-loaded.

1 도 13 ; 엔진(1 도 8) 의 프로펠러1 FIG. 13; Propeller of engine 1 FIG. 8

1 도 14 : 좌우회전 가능한 바퀴1 Fig. 14: Rotatable wheel

1 도 15 : 바퀴1 degree 15: wheels

1 도 16 : 탑승자들의 의자를 걸수 있는 고리로서, 의자는 그네식으로 줄의 일부는 스프링으로 됨.1 FIG. 16: Hooks for hanging chairs of passengers, the chairs being swinged, part of the rope being a spring.

1 도 17 : 서까래의 고정용 와이어1 Fig. 17: Fixing wire for rafters

1 도 18 : 고도계 및 각엔진의 조작 레바를 설치한 조작판1 Fig. 18: Operation panel on which altimeter and operating lever of each engine are installed

2 도 1 : 엔진 설치대를 장착한 동채 앞부분의 골간2 Fig. 1: Interbody bone of the front part of the copper clad with engine mount

2 도 2 : 엔진 설치대의 좌우 요동을 제한한 고정용 링.2 Fig. 2: Retaining ring with limited left and right swing of the engine mount.

2 도 3 : 골간(2 도 1)에 끼워진 파이프로서 설치대(2 도 4)와 견고하게 결합되 있으며 프로펠러를 수평 및 상하로 조작할 때 자유로이 조작됨.2 Fig. 3: Pipe fitted into the interbody bone (2 Fig. 1), firmly coupled to the mounting table (2 Fig. 4), and freely operated when the propeller is operated horizontally and vertically.

2 도 4 : 파이프(2 도 3)에 견고하게 접착되 있는 엔진 설치대의 밑판으로 중앙에는 견실한 볼트가 입설 되있으며 설치대의 좌우 가동용 상판(2 도 10)을 스프링, 와샤,볼트,낫트 등으로 고정시킴.2 Fig. 4: The bottom plate of the engine mount that is firmly bonded to the pipe (2 Fig. 3) with a solid bolt installed in the center and the springs, washers, bolts, nuts, etc. Fixed with.

2 도 5 : 파이프(2 도 3)에 견고하게 부착되 있는 톱니 바퀴로 톱니의 골이 깊게 파여 있으며 쐐기용핀(2 도 7)을 당겼다 놓면은 견고하게 삽착 하게 되있음. 그러므로 엔진 설치대를 필요한 각도로 유지할 수 있음.2 Fig. 5: Cog wheels firmly attached to pipe (2 Fig. 3), the teeth of the tooth are deeply dug and pull the wedge pin (2 Fig. 7). Therefore, the engine mount can be kept at the required angle.

2 도 6 : 톱니판에 작용되는 핀(2 도 7)을 톱니판 쪽으로만 작용시키기 위한 스프링이 장착된 통.Fig. 6: Spring-loaded barrel for actuating pins (2 Fig. 7) acting on the tooth plate only toward the tooth plate.

2 도 7 : 톱니판(2 도 5)에 작용되는 핀으로써 조작시에는 손잡이를 당겨서사용함.2 Fig. 7: It is a pin acting on the tooth plate (2 Fig. 5).

2 도 8 : 핀(2 도 7)을 견고하게 고정키 위한 대판으로서 골간(2 도 9)에 견고하게 부착되 있음.2 Fig. 8: A base for firmly fixing the pin (2 Fig. 7) and firmly attached to the bone shaft (2 Fig. 9).

2 도 9 : 동채 왼쪽 골간의 일부.2 Figure 9: Dongchae left bone of the bone.

2 도 10: 여기에 엔진(1 도 8)이 설치되며 좌우로 움직일 수 있는 작용을 할 수 있게 된 엔진 부착대의 상판.2 Fig. 10: An upper plate of an engine mount on which an engine (1 Fig. 8) is installed and which can move left and right.

2 도 11: 엔진 부착대(2 도 10)의 결합용 볼트,낫트2 Fig. 11: Bolts and nuts for joining the engine mount (2 Fig. 10)

2 도 12: 엔진 부착대(2 도 10)가 정면 위치에 있을 때 좌우 요동을 막기 위한 철 구슬을 스프링으로 누르는 형의 고정구의 구멍.2 Fig. 12: Holes in the fixture of the spring pressing iron balls to prevent left and right swings when the engine mount (2 Fig. 10) is in the front position.

2 도 13 : 엔진 부착대(2 도 10)의 좌우조작한계 핀.2 Fig. 13: Left and right operation limit pins of the engine mount (2 Fig. 10).

본 발명을 도면에 의하여 자세히 설명하면 제 1도와 같이 상하 두개의 사다리꼴(1도 1,2)의 경금속제 구조물을 기둥(1 도 3)으로 구축한 골조형의 동채의 상개에는 좌우로 각기 발취식의 석가래(1 도 4)를 연설하여 기둥 밑쪽과 와이어(1 도 17)로 고정시키고, 그리고 동채의 밑쪽에는 바퀴(1 도,14,15)를 착설하고 각기둥(1 도 3)옆에는 각기 소형엔진(1 도 5)등을 설치코 구동 장치를 동채의 상개 윗쪽으로 충분히 연설코 상단에 프로펠러를 각기 착설코 조작케이불은 조작판(1 도 18)에 연결하고 동채의 중앙 앞에는 프로펠러의 추진방향을 좌우상하로 조작 할 수 있는 엔진설치대(1 도10,2 도 10)에 큰엔진(1 도 8)을 설치하며, 엔진에 부착된 손잡이(1 도 9)등으로 조작하며 방향을 고정할 때에는 제 2 도에서 보는 바와 같은 고정구 손잡이(2 도 7)를 당겼다가 위치 변경후 다시 놓으면 톱니판(2 도 5)에 핀이 삽착 되면서 고정됨, 그리고 동채의 지붕은 앞쪽 큰 엔진(1 도 8)이 설치된 칸외에는 모두 적절한 천을 씌워서 비행시 날개로 역활케 됐으며, 운항방법은 필요에 의해 여러가지로 동작 시킬 수 있겠으나 일반적으로 동작하는 순서를 말하자면 모든 엔진을 하나하나 저속으로 가동시키며 이때에 전진용 큰엔진(1 도 8)은 프로펠러의 위치를 수직상향시켜 놓고 나머지 각엔진을 순차적으로 조금씩 세개 가동함으로서 수직으로 이륙비상하며 적당한 고도에 달했을때 전진용 큰엔진(1 도 8)을 수평 혹은 수평보다 약간 상향하여 고정 시키고 비행하며 고도계를 보며 나머지 소형엔진 등을 다시 약하게 가동 하면 된다. 하강시는 앞큰엔진으로 적당한 고도까지 하향하여 목적지에 달했을 때 큰언진(1 도 8)을 약하게 가동하며 다시 프로펠러를 사향고정시키고 가타 엔진의 기동력을 적당히 가감하며 착륙함, 이때 큰엔진(1 도 8)을 상향함은 하강시 기타 엔진에 이상이 발생시는 즉시 강하게 가동하여 보조 역활을 하여 사고를 막기 위함임. 동채의 바닥은 와이어(1 도 7)로 절어서 만들며 탑승석은 그네식 의자를 고리(1 도 16)에 걸어서 사용한다.When the present invention is described in detail with reference to the drawings, the upper and lower two trapezoids (1 and 1 and 2) of the light metal structure, which is constructed from pillars (1 and 3), respectively, the upper and lower sides of the framed copper-collars Speaking of sputum (1 Fig. 4) to the bottom of the pillar and fixed with a wire (1 Fig. 17), and the bottom of the Dongchae to install the wheels (1 Fig., 14, 15) and next to each pillar (1 Fig. 3) Install a small engine (1 Fig. 5), etc. Install the nose drive device to the upper part of the Dong Chae. The propeller is installed at the top of the main engine. The operation cable is connected to the operation panel (1 Fig. 18). Install a large engine (1 Fig. 8) on an engine mount (1 Fig. 10, 2 Fig. 10) that can be operated up and down and up and down. Pull the fixture handle (2 Fig. 7) as shown in Fig. 2 and then change the position When it is put back, the pin is inserted into the tooth plate (2 degrees 5) and fixed, and the roof of the dongchae is covered with the appropriate cloth outside the compartment where the large engine (1 degrees 8) is installed, and it becomes a wing during the flight. It can be operated in various ways, but in general, all the engines are operated at low speed one by one. In this case, the large engine for forward movement (1 Fig. 8) moves the propellers vertically upward and the rest of the engines sequentially. By operating three, take off vertically and take off vertically. When the proper altitude is reached, the large engine for forward movement (1 degree 8) is fixed up or down slightly above the horizontal or horizontal. When descending, the engine is lowered to the proper altitude, and the large engine (1 degree 8) is weakly operated when reaching the destination, and the propeller is fixed again, and the maneuvering power of the other engine is moderately added or lowered. ) Is to prevent accidents by acting strongly as soon as possible when other engine abnormalities occur when descending. The bottom of the copper house is made by folding the wire (1 Fig. 7) and the boarding seat is used by hanging the swing chair on the hook (1 Fig. 16).

또한 이륙용 소엔진 등의 회전방향은 동채의 좌우 엔진이 서로 반대임.In addition, the direction of rotation of small engines for takeoff is the opposite of the left and right engines of Dongchae.

본 발명은 저렴한 생산비로 조종이 용이하며, 관광용, 레저용,농업용,근거리 교통수단 등 아주 편리함이 있다.The present invention is easy to operate at a low production cost, it is very convenient for tourism, leisure, agriculture, local transportation and the like.

Claims (1)

본 발명은 도면과 전항에서 설명한 바와 같이 수직 이착륙 소형비행기로서 동채를 도면과 같은 길다란 사각통형의 경금속 골조물로 구성하고 그 지붕은 적절한 직포로 전면을 씌우고 동채의 좌우로 각기종의 크기의 필요에 따른 형의 상승용 프로펠러 엔진(1 도 5)을 다수 설치하여 동채에 작용하는 인양력을 분산시키며 이로 인하여 동채의 평행유지를 용이하게 한점과 전진용 큰엔진(1 도 8)을 동채의 앞부분에 설치하여 전진 및 수직상승에 이용하며 상하 좌우 방향의 비행을 할 수 있게 한 것이며, 특히 큰엔진(1 도 8)을 설치함에 상하 좌우로 움직일 수 있는 엔진 설치대(제 2 도)의 구조.The present invention is a vertical take-off and landing small airplane as described in the drawings and the preceding paragraph is composed of a light metal frame of elongated rectangular cylindrical shape as shown in the drawing and the roof is covered with the appropriate woven front and the right and left of the Dongchae to meet the needs of different sizes A plurality of lifting propeller engines (1 Fig. 5) of the type are installed to distribute the lifting force acting on the Dongchae, which makes it easier to maintain the parallelism of the Dongchae and a large engine for moving forward (1 Fig. 8) on the front of the Dongchae. It is installed to be used for forward and vertical ascension and to be able to fly vertically and horizontally. In particular, the structure of the engine mount (second degree) that can move up, down, left and right when installing a large engine (1 degree 8).
KR1020000050940A 2000-08-30 2000-08-30 Vertical takeoff and landing small plane KR20020017542A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160120094A (en) 2015-04-07 2016-10-17 문종성 Flying board
CN106697304A (en) * 2017-02-28 2017-05-24 天峋(常州)智能科技有限公司 High-reliability aircraft engine mounting mechanism

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5461799A (en) * 1977-10-24 1979-05-18 Takayoshi Ishigaki Vertical takeeoff and landing plane
JPS62238196A (en) * 1986-04-09 1987-10-19 菊池 直美 Rotor type missile
JPH04173497A (en) * 1990-11-05 1992-06-22 Haruo Sukai Flying body
JP2000085692A (en) * 1998-09-16 2000-03-28 Homare Shoji:Kk Airplane

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5461799A (en) * 1977-10-24 1979-05-18 Takayoshi Ishigaki Vertical takeeoff and landing plane
JPS62238196A (en) * 1986-04-09 1987-10-19 菊池 直美 Rotor type missile
JPH04173497A (en) * 1990-11-05 1992-06-22 Haruo Sukai Flying body
JP2000085692A (en) * 1998-09-16 2000-03-28 Homare Shoji:Kk Airplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160120094A (en) 2015-04-07 2016-10-17 문종성 Flying board
CN106697304A (en) * 2017-02-28 2017-05-24 天峋(常州)智能科技有限公司 High-reliability aircraft engine mounting mechanism

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