KR20170028615A - 분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술 - Google Patents

분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술 Download PDF

Info

Publication number
KR20170028615A
KR20170028615A KR1020150125439A KR20150125439A KR20170028615A KR 20170028615 A KR20170028615 A KR 20170028615A KR 1020150125439 A KR1020150125439 A KR 1020150125439A KR 20150125439 A KR20150125439 A KR 20150125439A KR 20170028615 A KR20170028615 A KR 20170028615A
Authority
KR
South Korea
Prior art keywords
principle
vstol
harrier
output
nozzles
Prior art date
Application number
KR1020150125439A
Other languages
English (en)
Inventor
한현
Original Assignee
한현
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 한현 filed Critical 한현
Priority to KR1020150125439A priority Critical patent/KR20170028615A/ko
Publication of KR20170028615A publication Critical patent/KR20170028615A/ko

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)

Abstract

VSTOL - vertical short take-off and landing.의 감추어진 원리 → 기존의 국내에 자료들은 수직이착륙이 양력값이 동체를 이긴다고만 추상적으로 말하고 원리를 설명하지 못하여 실제 생산이나 전투기에 반영하지 못함.
하지많 양력값이라는 vstol의 수직양력이 동체를 들어올리는 것은 일반인들이 생각하는것 같이 그 힘이(출력이) 강하기 때문이 아님.
이유(원리)는 간단함. 헤리어(영국제 vstol) 이륙 장면을 보면 완전 평형 상태로 이륙하지 않는 것을 볼수 있음. 이유는 바로 노즐에 있는데 이 노즐이 두개가 가까이에 붙어서 출력을 하는데, 이때 출력이 동시에 일어나면 동체가 공기도르레 원리를 받을수 없으나 가깝게 배치된 노즐이 약각의 시간차를 두고 연료를 내뿜으면 동체가 쉽게 {(쉬운힘 - 쉬운출력)으로) 동체가 공기도르레 힘을 받아} 뜨게됨
이게 바로 헤리어(vstol)의 수직이착륙 원리임.

Description

분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술{the vstol principle}
항공우주공학
수직이착륙 항공기의 기술이 국내에는 이해되지 못하고 잘못 알려져 있어 실제로 엔진 분사형 수직이착륙기(영국의 해리어)를 만들지 못하나, 항공우주공학과 물리학 기술이 적용되면 vstol 기능이 가능
.
과제는 수직이착륙기를 생산하지 못하는 국내현실이고 요약서 기술을 응용 vstol 기 생산 가능화
수직이착륙 분사형 항공기 국내 생산(영국의 해리어 유형)
분사의 시간 차이가 나는 쌍노즐 항공기 장착

Claims (1)

  1. 수직이착륙기(분사형) 기본 설계
KR1020150125439A 2015-09-04 2015-09-04 분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술 KR20170028615A (ko)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1020150125439A KR20170028615A (ko) 2015-09-04 2015-09-04 분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1020150125439A KR20170028615A (ko) 2015-09-04 2015-09-04 분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술

Publications (1)

Publication Number Publication Date
KR20170028615A true KR20170028615A (ko) 2017-03-14

Family

ID=58459967

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020150125439A KR20170028615A (ko) 2015-09-04 2015-09-04 분사형 수직이착륙 비행기(vstol) - 수직이착륙 기술

Country Status (1)

Country Link
KR (1) KR20170028615A (ko)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113428391A (zh) * 2021-08-09 2021-09-24 哈尔滨工业大学 一种结合气浮球轴承与气浮平面止推轴承的单球式气浮滑轮装置

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113428391A (zh) * 2021-08-09 2021-09-24 哈尔滨工业大学 一种结合气浮球轴承与气浮平面止推轴承的单球式气浮滑轮装置
CN113428391B (zh) * 2021-08-09 2022-04-29 哈尔滨工业大学 一种结合气浮球轴承与气浮平面止推轴承的单球式气浮滑轮装置

Similar Documents

Publication Publication Date Title
WO2016109003A3 (en) Delta fuselage for vertical take-off and landing (vtol) aircraft
WO2017048336A3 (en) Devices and methods for in flight transition vtol/fixed wing hybrid aircraft structures and flight modes
USD875643S1 (en) Aircraft galley bay air vent
CA2947974A1 (en) Vtol aircraft
USD741247S1 (en) VTOL aircraft
USD810095S1 (en) Display panel portion with a graphical user interface component for an aircraft maintenance interface
EP3724071A4 (en) VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT SYSTEM WITH VARIABLE GEOMETRY
USD801856S1 (en) Amphibious unmanned vertical takeoff and landing aircraft
NZ742223A (en) Vertical takeoff and landing aircraft
WO2017131834A3 (en) Pivoting wing system for vtol aircraft
WO2016003530A3 (en) Vertical takeoff and landing (vtol) unmanned aerial vehicle (uav)
EP3941828A4 (en) PLANE TAKE OFF AND LAND VERTICALLY
WO2016200502A3 (en) Remotely controlled modular vtol aircraft and re-configurable system using same
WO2017123346A3 (en) Uav with wing-plate assemblies providing efficient vertical takeoff and landing capability
WO2015108578A3 (en) Vertical take-off and landing aircraft
EP3464064A4 (en) AIR VEHICLE WITH VERTICAL TAKE-OFF AND LANDING WINGS (VTOL) WITH ADDITIONAL ANGULAR ROTORS
EP3458356A4 (en) VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH INCLINED WING CONFIGURATIONS
WO2016053996A3 (en) Aircraft with speed or acceleration command
EP3492377A4 (en) VERTICAL STARTING AND LANDING PLANE
EP3224140B8 (en) High speed multi-rotor vertical takeoff and landing aircraft
WO2015160394A3 (en) Asymmetric aircraft and their launch and recovery systems from small ships
WO2015143093A3 (en) Aerodynamically efficient lightweight vertical take-off and landing aircraft with pivoting rotors and stowing rotor blades
WO2017085616A3 (en) Detachable pilotable capsules and aircrafts including detachable pilotable capsules
WO2011081683A8 (en) Lightweight vertical take-off and landing aircraft and flight control paradigm using thrust differentials
WO2016028358A3 (en) High Performance VTOL Aircraft

Legal Events

Date Code Title Description
A201 Request for examination
E902 Notification of reason for refusal
E601 Decision to refuse application