RU2071213C1 - BALANCED AIRCRAFT - Google Patents

BALANCED AIRCRAFT Download PDF

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Publication number
RU2071213C1
RU2071213C1 RU94020216/11A RU94020216A RU2071213C1 RU 2071213 C1 RU2071213 C1 RU 2071213C1 RU 94020216/11 A RU94020216/11 A RU 94020216/11A RU 94020216 A RU94020216 A RU 94020216A RU 2071213 C1 RU2071213 C1 RU 2071213C1
Authority
RU
Russia
Prior art keywords
pylon
screen
fairing
aircraft
nose
Prior art date
Application number
RU94020216/11A
Other languages
Russian (ru)
Other versions
RU94020216A (en
Inventor
А.П. Даньшин
И.В. Кучеров
А.С. Перловский
М.М. Печенкин
М.Е. Трушин
А.В. Храпов
С.В. Червяков
Е.С. Шахиджанов
В.А. Щербаков
Original Assignee
Акционерное общество "Компания "Биман"
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 Акционерное общество "Компания "Биман" filed Critical Акционерное общество "Компания "Биман"
Priority to RU94020216/11A priority Critical patent/RU2071213C1/en
Priority to PCT/RU1994/000177 priority patent/WO1995007216A1/en
Priority to AU75099/94A priority patent/AU7509994A/en
Application granted granted Critical
Publication of RU2071213C1 publication Critical patent/RU2071213C1/en
Publication of RU94020216A publication Critical patent/RU94020216A/en

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  • Bridges Or Land Bridges (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1. Летательный аппарат с балансирным управлением, содержащий крыло, шарнирно соединенное с пилоном балочной матотележки, обтекатель и защитный экран, закрепленный в носовой части обтекателя и на пилоне, отличающийся тем, что летательный аппарат дополнительно снабжен шарнирными механизмами и механизмом компенсации, кинематически взаимодействующим с защитным экраном и пилоном, при этом на экране закреплены П-образные направляющие, в которые помещены цилиндрические опоры, закрепленные на пилоне, а шарнирные механизмы установлены симметрично в передней части экрана и закреплены в носовой части обтекателя.2. Аппарат по п.1, отличающийся тем, что шарнирный механизм выполнен в форме замка.1. Aircraft with balancer control, comprising a wing pivotally connected to the pylon of the girder, a fairing and a protective screen mounted in the nose of the fairing and on the pylon, characterized in that the aircraft is additionally equipped with hinged mechanisms and a compensation mechanism that kinematically interacts with the protective a screen and a pylon, while U-shaped guides are fixed on the screen, into which cylindrical supports are mounted, mounted on the pylon, and the hinge mechanisms are installed symmetrically at the front of the screen and secured to the nose of the fairing. 2. The apparatus according to claim 1, characterized in that the hinge mechanism is made in the form of a lock.

RU94020216/11A 1993-03-29 1994-05-31 BALANCED AIRCRAFT RU2071213C1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
RU94020216/11A RU2071213C1 (en) 1994-05-31 1994-05-31 BALANCED AIRCRAFT
PCT/RU1994/000177 WO1995007216A1 (en) 1993-03-29 1994-08-03 Ultra-lightweight aircraft and an aircraft wing with a soft skin
AU75099/94A AU7509994A (en) 1993-03-29 1994-08-03 Ultra-lightweight aircraft and an aircraft wing with a soft skin

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94020216/11A RU2071213C1 (en) 1994-05-31 1994-05-31 BALANCED AIRCRAFT

Publications (2)

Publication Number Publication Date
RU2071213C1 true RU2071213C1 (en) 1996-12-27
RU94020216A RU94020216A (en) 1997-04-10

Family

ID=48432112

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94020216/11A RU2071213C1 (en) 1993-03-29 1994-05-31 BALANCED AIRCRAFT

Country Status (1)

Country Link
RU (1) RU2071213C1 (en)

Also Published As

Publication number Publication date
RU94020216A (en) 1997-04-10

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