RU2071213C1 - BALANCED AIRCRAFT - Google Patents
BALANCED AIRCRAFT Download PDFInfo
- 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
Links
Landscapes
- 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.
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) |
-
1994
- 1994-05-31 RU RU94020216/11A patent/RU2071213C1/en active
Also Published As
Publication number | Publication date |
---|---|
RU94020216A (en) | 1997-04-10 |
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