RU2013148254A - SHORT AIRPLANE AND LANDING WING - Google Patents
SHORT AIRPLANE AND LANDING WING Download PDFInfo
- Publication number
- RU2013148254A RU2013148254A RU2013148254/11A RU2013148254A RU2013148254A RU 2013148254 A RU2013148254 A RU 2013148254A RU 2013148254/11 A RU2013148254/11 A RU 2013148254/11A RU 2013148254 A RU2013148254 A RU 2013148254A RU 2013148254 A RU2013148254 A RU 2013148254A
- Authority
- RU
- Russia
- Prior art keywords
- flap
- pivotally connected
- sliding panels
- link
- wing
- Prior art date
Links
Landscapes
- Transmission Devices (AREA)
- Cleaning In General (AREA)
Abstract
Крыло самолета короткого взлета и посадки, с установленными в верхней части жесткими сдвижными панелями, содержащее щелевые закрылки с каретками и опорными роликами, направляющие рельсы перемещения закрылка, механизмы уборки выпуска, отличающееся тем, что сдвижные панели через складывающиеся тяги шарнирно связаны с щитком дефлектора, подвижно установленным в носовой части основного звена закрылка, а верхнее звено складывающейся тяги шарнирно соединено с механизмом уборки выпуска закрылка.The wing of a short take-off and landing aircraft, with rigid sliding panels installed in the upper part, containing slotted flaps with carriages and support rollers, flap guiding rails, exhaust cleaning mechanisms, characterized in that the sliding panels are pivotally connected to the deflector shield via folding drafts, movably installed in the bow of the main flap link, and the upper link of the folding thrust is pivotally connected to the flap release cleaning mechanism.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013148254/11A RU2562005C2 (en) | 2013-10-29 | 2013-10-29 | Vtol aircraft wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2013148254/11A RU2562005C2 (en) | 2013-10-29 | 2013-10-29 | Vtol aircraft wing |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2013148254A true RU2013148254A (en) | 2015-05-27 |
RU2562005C2 RU2562005C2 (en) | 2015-09-10 |
Family
ID=53284712
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2013148254/11A RU2562005C2 (en) | 2013-10-29 | 2013-10-29 | Vtol aircraft wing |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2562005C2 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3874617A (en) * | 1974-07-17 | 1975-04-01 | Mc Donnell Douglas Corp | Stol flaps |
RU2072944C1 (en) * | 1992-12-03 | 1997-02-10 | Московский машиностроительный завод "Скорость" им.А.С.Яковлева | Flap extending device |
RU2261821C2 (en) * | 2003-12-05 | 2005-10-10 | Воронежский государственный технический университет | Slotted flap |
RU2385261C1 (en) * | 2008-12-10 | 2010-03-27 | Государственное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Vtol aircraft wing |
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2013
- 2013-10-29 RU RU2013148254/11A patent/RU2562005C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2562005C2 (en) | 2015-09-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20161030 |