SU1804039A1 - Device for controlling flaps - Google Patents
Device for controlling flapsInfo
- Publication number
- SU1804039A1 SU1804039A1 SU4608905/63A SU4608905A SU1804039A1 SU 1804039 A1 SU1804039 A1 SU 1804039A1 SU 4608905/63 A SU4608905/63 A SU 4608905/63A SU 4608905 A SU4608905 A SU 4608905A SU 1804039 A1 SU1804039 A1 SU 1804039A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- fairing
- flap
- link
- piece
- cross
- Prior art date
Links
Landscapes
- Transmission Devices (AREA)
Abstract
FIELD: aircraft engineering. SUBSTANCE: device has a beam made in the form of rectilinear rail and connected with bearing frame of the wing, flap connected through a hinge with variable-length tie made in the form of a carriage moving along the rail. The flap is connected also with the fairing by means of a cross-piece and ties pivotally secured to this cross-piece. The fairing consists of tail and nose links. The cross piece is connected with the carriage through a hinge, with the nose link of the fairing by means of hinges mounted on the ties and with tail link of the fairing by means of variable-length tie. The tail link is rotatable relative to the nose link and the nose link is rotatable relative to beam made in the form of rectilinear rail. When actuated by the drive, the carriage, connected with the cross-piece and the flap, moves along the rail and makes the links rotate together with deviation of the flap. The device may be used both in straight-winged and swept winged aircraft. EFFECT: reduced overall dimensions of the flap control device, reduced aerodynamic resistance of fairing and the aircraft as a whole. 3 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4608905/63A SU1804039A1 (en) | 1988-11-25 | 1988-11-25 | Device for controlling flaps |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4608905/63A SU1804039A1 (en) | 1988-11-25 | 1988-11-25 | Device for controlling flaps |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1804039A1 true SU1804039A1 (en) | 1995-01-27 |
Family
ID=60536912
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4608905/63A SU1804039A1 (en) | 1988-11-25 | 1988-11-25 | Device for controlling flaps |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1804039A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2560218C1 (en) * | 2014-06-19 | 2015-08-20 | Открытое Акционерное Общество "Научно-Производственная Корпорация "Иркут" | Flaps drive assembly |
RU2613375C2 (en) * | 2011-07-21 | 2017-03-16 | Зе Боинг Компани | Aerodynamic device with hinged flap (versions) and method of deploying hinged flap |
CN113602475A (en) * | 2021-08-31 | 2021-11-05 | 中国商用飞机有限责任公司 | Wing flap fairing mechanism |
-
1988
- 1988-11-25 SU SU4608905/63A patent/SU1804039A1/en active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2613375C2 (en) * | 2011-07-21 | 2017-03-16 | Зе Боинг Компани | Aerodynamic device with hinged flap (versions) and method of deploying hinged flap |
RU2560218C1 (en) * | 2014-06-19 | 2015-08-20 | Открытое Акционерное Общество "Научно-Производственная Корпорация "Иркут" | Flaps drive assembly |
CN113602475A (en) * | 2021-08-31 | 2021-11-05 | 中国商用飞机有限责任公司 | Wing flap fairing mechanism |
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