SU1272628A1 - MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT - Google Patents
MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFTInfo
- Publication number
- SU1272628A1 SU1272628A1 SU3834386/23A SU3834386A SU1272628A1 SU 1272628 A1 SU1272628 A1 SU 1272628A1 SU 3834386/23 A SU3834386/23 A SU 3834386/23A SU 3834386 A SU3834386 A SU 3834386A SU 1272628 A1 SU1272628 A1 SU 1272628A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- aerodynamic surface
- steering actuator
- longitudinal axis
- aircraft
- supporting element
- Prior art date
Links
Landscapes
- Details Of Aerials (AREA)
Abstract
1. Система управления аэродинамической поверхностью летательного аппарата, содержащая шарнирно установленный на неподвижной конструкции рулевой привод, шарнирно присоединенный к аэродинамической поверхности, отличающаяся тем, что, с целью увеличения ресурса и снижения веса аэродинамической поверхности за счет уменьшения изгибающих нагрузок, параллельно продольной оси рулевого привода установлен опорный элемент, шарнирно соединенный одним концом с основной неподвижной частью конструкции, а другим - с аэродинамической поверхностью, ось вращения которой совмещена с осью шарнира опорного элемента.2. Система по п.1, отличающаяся тем, что опорный элемент выполнен в виде двух жестких стержней, расположенных по разные стороны рулевого привода и параллельных продольной оси рулевого привода.3. Система по п.1, отличающаяся тем, что опорный элемент выполнен в виде охватывающего рулевой привод У-образного элемента, продольная ось которого совпадает с продольной осью рулевого привода.1. The control system of the aerodynamic surface of the aircraft, containing pivotally mounted on a fixed structure steering gear, pivotally attached to the aerodynamic surface, characterized in that, in order to increase the resource and reduce the weight of the aerodynamic surface by reducing bending loads the supporting element, pivotally connected at one end with the main fixed part of the structure, and the other with the aerodynamic surface, the axis of rotation of which is combined with the axis of the hinge of the support element. A system according to claim 1, characterized in that the supporting element is made in the form of two rigid rods located on opposite sides of the steering actuator and parallel to the longitudinal axis of the steering actuator. A system according to claim 1, characterized in that the supporting element is made in the form of a U-shaped element encompassing the steering actuator, whose longitudinal axis coincides with the longitudinal axis of the steering actuator.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3834386/23A SU1272628A1 (en) | 1985-01-04 | 1985-01-04 | MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3834386/23A SU1272628A1 (en) | 1985-01-04 | 1985-01-04 | MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1272628A1 true SU1272628A1 (en) | 2004-12-27 |
Family
ID=60519227
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3834386/23A SU1272628A1 (en) | 1985-01-04 | 1985-01-04 | MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1272628A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2505455C2 (en) * | 2009-04-06 | 2014-01-27 | Эйрбас Оперэйшнз Гмбх | Aircraft or airship wing including moving streamlined body |
-
1985
- 1985-01-04 SU SU3834386/23A patent/SU1272628A1/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2505455C2 (en) * | 2009-04-06 | 2014-01-27 | Эйрбас Оперэйшнз Гмбх | Aircraft or airship wing including moving streamlined body |
US9242719B2 (en) | 2009-04-06 | 2016-01-26 | Airbus Operations Gmbh | Wing of an aircraft or spacecraft, comprising a mobile flow body |
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