SU1272628A1 - MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT - Google Patents

MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT

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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
Application number
SU3834386/23A
Other languages
Russian (ru)
Inventor
И.Л. Сосульников
И.Я. Катырев
Original Assignee
И.Л. Сосульников
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 И.Л. Сосульников filed Critical И.Л. Сосульников
Priority to SU3834386/23A priority Critical patent/SU1272628A1/en
Application granted granted Critical
Publication of SU1272628A1 publication Critical patent/SU1272628A1/en

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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.

SU3834386/23A 1985-01-04 1985-01-04 MANAGEMENT SYSTEM OF AERODYNAMIC SURFACE OF AIRCRAFT SU1272628A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (2)

* Cited by examiner, † Cited by third party
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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