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SU369053A1 - MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT - Google Patents

MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT

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Publication number
SU369053A1
SU369053A1 SU1668661/23A SU1668661A SU369053A1 SU 369053 A1 SU369053 A1 SU 369053A1 SU 1668661/23 A SU1668661/23 A SU 1668661/23A SU 1668661 A SU1668661 A SU 1668661A SU 369053 A1 SU369053 A1 SU 369053A1
Authority
SU
USSR - Soviet Union
Prior art keywords
carriage
extension
rail
link
flap
Prior art date
Application number
SU1668661/23A
Other languages
Russian (ru)
Inventor
В.Б. Горохов
Г.В. Новожилов
Р.И. Рокитянский
Е.И. Санков
Ю.Г. Чернов
Original Assignee
В.Б. Горохов
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 В.Б. Горохов filed Critical В.Б. Горохов
Priority to SU1668661/23A priority Critical patent/SU369053A1/en
Application granted granted Critical
Publication of SU369053A1 publication Critical patent/SU369053A1/en

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Abstract

Механизм управления трехщелевым закрылком летательного аппарата, содержащий рельс выдвижения основного звена закрылка, каретку выдвижения основного звена, каретку выдвижения дефлектора, устройство выдвижения хвостового звена закрылка и межзвеньевой механизм, отличающийся тем, что, с целью улучшения аэродинамических характеристик крыла при выдвижении закрылка, рельс выдвижения основного звена закреплен неподвижно на крыле, каретка выдвижения основного звена закреплена на основном звене и имеет возможность перемещения по рельсу, дефлектор имеет закрепленный на нем рельс перемещения каретки выдвижения дефлектора, закрепленной неподвижно на основном звене, основное звено имеет рельс выдвижения хвостового звена посредством прикрепленной к нему каретки, межзвеньевой механизм снабжен механическим приводом от рельса выдвижения дефлектора, сочлененного с управляющей кареткой, имеющей возможность перемещения по рельсу выдвижения основного звена, на котором выполнен упор для фиксации управляющей каретки при выдвижении звеньев.The control mechanism of a three-slot flap of an aircraft, comprising a main flap extension rail, a main link extension carriage, a deflector extension carriage, a flap tail section extension device, and an intersink mechanism, characterized in that, in order to improve the wing aerodynamic characteristics when the flap extends, the main rail extension the link is fixed on the wing, the carriage extending the main link is fixed on the main link and has the ability to move along the rail, de the lecturer has a rail mounted on it moving the carriage for extending the deflector fixedly mounted on the main link, the main link has the rail extending the tail link by means of the carriage attached to it extension of the main link, on which an emphasis is made for fixing the control carriage when extending the links.

SU1668661/23A 1971-06-07 1971-06-07 MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT SU369053A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1668661/23A SU369053A1 (en) 1971-06-07 1971-06-07 MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1668661/23A SU369053A1 (en) 1971-06-07 1971-06-07 MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT

Publications (1)

Publication Number Publication Date
SU369053A1 true SU369053A1 (en) 2004-11-20

Family

ID=60514710

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1668661/23A SU369053A1 (en) 1971-06-07 1971-06-07 MECHANISM OF MANAGEMENT OF THREE-CHAIN FLAP OF THE AIRCRAFT

Country Status (1)

Country Link
SU (1) SU369053A1 (en)

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