RU1819816C - Device for securing the engine to wing pylon - Google Patents

Device for securing the engine to wing pylon

Info

Publication number
RU1819816C
RU1819816C SU4797043A RU1819816C RU 1819816 C RU1819816 C RU 1819816C SU 4797043 A SU4797043 A SU 4797043A RU 1819816 C RU1819816 C RU 1819816C
Authority
RU
Russia
Prior art keywords
engine
securing
wing pylon
damper
pylon
Prior art date
Application number
Other languages
Russian (ru)
Inventor
Ростислав Иванович Виноградов
Олег Инсафович Гайнутдинов
Альтаф Хуснимарзанович Каримов
Original Assignee
Рижский Краснознаменный Институт Инженеров Гражданской Авиации Им.Ленинского Комсомола
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 Рижский Краснознаменный Институт Инженеров Гражданской Авиации Им.Ленинского Комсомола filed Critical Рижский Краснознаменный Институт Инженеров Гражданской Авиации Им.Ленинского Комсомола
Priority to SU4797043 priority Critical patent/RU1819816C/en
Application granted granted Critical
Publication of RU1819816C publication Critical patent/RU1819816C/en

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Abstract

Изобретение относитс  к авиации, а именно к устройствам креплени  двигател  к пилону крыла. Цель изобретени  - повышение надежности путем уменьшени  динамических нагрузок. Дл  достижени  цели изобретени  передний узел креплени  двигател  1 снабжен подкосом 5, одним концом жестко закрепленным на полураме, а другим шарнирно закрепленным на передней раме кессона с возможностью поворота вокруг своей продольной оси Oi. Задний узел (феплени  снабжен горизонтальным демпфером и упругим элементом, установленным перпендикул рно демпферу и ротору двигател  1. 3 ил.FIELD OF THE INVENTION This invention relates to aviation, and in particular to devices for attaching an engine to a wing pylon. The purpose of the invention is to increase reliability by reducing dynamic loads. In order to achieve the object of the invention, the front engine mount 1 is provided with a strut 5, one end rigidly fixed to the half frame and the other pivotally mounted to the front frame of the box with the possibility of rotation around its longitudinal axis Oi. The rear assembly (the fencing is equipped with a horizontal damper and an elastic element mounted perpendicular to the damper and the rotor of the engine 1. 3 ill.

Description

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SU4797043 1990-02-26 1990-02-26 Device for securing the engine to wing pylon RU1819816C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4797043 RU1819816C (en) 1990-02-26 1990-02-26 Device for securing the engine to wing pylon

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4797043 RU1819816C (en) 1990-02-26 1990-02-26 Device for securing the engine to wing pylon

Publications (1)

Publication Number Publication Date
RU1819816C true RU1819816C (en) 1993-06-07

Family

ID=21499185

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4797043 RU1819816C (en) 1990-02-26 1990-02-26 Device for securing the engine to wing pylon

Country Status (1)

Country Link
RU (1) RU1819816C (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011087389A1 (en) * 2010-01-15 2011-07-21 Oleynov Gennady Aleksandrovitsch Device for modifying a counteracting force
RU2487820C2 (en) * 2007-06-25 2013-07-20 Снекма Gas turbine engine mount

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Самолет ИЛ-76, Инструкци ТО, М.: Машиностроение, 1979, гл. 42, с. 2. Альманах Истори развити авиации, Нью-Йорк-Лондон, под ред. Вилли Гансто- на, 1985, с. 58. *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2487820C2 (en) * 2007-06-25 2013-07-20 Снекма Gas turbine engine mount
WO2011087389A1 (en) * 2010-01-15 2011-07-21 Oleynov Gennady Aleksandrovitsch Device for modifying a counteracting force

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