SU1489104A1 - ENGINE MOUNTING SYSTEM ON THE AIRCRAFT - Google Patents

ENGINE MOUNTING SYSTEM ON THE AIRCRAFT

Info

Publication number
SU1489104A1
SU1489104A1 SU4303077/23A SU4303077A SU1489104A1 SU 1489104 A1 SU1489104 A1 SU 1489104A1 SU 4303077/23 A SU4303077/23 A SU 4303077/23A SU 4303077 A SU4303077 A SU 4303077A SU 1489104 A1 SU1489104 A1 SU 1489104A1
Authority
SU
USSR - Soviet Union
Prior art keywords
pylon
struts
front suspension
aircraft
insert
Prior art date
Application number
SU4303077/23A
Other languages
Russian (ru)
Inventor
В.Ф. Гордеев
Original Assignee
В.Ф. Гордеев
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.Ф. Гордеев filed Critical В.Ф. Гордеев
Priority to SU4303077/23A priority Critical patent/SU1489104A1/en
Application granted granted Critical
Publication of SU1489104A1 publication Critical patent/SU1489104A1/en

Links

Abstract

Система крепления двигателя на летательном аппарате, содержащая закрепленный на крыльевых кронштейнах пилон, переднюю подвеску двигателя, состоящую из подкосов, объединенных узлом крепления кронштейна пилона и заднюю подвеску, выполненную в виде подкосов, закрепленных на пилоне, отличающаяся тем, что, с целью снижения массы и повышения жесткости системы, подкосы задней подвески двигателя закреплены на крыльевых кронштейнах пилона, а узел крепления передней подвески выполнен в виде жестко соединенных между собой конической втулки, закрепленной на кронштейне пилона, и вкладыша, соединенного шарнирно с подкосами передней подвески, причем оси этих подкосов пересекаются внутри конического участка вкладыша в точке, лежащей в плоскости несущей балки пилона.An engine mount system on an aircraft containing a pylon fixed to the wing brackets, an engine front suspension consisting of struts connected by a pylon bracket fixing unit and a rear suspension made in the form of struts fixed on the pylon, characterized in that increase the rigidity of the system, the struts of the rear engine mount mounted on the pylon wing brackets, and the mount of the front suspension is made in the form of rigidly interconnected conical bushings eplennoy pylon bracket, and the insert is pivotally coupled to the front suspension struts, the axes of the struts intersect in the conical portion of the insert at a point lying in the plane of the carrier girder pylon.

SU4303077/23A 1987-09-03 1987-09-03 ENGINE MOUNTING SYSTEM ON THE AIRCRAFT SU1489104A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4303077/23A SU1489104A1 (en) 1987-09-03 1987-09-03 ENGINE MOUNTING SYSTEM ON THE AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4303077/23A SU1489104A1 (en) 1987-09-03 1987-09-03 ENGINE MOUNTING SYSTEM ON THE AIRCRAFT

Publications (1)

Publication Number Publication Date
SU1489104A1 true SU1489104A1 (en) 2005-02-20

Family

ID=60528018

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4303077/23A SU1489104A1 (en) 1987-09-03 1987-09-03 ENGINE MOUNTING SYSTEM ON THE AIRCRAFT

Country Status (1)

Country Link
SU (1) SU1489104A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2583243C2 (en) * 2010-06-14 2016-05-10 Снекма Gas turbine engine mounted on pylon of aircraft fuselage by apparatus ensuring safety of suspension

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2583243C2 (en) * 2010-06-14 2016-05-10 Снекма Gas turbine engine mounted on pylon of aircraft fuselage by apparatus ensuring safety of suspension

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