SU1489104A1 - ENGINE MOUNTING SYSTEM ON THE AIRCRAFT - Google Patents
ENGINE MOUNTING SYSTEM ON THE AIRCRAFTInfo
- 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
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.
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)
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 |
-
1987
- 1987-09-03 SU SU4303077/23A patent/SU1489104A1/en active
Cited By (1)
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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