SU1394636A1 - ENGINE MOUNTING KNOT - Google Patents
ENGINE MOUNTING KNOTInfo
- Publication number
- SU1394636A1 SU1394636A1 SU4129032/23A SU4129032A SU1394636A1 SU 1394636 A1 SU1394636 A1 SU 1394636A1 SU 4129032/23 A SU4129032/23 A SU 4129032/23A SU 4129032 A SU4129032 A SU 4129032A SU 1394636 A1 SU1394636 A1 SU 1394636A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- engine mounting
- mounting belt
- mounting knot
- belt consisting
- knot
- Prior art date
Links
Landscapes
- Body Structure For Vehicles (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
Узел крепления двигателя, содержащий передний пояс крепления, состоящий из двух основных опор, и задний пояс крепления, состоящий из дополнительных опор в виде подкосов, один из которых выполнен жестким, отличающийся тем, что, с целью повышения надежности путем уменьшения воздействия на двигатель крутящих и изгибающих моментов, в заднем поясе крепления второй подкос выполнен телескопическим с пружиной предварительного сжатия внутри.An engine mount containing a front mounting belt consisting of two main supports and a rear mounting belt consisting of additional supports in the form of struts, one of which is rigid, characterized in that, in order to increase reliability by reducing the impact bending moments, in the rear girdle, the second strut is made telescopic with a pre-compression spring inside.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4129032/23A SU1394636A1 (en) | 1986-10-03 | 1986-10-03 | ENGINE MOUNTING KNOT |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4129032/23A SU1394636A1 (en) | 1986-10-03 | 1986-10-03 | ENGINE MOUNTING KNOT |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1394636A1 true SU1394636A1 (en) | 2004-07-27 |
Family
ID=60535534
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4129032/23A SU1394636A1 (en) | 1986-10-03 | 1986-10-03 | ENGINE MOUNTING KNOT |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1394636A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2483004C2 (en) * | 2008-01-25 | 2013-05-27 | Снекма | Attachment of multistage turbojet to aircraft |
RU2483002C2 (en) * | 2008-01-23 | 2013-05-27 | Снекма | Aircraft power plant attachment to aircraft structural element |
RU2542730C2 (en) * | 2009-11-17 | 2015-02-27 | Снекма | Fitting of agb at turbojet housing blower mid housing |
RU2635023C2 (en) * | 2012-09-13 | 2017-11-08 | Снекма | Pylon for engine installation on aircraft structure |
-
1986
- 1986-10-03 SU SU4129032/23A patent/SU1394636A1/en active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2483002C2 (en) * | 2008-01-23 | 2013-05-27 | Снекма | Aircraft power plant attachment to aircraft structural element |
RU2483004C2 (en) * | 2008-01-25 | 2013-05-27 | Снекма | Attachment of multistage turbojet to aircraft |
RU2542730C2 (en) * | 2009-11-17 | 2015-02-27 | Снекма | Fitting of agb at turbojet housing blower mid housing |
RU2635023C2 (en) * | 2012-09-13 | 2017-11-08 | Снекма | Pylon for engine installation on aircraft structure |
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