SU1394636A1 - ENGINE MOUNTING KNOT - Google Patents

ENGINE MOUNTING KNOT

Info

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
Application number
SU4129032/23A
Other languages
Russian (ru)
Inventor
В.С. Вигант
В.Я. Сигайло
Original Assignee
В.С. Вигант
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.С. Вигант filed Critical В.С. Вигант
Priority to SU4129032/23A priority Critical patent/SU1394636A1/en
Application granted granted Critical
Publication of SU1394636A1 publication Critical patent/SU1394636A1/en

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.

SU4129032/23A 1986-10-03 1986-10-03 ENGINE MOUNTING KNOT SU1394636A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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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