RU2005129231A - DEVICE FOR MOUNTING THE ENGINE TO THE HOUSING - Google Patents

DEVICE FOR MOUNTING THE ENGINE TO THE HOUSING Download PDF

Info

Publication number
RU2005129231A
RU2005129231A RU2005129231/11A RU2005129231A RU2005129231A RU 2005129231 A RU2005129231 A RU 2005129231A RU 2005129231/11 A RU2005129231/11 A RU 2005129231/11A RU 2005129231 A RU2005129231 A RU 2005129231A RU 2005129231 A RU2005129231 A RU 2005129231A
Authority
RU
Russia
Prior art keywords
engine
housing
spherical
mounting
attached
Prior art date
Application number
RU2005129231/11A
Other languages
Russian (ru)
Other versions
RU2309086C2 (en
Inventor
Николай В чеславович Шлейников (RU)
Николай Вячеславович Шлейников
В чеслав Константинович Захаренков (RU)
Вячеслав Константинович Захаренков
Владимир Николаевич Никулин (RU)
Владимир Николаевич Никулин
Федор Данилович Тихонов (RU)
Федор Данилович Тихонов
Original Assignee
Открытое акционерное общество "Калужское опытное бюро моторостроени " (ОАО "КОБМ") (RU)
Открытое акционерное общество "Калужское опытное бюро моторостроения" (ОАО "КОБМ")
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 Открытое акционерное общество "Калужское опытное бюро моторостроени " (ОАО "КОБМ") (RU), Открытое акционерное общество "Калужское опытное бюро моторостроения" (ОАО "КОБМ") filed Critical Открытое акционерное общество "Калужское опытное бюро моторостроени " (ОАО "КОБМ") (RU)
Priority to RU2005129231/11A priority Critical patent/RU2309086C2/en
Publication of RU2005129231A publication Critical patent/RU2005129231A/en
Application granted granted Critical
Publication of RU2309086C2 publication Critical patent/RU2309086C2/en

Links

Landscapes

  • Pivots And Pivotal Connections (AREA)

Claims (2)

1. Устройство крепления двигателя к корпусу, преимущественно летательного аппарата, содержащее две, разнесенные вдоль оси двигателя, сферические опоры, прикрепленные к двигателю и к корпусу, а каждая из сферических опор имеет четыре концентрических, сопряженных попарно, сферических поверхности, при этом одна сферическая поверхность из каждой пары размещена на детали сферической опоры, прикрепленной к двигателю, а другая на детали, прикрепленной к корпусу, отличающееся тем, что одна из сферических опор прикреплена к двигателю неподвижно, а вторая подвижно, телескопически, с возможностью осевого перемещения двигателя относительно корпуса.1. The device for mounting the engine to the body, mainly the aircraft, containing two spherical bearings spaced along the axis of the engine attached to the engine and the body, and each of the spherical bearings has four concentric, paired, spherical surfaces, with one spherical surface of each pair is placed on a part of a spherical support attached to the engine, and the other on a part attached to the housing, characterized in that one of the spherical supports is fixed to the engine, and the second is movable, telescopically, with the possibility of axial movement of the engine relative to the housing. 2. Устройство по п.1, отличающееся тем, что одна из сферических опор прикреплена к корпусу подвижно, с возможностью радиального перемещения двигателя относительно корпуса, и зафиксирована радиально с помощью подвижных, управляемых по специальной программе, фиксаторов.2. The device according to claim 1, characterized in that one of the spherical bearings is mounted to the housing movably, with the possibility of radial movement of the engine relative to the housing, and is fixed radially using movable, controlled by a special program, clamps.
RU2005129231/11A 2005-09-19 2005-09-19 Device for securing the engine to flying vehicle body RU2309086C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005129231/11A RU2309086C2 (en) 2005-09-19 2005-09-19 Device for securing the engine to flying vehicle body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005129231/11A RU2309086C2 (en) 2005-09-19 2005-09-19 Device for securing the engine to flying vehicle body

Publications (2)

Publication Number Publication Date
RU2005129231A true RU2005129231A (en) 2007-03-27
RU2309086C2 RU2309086C2 (en) 2007-10-27

Family

ID=37998889

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005129231/11A RU2309086C2 (en) 2005-09-19 2005-09-19 Device for securing the engine to flying vehicle body

Country Status (1)

Country Link
RU (1) RU2309086C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914907B1 (en) * 2007-04-16 2009-10-30 Snecma Sa SOFT SUSPENSION WITH COMB FOR TURBOMOTEUR
FR2941673B1 (en) * 2009-02-04 2011-01-14 Aircelle Sa SUSPENSION ASSEMBLY FOR AIRCRAFT TURBOJET ENGINE
RU2573628C2 (en) * 2014-02-04 2016-01-20 Открытое акционерное общество "Конструкторское бюро химавтоматики" Liquid-propellant rocket engine units attachment

Also Published As

Publication number Publication date
RU2309086C2 (en) 2007-10-27

Similar Documents

Publication Publication Date Title
RU2007127900A (en) CLAMPING DEVICE FOR GRINDING SPINDLE ROTOR AND PART IN THE TYPE OF ROTATION OF THE ROTATION FOR CLAMPING DEVICE
RU2008103103A (en) DEVICE FOR PISTON POSITION IN CYLINDER, ASSEMBLY CONTAINING CYLINDER, PISTON AND SUCH DEVICE, AND AIRCRAFT ENGINE CONTAINING SUCH ASSEMBLY
NL1022788A1 (en) Decoupling device for bearing a shaft on a basic body as well as a radially corrugated spring.
RU2005129231A (en) DEVICE FOR MOUNTING THE ENGINE TO THE HOUSING
RU2010103446A (en) FIXING AT THREE POINTS OF FIRING BURNER ELECTRODES
RU2007146465A (en) ROTOR SUPPORT FOR BALANCING MACHINE
RU2005137888A (en) PIPELINE SUPPORT
CN203945135U (en) Nut machine frame
JP2016095525A5 (en)
RU2009109511A (en) DEVICE FOR FASTENING AND FIXING OF PIECES WITH BASING OF THEM ON THE CENTRAL AXIAL HOLE
RU2008123035A (en) NUTROMER
RU2004114663A (en) DEVICE FOR TESTING CYLINDRICAL ELBOWS
RU2006111894A (en) Cone Eccentric Crusher
RU2004112094A (en) THREADED CONNECTION OF AIRCRAFT HOUSING COMPARTMENTS
RU2005103046A (en) DEVICE FOR ATTACHING DISC SAWS TO THE SHAFT
RU2004131340A (en) METHOD FOR SURFACE PLASTIC DEFORMATION BY COVERING RINGS
SU1580157A1 (en) Arrangement for moving interferometer mirror
RU2007116576A (en) SPRING ENGINE
RU2006143693A (en) DISC-VANE ENGINE
GB0329292D0 (en) Rotating support
RU2005139645A (en) PILLOW PLATFORM
RU2005112107A (en) DEVICE FOR APPLICATION OF ULTRASONIC VIBRATIONS ON THE PREPARATION DURING THREADING
RU2006113445A (en) INTERNAL INSPECTION APPLIANCE WITH CONTROLLED MOVEMENT SPEED
RU2005123447A (en) VERTICAL ROTOR DAMPER
RU97101537A (en) ELASTIC DAMPING BRACKET

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20090920