SU460694A1 - DEVICE FOR INSTALLATION OF A TURBO-REACTIVE ENGINE ON A PLANE - Google Patents

DEVICE FOR INSTALLATION OF A TURBO-REACTIVE ENGINE ON A PLANE

Info

Publication number
SU460694A1
SU460694A1 SU1932310/23A SU1932310A SU460694A1 SU 460694 A1 SU460694 A1 SU 460694A1 SU 1932310/23 A SU1932310/23 A SU 1932310/23A SU 1932310 A SU1932310 A SU 1932310A SU 460694 A1 SU460694 A1 SU 460694A1
Authority
SU
USSR - Soviet Union
Prior art keywords
engine
turbo
installation
plane
pylon
Prior art date
Application number
SU1932310/23A
Other languages
Russian (ru)
Inventor
М.С. Неймарк
В.М. Душский
А.П. Карпачев
С.П. Булкин
Original Assignee
М.С. Неймарк
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 М.С. Неймарк filed Critical М.С. Неймарк
Priority to SU1932310/23A priority Critical patent/SU460694A1/en
Application granted granted Critical
Publication of SU460694A1 publication Critical patent/SU460694A1/en

Links

Abstract

Устройство для установки турбореактивного двигателя на самолете, содержащее передний узел крепления двигателя к пилону, выполненный в виде шарнира и задний в виде шарнирно прикрепленного к двигателю и пилону силового привода, отличающееся тем, что, с целью исключения помпажа на входе в двигатель путем автоматического разворота его вдоль потока, оно снабжено следящей системой, включающей установленные на двигателе в вертикальной плоскости симметрии датчики давления, подключенные к блоку сравнения сигналов датчиков, и усилитель сигнала их рассогласования, управляющий силовым приводом.A device for installing a turbojet engine on an airplane, containing a front engine mount to a pylon, made in the form of a hinge and rear in the form of a power drive pivotally attached to the engine and the pylon, in order to eliminate the surge at the engine entrance by automatically turning it along the stream, it is equipped with a tracking system that includes pressure sensors mounted on the engine in a vertical plane of symmetry, connected to a sensor signal comparison unit, and a signal amplifier their mismatch, managing the power drive.

SU1932310/23A 1973-06-22 1973-06-22 DEVICE FOR INSTALLATION OF A TURBO-REACTIVE ENGINE ON A PLANE SU460694A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1932310/23A SU460694A1 (en) 1973-06-22 1973-06-22 DEVICE FOR INSTALLATION OF A TURBO-REACTIVE ENGINE ON A PLANE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1932310/23A SU460694A1 (en) 1973-06-22 1973-06-22 DEVICE FOR INSTALLATION OF A TURBO-REACTIVE ENGINE ON A PLANE

Publications (1)

Publication Number Publication Date
SU460694A1 true SU460694A1 (en) 2004-11-20

Family

ID=60520601

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1932310/23A SU460694A1 (en) 1973-06-22 1973-06-22 DEVICE FOR INSTALLATION OF A TURBO-REACTIVE ENGINE ON A PLANE

Country Status (1)

Country Link
SU (1) SU460694A1 (en)

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