SU849694A1 - Device for attachment of double-flow turbojet engine - Google Patents

Device for attachment of double-flow turbojet engine

Info

Publication number
SU849694A1
SU849694A1 SU2894569/23A SU2894569A SU849694A1 SU 849694 A1 SU849694 A1 SU 849694A1 SU 2894569/23 A SU2894569/23 A SU 2894569/23A SU 2894569 A SU2894569 A SU 2894569A SU 849694 A1 SU849694 A1 SU 849694A1
Authority
SU
USSR - Soviet Union
Prior art keywords
rod
articulated
gas generator
suspension
attachment
Prior art date
Application number
SU2894569/23A
Other languages
Russian (ru)
Inventor
А.А. Бобух
Г.М. Горелов
В.Ф. Гордеев
С.В. Михайлов
А.П. Сергеев
Г.А. Тетюшин
П.И. Чернышев
В.А. Чистяков
Л.И. Фридман
Original Assignee
А.А. Бобух
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 А.А. Бобух filed Critical А.А. Бобух
Priority to SU2894569/23A priority Critical patent/SU849694A1/en
Application granted granted Critical
Publication of SU849694A1 publication Critical patent/SU849694A1/en

Links

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: device for attachment of double-flow turbojet engine mounted on aircraft pylon has gas generator with front and rear supports of rotors, inner and outer housings of rotor center support, front and rear bands of rod suspension whose rods are articulated on pylons at one end and on outer envelope of gas generator at other end. Device has inclined thrust transfer rod whose rear end is articulated on bracket of pylon in rear band of suspension. Front end of rod is articulated on inner ring of outer housing of center support. Axis of rod passes through point of intersection of gas generator axis and plane of front band of suspension. EFFECT: increased service life, enhanced economical efficiency and reduced mass of engine.
SU2894569/23A 1980-03-12 1980-03-12 Device for attachment of double-flow turbojet engine SU849694A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2894569/23A SU849694A1 (en) 1980-03-12 1980-03-12 Device for attachment of double-flow turbojet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2894569/23A SU849694A1 (en) 1980-03-12 1980-03-12 Device for attachment of double-flow turbojet engine

Publications (1)

Publication Number Publication Date
SU849694A1 true SU849694A1 (en) 1996-09-20

Family

ID=60523685

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2894569/23A SU849694A1 (en) 1980-03-12 1980-03-12 Device for attachment of double-flow turbojet engine

Country Status (1)

Country Link
SU (1) SU849694A1 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7313920B2 (en) 2003-12-11 2008-01-01 Rolls-Royce Plc Aircraft engine mounting
RU2566835C2 (en) * 2010-02-26 2015-10-27 Снекма Device for reduction of noise of interaction of jet/strut in turbojet engines
RU2682206C2 (en) * 2013-08-28 2019-03-15 Сафран Эркрафт Энджинз Isostatic suspension of a turbojet by rear double support
RU2399558C9 (en) * 2005-10-03 2019-12-30 Эрбюс Франс Aircraft turbojet engine attachment strut
RU199280U1 (en) * 2019-03-07 2020-08-25 Публичное акционерное общество "МОТОР СИЧ" TURBO-SCREW ENGINE SUSPENSION HOUSING
CN112678193A (en) * 2020-12-30 2021-04-20 中国航发沈阳发动机研究所 Aeroengine pull rod circumferential adjusting mechanism
RU2804492C2 (en) * 2019-04-26 2023-10-02 Сафран Насель Nacelle air intake and nacelle containing such air intake

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7313920B2 (en) 2003-12-11 2008-01-01 Rolls-Royce Plc Aircraft engine mounting
RU2399558C9 (en) * 2005-10-03 2019-12-30 Эрбюс Франс Aircraft turbojet engine attachment strut
RU2566835C2 (en) * 2010-02-26 2015-10-27 Снекма Device for reduction of noise of interaction of jet/strut in turbojet engines
RU2682206C2 (en) * 2013-08-28 2019-03-15 Сафран Эркрафт Энджинз Isostatic suspension of a turbojet by rear double support
RU199280U1 (en) * 2019-03-07 2020-08-25 Публичное акционерное общество "МОТОР СИЧ" TURBO-SCREW ENGINE SUSPENSION HOUSING
RU2804492C2 (en) * 2019-04-26 2023-10-02 Сафран Насель Nacelle air intake and nacelle containing such air intake
CN112678193A (en) * 2020-12-30 2021-04-20 中国航发沈阳发动机研究所 Aeroengine pull rod circumferential adjusting mechanism
CN112678193B (en) * 2020-12-30 2023-06-02 中国航发沈阳发动机研究所 Circumferential adjusting mechanism for pull rod of aero-engine

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