SU1828026A1 - System of attachment of engine to flying vehicle - Google Patents

System of attachment of engine to flying vehicle

Info

Publication number
SU1828026A1
SU1828026A1 SU4870623/23A SU4870623A SU1828026A1 SU 1828026 A1 SU1828026 A1 SU 1828026A1 SU 4870623/23 A SU4870623/23 A SU 4870623/23A SU 4870623 A SU4870623 A SU 4870623A SU 1828026 A1 SU1828026 A1 SU 1828026A1
Authority
SU
USSR - Soviet Union
Prior art keywords
engine
rods
flying vehicle
attachment
enhanced
Prior art date
Application number
SU4870623/23A
Other languages
Russian (ru)
Inventor
В.Ф. Гордеев
Original Assignee
Московский машиностроительный завод им.С.В.Ильюшина
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 Московский машиностроительный завод им.С.В.Ильюшина filed Critical Московский машиностроительный завод им.С.В.Ильюшина
Priority to SU4870623/23A priority Critical patent/SU1828026A1/en
Application granted granted Critical
Publication of SU1828026A1 publication Critical patent/SU1828026A1/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

  • Body Structure For Vehicles (AREA)

Abstract

FIELD: aeronautical engineering. SUBSTANCE: system has engine 1 secured on structural member 2 of flying vehicle by means of front suspension band which includes rods 3, rear suspension unit which includes trots 5 and brackets, diverging rods 7 for transmission of thrust articulated to units 4. Axes of rods 3 and 5 lie in planes of front and rear suspensions, respectively, which are perpendicular to longitudinal axis 16 of engine. EFFECT: enhanced reliability, increased service life of engine and enhanced economical efficiency. 10 dwg
SU4870623/23A 1990-10-02 1990-10-02 System of attachment of engine to flying vehicle SU1828026A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4870623/23A SU1828026A1 (en) 1990-10-02 1990-10-02 System of attachment of engine to flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4870623/23A SU1828026A1 (en) 1990-10-02 1990-10-02 System of attachment of engine to flying vehicle

Publications (1)

Publication Number Publication Date
SU1828026A1 true SU1828026A1 (en) 1996-11-10

Family

ID=60541162

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4870623/23A SU1828026A1 (en) 1990-10-02 1990-10-02 System of attachment of engine to flying vehicle

Country Status (1)

Country Link
SU (1) SU1828026A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2606524C2 (en) * 2011-09-01 2017-01-10 Снекма Assembly formed by gas turbine engine and system for its attachment to aircraft structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2606524C2 (en) * 2011-09-01 2017-01-10 Снекма Assembly formed by gas turbine engine and system for its attachment to aircraft structure

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