SU801441A1 - ROD OF THE ENGINE ENGINE GONDOLA - Google Patents

ROD OF THE ENGINE ENGINE GONDOLA

Info

Publication number
SU801441A1
SU801441A1 SU2824312/23A SU2824312A SU801441A1 SU 801441 A1 SU801441 A1 SU 801441A1 SU 2824312/23 A SU2824312/23 A SU 2824312/23A SU 2824312 A SU2824312 A SU 2824312A SU 801441 A1 SU801441 A1 SU 801441A1
Authority
SU
USSR - Soviet Union
Prior art keywords
engine
hinged
rod
gondola
suspension
Prior art date
Application number
SU2824312/23A
Other languages
Russian (ru)
Inventor
И.В. Козлов
В.М. Шамонин
В.В. Зюскин
Е.А. Кашин
Г.В. Степанов
Original Assignee
И.В. Козлов
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 И.В. Козлов filed Critical И.В. Козлов
Priority to SU2824312/23A priority Critical patent/SU801441A1/en
Application granted granted Critical
Publication of SU801441A1 publication Critical patent/SU801441A1/en

Links

Landscapes

  • Flexible Shafts (AREA)

Abstract

Створка гондолы двигателя летательного аппарата, содержащая обшивку с профилями жесткости, соединенную с каркасом через узлы подвески, и фиксирующие штанги, шарнирно закрепленные одним концом на профилях жесткости по бокам створки, отличающаяся тем, что, с целью повышения надежности подвески и обеспечения удобства эксплуатации, фиксирующие штанги шарнирно закреплены на двигателе и выполнены в виде телескопически соединенных труб, состыкованных при помощи шариковых замков, снабженных муфтами и тросовым управлением, включающим тросы Боудена, соединенные с муфтами, и подпружиненную рукоятку управления замками, установленную с возможностью поступательного перемещения по направляющим, которые смонтированы на нижнем срезе внутренней поверхности обшивки.A wing of the engine nacelle of an aircraft comprising a casing with stiffness profiles connected to the frame through suspension assemblies and locking rods hinged at one end on the stiffness profiles on the sides of the flap, in order to increase the reliability of the suspension and ensure ease of operation the rods are hinged on the engine and are made in the form of telescopically connected pipes, joined with ball locks, fitted with clutches and cable controls, including cables B Uden connected with couplings and the spring-loaded locks the control lever mounted for translational movement along guides which are mounted on the lower surface of the cut inner cladding.

SU2824312/23A 1979-10-02 1979-10-02 ROD OF THE ENGINE ENGINE GONDOLA SU801441A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2824312/23A SU801441A1 (en) 1979-10-02 1979-10-02 ROD OF THE ENGINE ENGINE GONDOLA

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2824312/23A SU801441A1 (en) 1979-10-02 1979-10-02 ROD OF THE ENGINE ENGINE GONDOLA

Publications (1)

Publication Number Publication Date
SU801441A1 true SU801441A1 (en) 2004-12-10

Family

ID=60523631

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2824312/23A SU801441A1 (en) 1979-10-02 1979-10-02 ROD OF THE ENGINE ENGINE GONDOLA

Country Status (1)

Country Link
SU (1) SU801441A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2460674C2 (en) * 2007-03-26 2012-09-10 Эрсель Guide system with locking means for nacelle moving section
RU2462573C2 (en) * 2007-08-20 2012-09-27 Эрсель Fixing device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2460674C2 (en) * 2007-03-26 2012-09-10 Эрсель Guide system with locking means for nacelle moving section
RU2462573C2 (en) * 2007-08-20 2012-09-27 Эрсель Fixing device

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