SU801441A1 - ROD OF THE ENGINE ENGINE GONDOLA - Google Patents
ROD OF THE ENGINE ENGINE GONDOLAInfo
- 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
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.
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)
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 |
-
1979
- 1979-10-02 SU SU2824312/23A patent/SU801441A1/en active
Cited By (2)
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 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2613688B1 (en) | PYLONE FOR AIRPLANE | |
ATE23500T1 (en) | AIRCRAFT EQUIPPED WITH A MULTI-DECKER LIFT STRUCTURE. | |
DE69108960D1 (en) | Main gearbox of a rotary wing aircraft with an emergency lubrication device. | |
BR8107210A (en) | SET OF TAPES ADAPTED TO BE FORMED IN A LACO | |
US2420433A (en) | Airplane wing of variable area construction | |
US2398601A (en) | Aircraft control | |
SU801441A1 (en) | ROD OF THE ENGINE ENGINE GONDOLA | |
US2385392A (en) | Crewless glider | |
NO147177C (en) | HELICOPTER. | |
CN114013629A (en) | Passive wing extending structure | |
SE8106271L (en) | AIRPLANE WITH ARRANGEMENTS FOR ASSEMBLY OF A PROBE | |
ATE86931T1 (en) | VTOL. | |
FR2227990A1 (en) | Pivoted wing aircraft with pilot operated control - transfer wing load to undercarriage on take-off | |
CN219506247U (en) | Unmanned aerial vehicle flies fast and rises to fall device | |
GB509161A (en) | Improvements in or relating to launching means for aircraft | |
Schweiger et al. | Design of a forward swept wing fighter aircraft | |
GB1535785A (en) | Wing leading edge flaps | |
ES8300168A1 (en) | Improvements introduced in the systems of driving for failure of rods, with device of self-insurance or protection of its positions of dead point. (Machine-translation by Google Translate, not legally binding) | |
DESTUYNDER | Recent progress in active controls applied to flutter suppressors | |
RU1818277C (en) | Catapult airplane | |
ES2068007T3 (en) | AN ANTIFREEZE DEVICE FOR AN AIRPLANE WING. | |
SU1804039A1 (en) | Device for controlling flaps | |
Zinberg | A low-cost forward fairing for the Bell Long Ranger Helicopter | |
FR2608450A3 (en) | Throwing game | |
SU1256353A1 (en) | AIRPLANE ELECTRONIC CONTROL SYSTEM |