RU2008115362A - UNMANNED AERIAL VEHICLE - Google Patents
UNMANNED AERIAL VEHICLE Download PDFInfo
- Publication number
- RU2008115362A RU2008115362A RU2008115362/11A RU2008115362A RU2008115362A RU 2008115362 A RU2008115362 A RU 2008115362A RU 2008115362/11 A RU2008115362/11 A RU 2008115362/11A RU 2008115362 A RU2008115362 A RU 2008115362A RU 2008115362 A RU2008115362 A RU 2008115362A
- Authority
- RU
- Russia
- Prior art keywords
- fuselage
- launch
- engine
- launch accelerator
- accelerator
- Prior art date
Links
- 238000000926 separation method Methods 0.000 claims abstract 6
- 239000000725 suspension Substances 0.000 claims abstract 2
Landscapes
- Elimination Of Static Electricity (AREA)
Abstract
1. Беспилотный летательный аппарат, имеющий маршевый двигатель, расположенный снаружи фюзеляжа в его нижней части на пилоне, стартовый ускоритель, соединенный с фюзеляжем устройством отделения с пиромеханизмом, а также гаргрот, расположенный в нижней части фюзеляжа, отличающийся тем, что стартовый ускоритель расположен снаружи фюзеляжа на подвеске за маршевым двигателем по направлению полета. ! 2. Летательный аппарат по п.1, отличающийся тем, что гаргрот в задней части имеет продольные направляющие, а устройство отделения содержит передний силовой кронштейн, расположенный на стартовом ускорителе и закрепленный к пилону маршевого двигателя с помощью пиромеханизма крепления и отделения, и задние кронштейны, жестко закрепленные на стартовом ускорителе и выполненные с возможностью скольжения в продольных направляющих гаргрота.1. An unmanned aerial vehicle having a mid-flight engine located outside the fuselage in its lower part on the pylon, a launch accelerator connected to the fuselage with a pyromechanical separation device, and a garrgot located in the lower part of the fuselage, characterized in that the launch accelerator is located outside the fuselage on the suspension behind the marching engine in the direction of flight. ! 2. The aircraft according to claim 1, characterized in that the gargrot in the rear has longitudinal guides, and the separation device contains a front power bracket located on the launch accelerator and mounted to the main engine pylon using a pyromechanism of fastening and separation, and rear brackets, rigidly mounted on the launch accelerator and made with the possibility of sliding in the longitudinal guides of the gargrot.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008115362/11A RU2008115362A (en) | 2008-04-23 | 2008-04-23 | UNMANNED AERIAL VEHICLE |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008115362/11A RU2008115362A (en) | 2008-04-23 | 2008-04-23 | UNMANNED AERIAL VEHICLE |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2008115362A true RU2008115362A (en) | 2009-10-27 |
Family
ID=41352546
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008115362/11A RU2008115362A (en) | 2008-04-23 | 2008-04-23 | UNMANNED AERIAL VEHICLE |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2008115362A (en) |
-
2008
- 2008-04-23 RU RU2008115362/11A patent/RU2008115362A/en unknown
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