RU2008110343A - UNMANNED AERIAL VEHICLE - Google Patents
UNMANNED AERIAL VEHICLE Download PDFInfo
- Publication number
- RU2008110343A RU2008110343A RU2008110343/11A RU2008110343A RU2008110343A RU 2008110343 A RU2008110343 A RU 2008110343A RU 2008110343/11 A RU2008110343/11 A RU 2008110343/11A RU 2008110343 A RU2008110343 A RU 2008110343A RU 2008110343 A RU2008110343 A RU 2008110343A
- Authority
- RU
- Russia
- Prior art keywords
- aerial vehicle
- unmanned aerial
- engine
- vehicle according
- accelerating
- Prior art date
Links
Landscapes
- Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
1. Беспилотный летательный аппарат, имеющий маршевый двигатель, расположенный снаружи фюзеляжа на подвеске, отличающийся тем, что содержит разгонный двигатель, расположенный снаружи фюзеляжа на подвеске за маршевым двигателем по направлению полета. ! 2. Беспилотный летательный аппарат по п.1, отличающийся тем, что разгонный двигатель выполнен с возможностью сброса в полете. ! 3. Беспилотный летательный аппарат по п.1 или 2, отличающийся тем, что разгонный двигатель снабжен передним и задним, выполненным с возможностью сброса, обтекателями. ! 4. Беспилотный летательный аппарат по п.1 или 2, отличающийся тем, что разгонный двигатель снабжен теплозащитным экраном, расположенным между ним и маршевым двигателем. ! 5. Беспилотный летательный аппарат по п.3, отличающийся тем, что разгонный двигатель снабжен теплозащитным экраном, расположенным между ним и маршевым двигателем.1. An unmanned aerial vehicle having a marching engine located outside the fuselage on the suspension, characterized in that it contains an accelerating engine located outside the fuselage on the suspension behind the marching engine in the direction of flight. ! 2. The unmanned aerial vehicle according to claim 1, characterized in that the accelerating engine is configured to reset in flight. ! 3. The unmanned aerial vehicle according to claim 1 or 2, characterized in that the accelerating engine is equipped with front and rear, resettable, cowls. ! 4. The unmanned aerial vehicle according to claim 1 or 2, characterized in that the accelerating engine is equipped with a heat shield located between it and the main engine. ! 5. The unmanned aerial vehicle according to claim 3, characterized in that the accelerating engine is equipped with a heat shield located between it and the main engine.
Claims (5)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008110343/11A RU2371359C1 (en) | 2008-03-20 | 2008-03-20 | Pilotless aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2008110343/11A RU2371359C1 (en) | 2008-03-20 | 2008-03-20 | Pilotless aircraft |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2008110343A true RU2008110343A (en) | 2009-09-27 |
RU2371359C1 RU2371359C1 (en) | 2009-10-27 |
Family
ID=41168933
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2008110343/11A RU2371359C1 (en) | 2008-03-20 | 2008-03-20 | Pilotless aircraft |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2371359C1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114248946A (en) * | 2020-09-22 | 2022-03-29 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle helps and separating mechanism |
-
2008
- 2008-03-20 RU RU2008110343/11A patent/RU2371359C1/en active IP Right Revival
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114248946A (en) * | 2020-09-22 | 2022-03-29 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle helps and separating mechanism |
Also Published As
Publication number | Publication date |
---|---|
RU2371359C1 (en) | 2009-10-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20160321 |
|
NF4A | Reinstatement of patent |
Effective date: 20171016 |