FIELD: engines and pumps.
SUBSTANCE: propelling device comprises a body, a cone-shaped combustion chamber, an exhaust pipe, two spring valves between the exhaust pipe and the combustion chamber, a control unit with hydraulic outlets.
EFFECT: invention makes it possible to increase reliability of operation of a jet engine without speed reduction.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2014 |
|
RU2595217C2 |
| AIRCRAFT | 2015 |
|
RU2577742C2 |
| AIRCRAFT | 2016 |
|
RU2616095C1 |
| AIRCRAFT | 2015 |
|
RU2577750C1 |
| FLIGHT VEHICLE | 2008 |
|
RU2363625C1 |
| AIRCRAFT | 2012 |
|
RU2494020C1 |
| AIRCRAFT | 2019 |
|
RU2704639C1 |
| AIRCRAFT | 2013 |
|
RU2521145C1 |
| AIRBORNE VEHICLE | 2014 |
|
RU2560224C1 |
| FLYING VEHICLE | 2006 |
|
RU2312045C1 |
