FIELD: aircraft engineering.
SUBSTANCE: invention relates to propellants of aircraft (AC). AC comprises auxiliary jet engines, a damper and a control unit connected with the damper. Latter includes a chamber with approaching side walls and two spring gas-isolating valves. Herewith the control unit provides selection of a certain time of fuel cassettes supply to the chamber with an interval till the moment of the AC uniform movement. This moment is the beginning of a new phase of the AC acceleration.
EFFECT: technical result of the invention is aimed at higher fuel efficiency at the AC acceleration.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
FLIGHT VEHICLE | 2008 |
|
RU2363625C1 |
AIRCRAFT | 2008 |
|
RU2380294C1 |
AIRCRAFT | 2015 |
|
RU2577742C2 |
AIRCRAFT | 2010 |
|
RU2438938C1 |
AIRCRAFT | 2015 |
|
RU2577750C1 |
AIRCRAFT | 2019 |
|
RU2704639C1 |
AIRBORNE VEHICLE | 2014 |
|
RU2560224C1 |
AIRCRAFT | 2013 |
|
RU2521145C1 |
AIRCRAFT | 2012 |
|
RU2494020C1 |
FLYING VEHICLE | 2006 |
|
RU2312045C1 |
Authors
Dates
2016-08-20—Published
2014-12-02—Filed