FIELD: aerospace engineering.
SUBSTANCE: invention relates to aerospace engineering. Aircraft consists of two jet engines rigidly connected to the body, cone-shaped combustion chamber, rigidly connected to the exhaust nozzle at the end of the combustion chamber. In the aircraft, a control unit with a laser is used and a light guide is inserted with consecutive branches within the combustion chamber and having an optical input, connected to the optical output of the control unit with a laser having optical outputs connected through refractory transparent inserts at the end of the respective branches, rigidly connected to the inner side of the wall of the combustion chamber, with optical inputs of the corresponding sections of this chamber.
EFFECT: technical result of the invention is higher acceleration of an aircraft.
1 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT | 2018 |
|
RU2701079C1 |
AIRCRAFT | 2012 |
|
RU2494020C1 |
AIRCRAFT | 2019 |
|
RU2704639C1 |
FLIGHT VEHICLE | 2008 |
|
RU2363625C1 |
AIRCRAFT | 2013 |
|
RU2521145C1 |
AIRBORNE VEHICLE | 2014 |
|
RU2560224C1 |
AIRCRAFT | 2014 |
|
RU2595217C2 |
AIRCRAFT | 2015 |
|
RU2577742C2 |
AIRCRAFT | 2008 |
|
RU2378162C1 |
AIRCRAFT | 2008 |
|
RU2380294C1 |
Authors
Dates
2018-09-24—Published
2017-07-25—Filed