FIELD: engines and pumps.
SUBSTANCE: method of control over aircraft with two and more engines consists in differential feed of fuel. Fuel feed is performed by main fuel pumps and extra fuel system driven by actuating spring of one of the main engines or by motor and electric or air operated stabilisation control system. Proposed device consists of differential fuel feed system, direction and/or pitch control stabilisation system and set of gyroscope transmitters.
EFFECT: bank control in hovering.
13 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT CONTROL DEVICE | 2013 |
|
RU2551584C1 |
| COUNTERAIR MISSILE | 2009 |
|
RU2439476C2 |
| AA MISSILE GUIDANCE SYSTEM | 2009 |
|
RU2400690C1 |
| CONTROL METHOD OF AIRCRAFT WITH TWO AND MORE ENGINES-2 | 2014 |
|
RU2553614C1 |
| ALTITUDE INDICATOR | 2010 |
|
RU2428657C1 |
| CANARD CONTROL (VERSIONS) | 2012 |
|
RU2531706C2 |
| CANARD CONTROL (VERSIONS) | 2007 |
|
RU2410286C2 |
| RESCUE SYSTEM OF AIRPLANE (VERSIONS) | 2006 |
|
RU2336203C2 |
| STAROVEROV'S AIRCRAFT (VERSIONS) | 2011 |
|
RU2490169C2 |
| STAROVEROV'S SPACECRAFT (VERSIONS) AND/OR ALGORITHMS OF ITS OPERATION | 2012 |
|
RU2503592C1 |
