FIELD: engines and pumps.
SUBSTANCE: invention relates to system for control over turbojet multiple various functions. Every said functions is associated with definite actuator. Said system comprises motor designed to feed mechanical power to every actuator, motor electronic control unit, and switch arranged between motor and actuators. Said switch serves to effect distribution mechanical power supplied by motor to one of actuators in selective manner.
EFFECT: lower costs, simplified design.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBOJET ENGINE ELECTROMECHANICAL THRUST REVERSER WITH DOOR AUTOMATIC CONTROL SYSTEM | 2003 |
|
RU2323360C2 |
TURBOJET ENGINE NACELLE CONTROL SYSTEM | 2006 |
|
RU2398716C2 |
TURBOJET NACELLE MOVING PANEL DRIVE SYSTEM | 2010 |
|
RU2521906C2 |
CONTROL SYSTEM OF ELECTRIC DEVICE OF NACELLE | 2011 |
|
RU2572730C2 |
CONTROL SYSTEM FOR TURBOJET ENGINE NACELLE AND NACELLE EQUIPPED WITH SUCH SYSTEM | 2010 |
|
RU2531204C2 |
METHOD OF CONTROLLING THRUST REVERSER MOTORS | 2008 |
|
RU2451198C2 |
STABILITY AND CONTROL AUGMENTATION SYSTEM | 2015 |
|
RU2638067C2 |
ELECTRICAL CONTROL SYSTEM FOR TURBOJET ENGINE THRUST REVERSER | 1997 |
|
RU2142569C1 |
POWER SUPPLY CIRCUIT FOR TURBOJET ENGINE NACELLE | 2010 |
|
RU2561613C2 |
CONTROL METHOD OF ACTIVATION OF THRUST REVERSER | 2005 |
|
RU2392474C2 |
Authors
Dates
2013-04-20—Published
2009-02-13—Filed