FIELD: controls to steering gears of aircraft. SUBSTANCE: moment of spring with rigidity twice as much as rigidity of spring working over the rest of path of movement of armature when its angles deviate from center position acts over length of movement of armature determined by angles -αs and αs. Saturation of magnetic circuit is additionally ensured by magnetizing force. Induction in it exceeds induction of maximum magnetic permeability of material of magnetic circuit of electromagnet by 10% or over. Neutral electromagnet has body in which there are mounted: two stators with control windings, rotary armature in the form of plate put on axis, flat spring with linear static characteristic anchored with center part on axis of armature and limiters on ends of spring in the form of screws installed on side of one plane of spring. Each end of spring is tightened in advance up with screw through angle Flat spring shows rigidity EFFECT: increased speed of response of neutral electromagnets, their ensured operation without bounces of armature, preservation of dimensions of magnetic system. 2 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
ELECTROMAGNETIC DRIVE FOR SWITCHES | 1994 |
|
RU2074438C1 |
DYNAMICALLY ADJUSTED GYRO | 1999 |
|
RU2178142C2 |
ELECTROMAGNETIC PUMP | 2010 |
|
RU2424447C1 |
ELECTROMAGNETIC VALVE | 1997 |
|
RU2154218C2 |
ELECTROMAGNETIC UNIT OF GUIDED MISSILE CONTROL ACTUATOR | 2005 |
|
RU2283472C1 |
TURNABLE-ARMATURE HIGH-SPEED TWO-POSITION ELECTROMAGNET | 2003 |
|
RU2261495C1 |
POWER ELECTROMAGNET OF PULSE NON-EXPLOSIVE SEISMIC SOURCE | 2000 |
|
RU2172497C1 |
STEPPING MOTOR | 1990 |
|
RU2006144C1 |
METHOD OF REDUCING ELECTRIC POWER CONSUMPTION OF QUICK-ACTING DISTRIBUTOR AND DEVICE TO THIS EFFECT | 2006 |
|
RU2329412C1 |
ELECTROMAGNETIC MOTOR | 2014 |
|
RU2572040C1 |
Authors
Dates
2003-12-10—Published
2001-11-14—Filed