FIELD: hydraulic controlling gears. SUBSTANCE: invention refers to driving cylindrical electromagnets. Electromagnet has magnetic body 1, cylindrical sleeve 3, anchor 4 moving in sleeve 3, flange 2 located in body and sleeve. Ferromagnetic sleeve 3 is divided into two parts by trapezoidal nonmagnetic ring 6, working butt of anchor has circular trapezoidal collar 7 that interacts with groove 8 of similar profile in flange and with sleeve. Side surface of anchor has flat 11 on side of working clearance 11 and frame 1 is formed by flange 2, sleeve 3 and washer 10. EFFECT: increased reliability and diminished energy consumption. 4 dwg
Title | Year | Author | Number |
---|---|---|---|
PROPORTIONAL ELECTROMAGNET | 1997 |
|
RU2121726C1 |
ELECTROMAGNET | 2002 |
|
RU2224314C1 |
LONG-STROKE ELECTROMAGNET WITH CONSTANT TRACTIVE FORCE IN OPERATING STROKE | 2019 |
|
RU2711179C1 |
PULSE PERMANENT-MAGNET GENERATOR | 1997 |
|
RU2122177C1 |
ELECTROMAGNET MANUFACTURING PROCESS AND DEVICE | 1998 |
|
RU2144714C1 |
AIR-DYNAMIC STEERING DRIVE OF GUIDED MISSILE | 1997 |
|
RU2121651C1 |
STATOR OF CONSTANT CURRENT ELECTRIC MACHINE WITH CONSTANT MAGNETS | 2006 |
|
RU2306658C1 |
DOUBLE-SIDED POLARIZED ELECTROMAGNET WITH PASSIVE STOCK RETENTION | 2016 |
|
RU2634423C1 |
POLARIZED ELECTROMAGNETIC WITH PASSIVE STOCK RETENTION | 2016 |
|
RU2634424C1 |
PULSE PERMANENT-MAGNET GENERATOR FOR ACTUATION OF ELECTRIC PRIMERS OF GUIDED MISSILE LAUNCHING AND ON-BOARD SYSTEMS AND METHOD FOR ITS REALIZATION | 1999 |
|
RU2168699C2 |
Authors
Dates
1998-07-10—Published
1996-07-11—Filed