FIELD: testing instruments. SUBSTANCE: device has chamber with socket for pneumatic distributor, compressed air source and pressure gage which are connected to chamber. Cross section of input channel from compressed air source and volume of chamber are equal to cross sections of input constrictor and volume of power cylinder respectively. Pneumatic chamber has two-position valve which provides through residual hole which section which is equal to one third of area of input constrictor of power cylinder. In addition it has sealed unit for tuning of electromagnet spring. EFFECT: possibility to model operations of pneumatic distributor in real conditions of pneumatic drive, simplified design of tuning. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIR-DYNAMIC UNIT OF GUIDED PROJECTILE ACTUATOR | 2002 |
|
RU2234670C2 |
| METHOD AND TEST STAND FOR CHECKING QUALITY OF OPERATION OF ACTUATORS AND GYROPILOTS OF CONTROLLED MISSILES | 1999 |
|
RU2182702C2 |
| AIR-DYNAMIC UNIT OF CONTROL ACTUATOR OF GUIDED MISSILE | 2002 |
|
RU2237857C2 |
| METHOD OF AND PNEUMATIC CONTROL ACTUATOR TO CONTROL GUIDE MISSILE | 2003 |
|
RU2254501C2 |
| SELF-SUSTAINED AUTOPILOT OF GUIDED MISSILE | 1992 |
|
RU2092784C1 |
| GUIDED MISSILE CONTROL ACTUATOR UNIT | 1996 |
|
RU2092783C1 |
| ELECTRO-PNEUMATIC CONTROL ACTUATOR OF GUIDED MISSILE | 1999 |
|
RU2157503C1 |
| METHOD OF CHECK OF FUNCTIONING OF ACTUATORS AND AUTOPILOTS OF CONTROLLABLE PROJECTILES AND DEVICE FOR REALIZATION OF THIS METHOD | 1999 |
|
RU2181681C2 |
| SELF-SUSTAINED CONTROL ACTUATOR OF GUIDED MISSILE | 1997 |
|
RU2114387C1 |
| GUIDED MISSILE AERODYNAMIC CONTROL ACTUATOR | 1994 |
|
RU2074382C1 |
