EA200600916A1 - CONTROL AND TESTING EQUIPMENT - Google Patents
CONTROL AND TESTING EQUIPMENTInfo
- Publication number
- EA200600916A1 EA200600916A1 EA200600916A EA200600916A EA200600916A1 EA 200600916 A1 EA200600916 A1 EA 200600916A1 EA 200600916 A EA200600916 A EA 200600916A EA 200600916 A EA200600916 A EA 200600916A EA 200600916 A1 EA200600916 A1 EA 200600916A1
- Authority
- EA
- Eurasian Patent Office
- Prior art keywords
- input
- output
- control
- unit
- switch
- Prior art date
Links
Abstract
Изобретение относится к области контрольной техники и, в частности, предназначено для автономного диагностического контроля и проверки бортовой аппаратуры реактивных снарядов (9М55К). Контрольно-проверочная аппаратура (КПА) содержит пульт контроля и управления, включающий вычислитель, через блок формирования кода управления соединенный с блоком управления режимами, первый выход которого соединен с управляющим входом второго коммутатора, а второй выход соединен с управляющим входом первого коммутатора, второй информационный вход которого соединен с выходом блока управляемых имитаторов частотных датчиков, первый выход первого коммутатора соединен с первым входом блока измерителей, первый блок преобразования постоянного напряжения, выход которого подключен ко входу электропитания пульта контроля и управления, причем выход блока формирования кода управления соединен со входом блока управляемых имитаторов аналоговых датчиков и входом блока управляемых имитаторов частотных датчиков. В КПА дополнительно введены соединенное своим входом с разъемом подключения автономного источника электропитания устройство блокировки, трансформатор, соединенный своим входом с разъемом электропитания 220 В, выпрямитель, соединенный своим входом с выходом трансформатора, третий коммутатор, соединенный первым входом с выходом устройства блокировки, вторым входом с выходом выпрямителя, пороговый элемент и ключевой элемент, выход которого соединен со входом второго блока преобразования постоянного напряжения, выход которого соединен со входом электропитания блока управления режимами и входом порогового элемента, выходThe invention relates to the field of control technology and, in particular, is intended for autonomous diagnostic monitoring and verification of onboard equipment of missiles (9M55K). Control and test equipment (KPA) contains a monitoring and control panel, including a calculator, through the control code generation unit connected to the mode control unit, the first output of which is connected to the control input of the second switch, and the second output is connected to the control input of the first switch which is connected to the output of the controlled frequency sensors simulator unit, the first output of the first switch is connected to the first input of the meter unit, the first conversion unit is constant nnogo voltage, the output of which is connected to the input of the power remote monitoring and control unit and generating a control code output connected to the input unit driven simulators analogue sensors and the input unit driven simulators frequency sensors. A blocking device, a transformer connected by its input to a 220 V power supply connector, a rectifier connected by its input to a transformer output, a third switch connected by a first input to an output of a blocking device, a second input to the rectifier output, the threshold element and the key element, the output of which is connected to the input of the second DC voltage conversion unit, the output of which is connected to on the input of the power supply of the mode control unit and the input of the threshold element, output
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EA200600916A EA200600916A1 (en) | 2006-04-21 | 2006-04-21 | CONTROL AND TESTING EQUIPMENT |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EA200600916A EA200600916A1 (en) | 2006-04-21 | 2006-04-21 | CONTROL AND TESTING EQUIPMENT |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EA008973B1 EA008973B1 (en) | 2007-10-26 |
| EA200600916A1 true EA200600916A1 (en) | 2007-10-26 |
Family
ID=41203581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EA200600916A EA200600916A1 (en) | 2006-04-21 | 2006-04-21 | CONTROL AND TESTING EQUIPMENT |
Country Status (1)
| Country | Link |
|---|---|
| EA (1) | EA200600916A1 (en) |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3597760A (en) * | 1968-10-31 | 1971-08-03 | Baxter Laboratories Inc | Differential digital converter |
| SU1636917A1 (en) * | 1987-09-21 | 1991-03-23 | Карельское Районное Энергетическое Управление | Phase-comparison carrier-current protection |
| SU1529242A1 (en) * | 1987-12-07 | 1989-12-15 | Предприятие П/Я Р-6292 | Device for monitoring digital computing system |
| CN1264076C (en) * | 2001-04-05 | 2006-07-12 | 费希尔控制国际公司 | Control device test system with remote switch activation |
| UA61712C2 (en) * | 2003-04-02 | 2005-03-15 | Vasyl Oleksiiovyc Bezschastnyi | Device for monitoring parameters of a multifunctional system |
| RU2250565C2 (en) * | 2003-06-20 | 2005-04-20 | Сухолитко Валентин Афанасьевич | Computer-based instrumentation |
-
2006
- 2006-04-21 EA EA200600916A patent/EA200600916A1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| EA008973B1 (en) | 2007-10-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): AM AZ KZ KG MD TJ TM |
|
| MM4A | Lapse of a eurasian patent due to non-payment of renewal fees within the time limit in the following designated state(s) |
Designated state(s): BY RU |