MT-3000-2S
electric motor
Description
MT-3000-2S aircraft electric motor
MT-3000-2S is a specialized aircraft electric motor used to convert electrical energy into mechanical rotation for onboard auxiliary equipment. In the supplied context, the motor is associated mainly with high-speed drive units and aviation centrifugal pumps. The unit may be classified as aviation technical property and is historically linked with production by the Dnepropetrovsk Aggregate Plant. MT-3000-2S is used where a compact aircraft motor with high shaft speed and continuous operating capability is required.
Full descriptionCollapse description
Function of MT-3000-2S in aircraft systems
The main function of MT-3000-2S is to provide mechanical drive power for rotating aircraft units. The motor supplies torque to connected pump or auxiliary equipment assemblies and supports operation of onboard systems that require liquid transfer, pressure generation or circulation. In the source context, its primary associated unit is the ECN-17 electric centrifugal pump. Correct motor operation is important for stable pump performance and reliable function of the connected aircraft system.
Use with ECN-17 centrifugal pump
MT-3000-2S is described as a drive motor for the ECN-17 electric centrifugal pump. In this configuration, the motor drives the pump impeller and allows fuel or other working liquid to be transferred or circulated through the aircraft system. The source context describes ECN-17 as a pump used for liquid transfer and pressure generation. When supplied or replaced, compatibility should be checked by the pump assembly documentation, shaft interface, mounting dimensions and electrical connection data.
Series and related modifications
The “2S” index indicates the second series / modification of the MT-3000 motor family. Related versions mentioned in the supplied context include MT-3000-3S and the modernized MT-3000M / MT-3000M-2S. These variants may differ by dimensions, mechanical interface, electrical characteristics or installation requirements. They should not be treated as automatic substitutes without checking the technical documentation of the parent unit. For repair or procurement, the exact designation on the motor label and passport should be used.
Electrical and mechanical characteristics
According to the supplied data, MT-3000-2S operates from a 200 V, 400 Hz three-phase supply in the relevant aircraft / equipment configuration. The motor has a shaft speed of not less than 7600 rpm, current consumption up to 16 A and rated shaft torque of 36 kgf·cm. Its compact body and mass limit make it suitable for integration into aircraft pump units and high-speed assemblies. Exact connection diagrams and phase wiring should be confirmed by the product passport and equipment documentation.
Identification and ordering of MT-3000-2S
Before ordering MT-3000-2S, the buyer should confirm the parent unit, aircraft type, pump model, shaft configuration, mounting interface, condition and documentation requirements. It is especially important to state whether the motor is required specifically for ECN-17 or for another onboard drive unit. The item may be needed for pump repair, replacement of a defective motor, overhaul stock or support of aircraft liquid-transfer systems. Product passport, test records and preservation documents should be checked before shipment.
Related equipment: MT-3000-3S, MT-3000M, ECN-17. These links are grouped by function and system context and do not indicate interchangeability.
Technical details
- Product Type
- Aircraft electric motor / onboard pump drive motor
- Designation
- MT-3000-2S
- Russian Designation
- МТ-3000-2С
- Alternative Designations
- MT3000-2S, MT-3000 2S, МТ3000-2С, МТ-3000 2С
- Related Modifications
- MT-3000-3S, MT-3000M, MT-3000M-2S / МТ-3000-3С, МТ-3000М, МТ-3000М-2С
All specificationsCollapse specifications
- Alternative Product Names
- Aircraft electric motor, pump drive motor, high-speed electric motor, onboard electric drive
- Function
- Conversion of electrical energy into mechanical rotation for aircraft pump and auxiliary equipment drives
- Application / Where Used
- Aircraft pump units, fuel transfer systems and auxiliary high-speed drive assemblies
- System / Installation Area
- ECN-17 centrifugal electric pump or related onboard equipment according to configuration
- Associated Pump
- ECN-17 electric centrifugal pump according to source context
- Manufacturer Reference
- Dnepropetrovsk Aggregate Plant according to source context
- Series / Version
- Second series
- Supply Type
- Three-phase electrical supply according to source context
- Nominal Voltage
- 200 V
- Voltage Tolerance Reference
- ±10–20 V according to source context
- Frequency
- 400 Hz
- Frequency Tolerance Reference
- ±20 Hz according to source context
- Maximum Current Consumption
- 16 A
- Rotational Speed
- Not less than 7600 rpm
- Rated Shaft Torque
- 36 kgf·cm / approximately 3.53 N·m according to source context
- Operating Mode
- Continuous operation according to source context
- Motor Weight
- Not more than 10 kg
- Motor Dimensions
- 170 × Ø184 mm
- MT-3000M-2S Dimension Reference
- 173 × Ø175 mm according to source context
- ECN-17 Pump Flow Reference
- Up to 9000 l/h according to source context
- ECN-17 Pressure Differential Reference
- Not less than 392.4 kPa / 4 kgf/cm² according to source context
- ECN-17 Pump Assembly Weight Reference
- 14 kg according to source context
- Technical Documentation
- Product passport, ECN-17 documentation, aircraft system documentation, wiring diagram, preservation records and test documents if available
Payment & delivery
Orders ship from our hub in Dubai. Partner stock is first transferred to Dubai, then shipped to you.
Dubai stock: 100% before dispatch. Partner stock (Remote stock) and Pre-order: 50% advance payment to start the order and 50% before shipment from Dubai to you.
Availability, lead time, delivery cost and payment terms are confirmed for your order before payment.
Payment & delivery terms