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Engine Cooling Fan & SiC Controller

Engine Cooling Fan & SiC Controller

Engine Cooling Fan & SiC Controller

Product catalog summary
Physical Specifications:
- Controller Weight: 9.52 kg (21 lbs.)
- EMI Weight: 3.75 kg (8.25 lbs)
- Controller Dimensions: 122mm (H) x 223mm (Dia) (4.8” x 8.77” inches)
- EMI Dimensions: 173mm x 168mm x 111mm (6.8” x 6.6” x 4.4” inches)
- Connector Type: MIL-C-38999
- Mounting: Top of Main Cooling Fan

Environmental Specifications:
- Operating Temperature: -46°C to +90°C ambient
- Temperature Shock, Shock, Vibration, Humidity, and Immersion: Compliant with MIL-STD-810G

Product Overview:
The 1068000G1 is a 610 Vdc silicon carbide (SiC) based, air-cooled inverter and motor controller integrated onto an electric Engine Cooling Fan. It uses GE’s SiC MOSFETs for a compact and efficient design, eliminating the need for separate motor drive inverters and related components. This integration reduces size and weight and enhances reliability in high-temperature environments.

Key Features:
- Best-in-Class SiC MOSFETs
- Digitally Controlled Operation
- Fault Reporting over CANBus
- High Efficiency and Reliability
- MIL-PRF-GCS600AVDC Input
- Overcurrent & Overvoltage Protection
- EMI Compliance: MIL-STD-461F
- Operates in 90°C ambient air
- Derating: NAVMAT-P-4855-1
- AEC-Q101 SiC device qualification
- Submergible up to 2 meters
- Nuclear Event Detection

Electrical I/O:
- Part Number: 1068000G1
- Input Voltage: 610 VDC
- Output: Variable Frequency 3 phase AC, 50A (RMS), 25.25 kW
- Connectors: J1-A: HVIL, J2-A: 28Vdc Control, J1-B: +305Vdc, J2-B: 28Vdc Cont. RTN, J1-C: HVIL RTN, J2-C: CANBus High, J1-D: -305Vdc, J2-D: CANBus Low

Contact Information:
- GE Aviation, 2705 Gateway Drive, Pompano Beach, Florida 33069 USA, 954-984-7000
- 1000 MacArthur Highway, Bohemia, New York 11716 USA, 631-467-5500
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Catalog excerpts

Engine Cooling Fan & SiC Controller-1

Engine Cooling Fan & SiC Controller The 1068000G1 is a 610 Vdc silicon carbide (SiC) based, air-cooled inverter and motor controller integrated onto an electric Engine Cooling Fan. The design utilizes GE’s SiC MOSFETs which enable an all-in-one Controller/Inverter/Fan solution, eliminating the traditional Fan with separate Motor Drive Inverter and its related coolant hoses and interconnecting cables. The SiC devices yield high power density and reduced size and weight for the cooling subsystem. Advanced thermal management technologies are employed to enable reliable operation in the high temperature environment. This Integrated Engine Cooling Fan solution allows the elimination of hydraulic motors and related pumps and hoses, or gear boxes and drive shafts in mechanically driven Fan solutions. Features: ♦ Best-in-Class SiC MOSFETs ♦ Digitally Controlled Operation ♦ Fault Reporting over CANBus ♦ High Efficiency ♦ Reduced weight versus Silicon ♦ High Reliability ♦ MIL-PRF-GCS600AVDC Input ♦ Overcurrent & Overvoltage Protection. ♦ EMI - MIL-STD-461F ♦ 90°C ambient air temperature ♦ Derating - NAVMAT-P-4855-1 ♦ AEC-Q101 SiC device qualification ♦ Submergible (up to 2 meters water) ♦ Nuclear Event Detection Electrical I/O: Physical: (See icd 1068001) Weight (Controller): 9.52kg (21 lbs.) (EMI): 3.75 kg (8.25 lbs) Dimensions (Controller): 122mm (H) x 223mm (Dia) (4.8” x 8.77”) (EMI):173mm x 168mm x 111mm (6.8” x 6.6” x 4.4”) Connector: MIL-C-38999 Mounting: Mounts to top of Main Cooling Fan Environmental: Operating Temperature: -46°C to +90°C ambient Temperature Shock: MIL-STD-810G, Shock: MIL-STD-810G, Vibration: MIL-STD-810G Method 514.4, Procedure I category 20, ground vehicles Humidity: MIL-STD-810G, Immersion: MIL-STD-810G, 2 meters for 2 hours

 Open the catalog to page 1
Engine Cooling Fan & SiC Controller-2

Mechanical Outline GE Aviation 2705 Gateway Drive Pompano Beach, Florida 33069 USA 954-984-7000 1000 MacArthur Highway Bohemia, New York 11716 USA 631-467-5500

 Open the catalog to page 2

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