NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters
In Stock

NGLM Series RTCA/DO-160 Compliant Three-Phase Output Pure Sine Wave DC-AC Inverters

RRP

FEATURES

  • RTCA/DO-160 and MIL-STD-704 Qualified
  • Compact and light weight
  • Rugged design
  • Tightly regulated output voltage and frequency
  • Able to supply inrush current
  • Factory set to 50 Hz, 60 Hz or 400 Hz output
  • Capable of driving highly reactive loads
  • Capable of driving highly capacitive loads
    such as non PFC switching power supplies
  • Very low harmonic distortion, THD<3%
  • Suitable for vehicle mounting
  • Fan cooled with air filter
SKU: 5285 Category: Tags: , , , , , ,

Description

[vc_row][vc_column][vc_column_text]Nova Electric’s rugged NGLM inverters are extremely reliable, designed to provide many years of service in high shock, vibration, humidity, and EMI environments in compliance to RTCA/DO-160G and MIL-STD-704F. These units accept standard inputs of 28, 48, 120, or 230 Volts DC nominal. They are offered in 3KVA, 4.5KVA and 6KVA output power, and output voltage is tightly regulated with less than 3% total harmonic distortion. The NGLM units are modular, with small footprints and flexible mounting configurations. The inverter chassis measures only 17.75”L x 13”W x 8”H and weighs just 34 pounds total. A mounting plate is integrated into the chassis. Input connection is typically via bus bars with terminal blocks for output, though circular MS-type connectors are available optionally. These inverters use field–proven, cutting edge IGBT-based high frequency switching technology to achieve very high MTBF, and very low mean time to repair. Typical applications include:

  • Airborne Applications
  • Military Vehicle Applications
  • Ground Support
  • Mobile Systems
  • Tactical Systems
  • Naval Applications
  • Communications

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Specifications

ELECTRICAL
  • Input Voltage (select): See Table for Nominal DC Input.
    28 VDC Nominal Range is 22-32 VDC
    48 VDC Nominal Range is 42-56 VDC
    120 VDC Nominal Range is 105-150 VDC
    230 VDC Nominal Range is 210-280 VDC
  • Output Voltage (select): Select 120/208, 115/200, or 220/380 VAC
  • Output Frequency: Select 50 Hz, 60 Hz or 400 Hz
  • Overload: 125% for 5 minutes
  • Output Waveform Sinewave: <3% THD
  • Output Regulation: ± 2.5%
  • MTBF: over 100,000 hours per field data
  • MTTR: 30 minutes
  • EMI: Designed to meet MIL-STD-461 optionally
  • Compliant to MIL-STD-704 Aircraft Electrical Power Characteristics
ENVIRONMENTAL (Standard)
  • Operating Temperature: -20°C to +50°C
  • Storage Temperature: -40°C to + 71°C
  • Shock: 20g / 11 mS per MIL-STD-810
  • Vibration: Designed to meet MIL-STD-810 and MIL-STD-167
  • Humidity: Designed to meet MIL-STD-810 to 95% non condensing
RTCA/DO-160G COMPLIANCE (Optional)
  • Humidity per RTCA/DO-160G, Section 6, paragraph 6.3.1, Category A, Figure 6-1
  • Ground survival low temperature per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.1, Table 4-1, Figure 4-1
  • Low temperature (operating) per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.2, Table 4-1, Figure 4-2
  • High temperature (operating) per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.4, Table 4-1, Figure 4-4
  • Altitude per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.6.1, Table 4-1, Figure 4-6
  • Ground survival high temperature per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.3, Table 4-1, Figure 4-3
  • Vibration per RTCA/DO-160G, Section 8, Category S, Fixed-Wing, Figure 8-3, Curve L 
  • Standard operational shock per RTCA/DO-160G, Section 7, Figure 7-2
  • Temperature variation per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, Section 5, Category C, Figure 5-1

 PROTECTIVE FEATURES

  • Overload
  • Overvoltage
  • Overtemperature

Popular Options

OPTIONS

Compliance

MIL-STD-704 Aircraft Electrical Power Characteristics

RTCA/DO-160G COMPLIANCE (Optional)
  • Humidity per RTCA/DO-160G, Section 6, paragraph 6.3.1, Category A, Figure 6-1
  • Ground survival low temperature per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.1, Table 4-1, Figure 4-1
  • Low temperature (operating) per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.2, Table 4-1, Figure 4-2
  • High temperature (operating) per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.4, Table 4-1, Figure 4-4
  • Altitude per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.6.1, Table 4-1, Figure 4-6
  • Ground survival high temperature per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, paragraph 4.5.3, Table 4-1, Figure 4-3
  • Vibration per RTCA/DO-160G, Section 8, Category S, Fixed-Wing, Figure 8-3, Curve L 
  • Standard operational shock per RTCA/DO-160G, Section 7, Figure 7-2
  • Temperature variation per RTCA/DO-160G, Category B1, Fixed Wing Aircraft, Section 5, Category C, Figure 5-1

 

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