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Power MOSFET Selection Analysis for High-End Chemical Transport eVTOLs – A Case Study on High Power Density, High Reliability, and Safety-Critical Power Systems
Chemical Transport eVTOL Power System Topology Diagram

Chemical Transport eVTOL Power System Overall Topology Diagram

graph LR %% High Voltage Battery & Propulsion System subgraph "High-Voltage Propulsion & Battery System" HV_BAT["800V High-Voltage
Battery Pack"] --> BMS["Battery Management System
(BMS)"] subgraph "Three-Phase Propulsion Inverter" PHASE_U["Phase U Bridge Leg"] PHASE_V["Phase V Bridge Leg"] PHASE_W["Phase W Bridge Leg"] end BMS --> DC_BUS["800V DC Bus"] DC_BUS --> PHASE_U DC_BUS --> PHASE_V DC_BUS --> PHASE_W subgraph "SiC MOSFET Array (Inverter)" Q_UH["VBP112MC60-4L
1200V/60A SiC"] Q_UL["VBP112MC60-4L
1200V/60A SiC"] Q_VH["VBP112MC60-4L
1200V/60A SiC"] Q_VL["VBP112MC60-4L
1200V/60A SiC"] Q_WH["VBP112MC60-4L
1200V/60A SiC"] Q_WL["VBP112MC60-4L
1200V/60A SiC"] end PHASE_U --> Q_UH PHASE_U --> Q_UL PHASE_V --> Q_VH PHASE_V --> Q_VL PHASE_W --> Q_WH PHASE_W --> Q_WL Q_UH --> MOTOR_U["Motor Phase U"] Q_UL --> GND_HV Q_VH --> MOTOR_V["Motor Phase V"] Q_VL --> GND_HV Q_WH --> MOTOR_W["Motor Phase W"] Q_WL --> GND_HV MOTOR_U --> PROP_MOTOR["Propulsion Motor"] MOTOR_V --> PROP_MOTOR MOTOR_W --> PROP_MOTOR end %% Intermediate Power Distribution subgraph "Intermediate Voltage Domain (48V/60V)" subgraph "Multi-Phase DC-DC Converter" PHASE1["Converter Phase 1"] PHASE2["Converter Phase 2"] PHASE3["Converter Phase 3"] end DC_BUS --> BUCK_IN["DC-DC Input"] BUCK_IN --> PHASE1 BUCK_IN --> PHASE2 BUCK_IN --> PHASE3 subgraph "Dual N-MOSFET Array" Q_DC1["VBGQA3610
60V/30A per Ch"] Q_DC2["VBGQA3610
60V/30A per Ch"] Q_DC3["VBGQA3610
60V/30A per Ch"] end PHASE1 --> Q_DC1 PHASE2 --> Q_DC2 PHASE3 --> Q_DC3 Q_DC1 --> INT_BUS["48V/60V Intermediate Bus"] Q_DC2 --> INT_BUS Q_DC3 --> INT_BUS INT_BUS --> AUX_LOADS["Auxiliary Systems"] end %% Intelligent Load Management subgraph "Intelligent Load Switching & Safety" FLIGHT_MCU["Flight Control MCU"] --> LOAD_SW_CONTROL["Load Switch Controller"] subgraph "Safety-Critical Load Switches" SW_AVIONICS["VBQG8218
Sensor Power"] SW_COMM["VBQG8218
Communication"] SW_CHEM_INT["VBQG8218
Chemical Interlock"] SW_SAFETY["VBQG8218
Safety Solenoid"] end LOAD_SW_CONTROL --> SW_AVIONICS LOAD_SW_CONTROL --> SW_COMM LOAD_SW_CONTROL --> SW_CHEM_INT LOAD_SW_CONTROL --> SW_SAFETY INT_BUS --> SW_AVIONICS INT_BUS --> SW_COMM INT_BUS --> SW_CHEM_INT INT_BUS --> SW_SAFETY SW_AVIONICS --> AVIONICS["Flight Sensors & Avionics"] SW_COMM --> COMM["Communication Module"] SW_CHEM_INT --> CHEM_INTERLOCK["Chemical Container Interlock"] SW_SAFETY --> SAFETY_SOL["Emergency Safety Solenoid"] end %% Driving & Protection Systems subgraph "Gate Driving & System Protection" subgraph "SiC Gate Drivers" DRV_UH["Phase U High-Side Driver"] DRV_UL["Phase U Low-Side Driver"] DRV_VH["Phase V High-Side Driver"] DRV_VL["Phase V Low-Side Driver"] DRV_WH["Phase W High-Side Driver"] DRV_WL["Phase W Low-Side Driver"] end INVERTER_CTRL["Inverter Controller"] --> DRV_UH INVERTER_CTRL --> DRV_UL INVERTER_CTRL --> DRV_VH INVERTER_CTRL --> DRV_VL INVERTER_CTRL --> DRV_WH INVERTER_CTRL --> DRV_WL DRV_UH --> Q_UH DRV_UL --> Q_UL DRV_VH --> Q_VH DRV_VL --> Q_VL DRV_WH --> Q_WH DRV_WL --> Q_WL subgraph "Protection Circuits" DC_LINK_CAP["DC-Link Capacitor Bank"] GATE_SNUB["Gate RC Snubbers"] TVS_PROT["TVS Diode Array"] OCP_CIRCUIT["Hardware Overcurrent Protection"] end DC_BUS --> DC_LINK_CAP DRV_UH --> GATE_SNUB TVS_PROT --> DRV_UH OCP_CIRCUIT --> FAULT_LATCH["Fault Latch"] FAULT_LATCH --> SHUTDOWN["System Shutdown"] end %% Thermal Management subgraph "Tiered Thermal Management" COOL_LVL1["Level 1: Liquid Cooling"] --> Q_UH COOL_LVL1 --> Q_VH COOL_LVL1 --> Q_WH COOL_LVL2["Level 2: PCB Heat Spreader"] --> Q_DC1 COOL_LVL2 --> Q_DC2 COOL_LVL2 --> Q_DC3 COOL_LVL3["Level 3: PCB Copper Pour"] --> SW_AVIONICS TEMP_SENSORS["Temperature Sensors"] --> THERMAL_MCU["Thermal Management MCU"] THERMAL_MCU --> PUMP_CTRL["Pump Control"] THERMAL_MCU --> FAN_CTRL["Fan Control"] end %% Communication Network FLIGHT_MCU --> CAN_BUS["Vehicle CAN Bus"] FLIGHT_MCU --> RF_COMM["RF Communication"] BMS --> CAN_BUS INVERTER_CTRL --> CAN_BUS %% Style Definitions style Q_UH fill:#e8f5e8,stroke:#4caf50,stroke-width:2px style Q_DC1 fill:#e3f2fd,stroke:#2196f3,stroke-width:2px style SW_AVIONICS fill:#fff3e0,stroke:#ff9800,stroke-width:2px style FLIGHT_MCU fill:#fce4ec,stroke:#e91e63,stroke-width:2px

In the context of advancing low-altitude logistics and specialized transport, Electric Vertical Take-Off and Landing (eVTOL) aircraft for chemical transport represent a critical and demanding application within the mobility ecosystem. Their performance and, most importantly, their safety are directly governed by the capabilities of their onboard electrical power systems. The propulsion motor drives, high-voltage battery management, and distributed auxiliary power distribution act as the vehicle's "power core and nervous system," responsible for reliable thrust, efficient energy utilization, and safe management of critical loads. The selection of power MOSFETs profoundly impacts system power-to-weight ratio, conversion efficiency, thermal management under demanding duty cycles, and intrinsic safety. This article, targeting the extreme application scenario of chemical transport eVTOLs—characterized by stringent requirements for specific power, ruggedness, fault tolerance, and operation in potentially harsh environments—conducts an in-depth analysis of MOSFET selection considerations for key power nodes, providing a complete and optimized device recommendation scheme.
Detailed MOSFET Selection Analysis
1. VBP112MC60-4L (Single-N SiC MOSFET, 1200V, 60A, TO-247-4L)
Role: Main switch in the high-voltage propulsion inverter or high-step-up DC-DC converter for the battery system.
Technical Deep Dive:
Voltage Stress & Efficiency Imperative: For high-performance eVTOLs utilizing 800V or higher battery buses, the 1200V rating of this Silicon Carbide (SiC) MOSFET provides a robust safety margin against switching voltage spikes and bus transients. Its SiC-S technology offers superior switching performance compared to silicon, drastically reducing switching losses at high frequencies. This enables higher PWM frequencies for the propulsion inverter, leading to reduced motor current ripple, lower torque pulsation, and smaller, lighter output filter components—a direct contribution to maximizing the vehicle's power density and flight time.
System Integration & Thermal Performance: The 4-lead TO-247-4L package features a separated source sense (Kelvin connection) which minimizes parasitic inductance in the gate drive loop, ensuring faster, cleaner switching and maximizing the performance benefits of SiC. The low Rds(on) of 40mΩ (typ. @18V) minimizes conduction losses in high-current phases. This combination is critical for building compact, liquid-cooled inverter modules that must deliver peak power reliably during take-off and climb, while maintaining high efficiency across the entire flight envelope.
2. VBGQA3610 (Dual-N+N MOSFET, 60V, 30A per Ch, DFN8(5X6)-B)
Role: Synchronous rectifier or main switch in intermediate 48V/60V domain DC-DC converters, or for parallelized high-current load switching in Battery Management System (BMS) modules.
Extended Application Analysis:
High-Density Power Conversion Core: The onboard 48V or low-voltage bus powers avionics, sensors, servo actuators, and safety systems. The dual N-channel configuration in an ultra-compact DFN8 package allows for a highly integrated power stage design. Utilizing SGT (Shielded Gate Trench) technology, it achieves an exceptionally low Rds(on) of 10mΩ (typ. @10V) per channel, minimizing conduction losses in space-constrained areas.
Power Density & Parallelability: The small footprint and dual-die design enable the creation of extremely power-dense multi-phase buck or boost converters. Multiple devices can be easily paralleled to scale current handling for high-power auxiliary systems. The low thermal resistance of the package allows efficient heat transfer to a PCB-mounted heatsink or cold plate, which is vital for maintaining reliability in the thermally challenging environment of an integrated eVTOL powertrain bay.
Dynamic Performance for Robust Control: The fast switching capability supported by low gate charge is essential for high-frequency DC-DC conversion, reducing the size of magnetics and capacitors. This contributes directly to weight savings. Furthermore, the dual independent channels enable redundant or interleaved control schemes, enhancing system fault tolerance—a key consideration for safety-critical transport.
3. VBQG8218 (Single-P MOSFET, -20V, -10A, DFN6(2X2))
Role: Intelligent high-side load switch for safety-critical auxiliary systems, sensor power rails, or isolation control in monitoring circuits.
Precision Power & Safety Management:
High-Reliability Load Control: This P-channel MOSFET in a miniature DFN6 package is ideal for point-of-load (PoL) power switching. Its -20V rating is perfectly suited for 12V/24V vehicle auxiliary buses. The extremely low Rds(on) (18mΩ typ. @4.5V) ensures minimal voltage drop and power loss when powering critical flight sensors, communication modules, or safety solenoids (e.g., for chemical container interlocks).
Intelligent & Protected Switching: The low gate threshold voltage (Vth: -0.8V) allows for direct, efficient control by low-voltage MCUs or logic-level outputs. This simplifies the drive circuitry while enabling sophisticated power sequencing and fault management. Each critical subsystem can be independently powered and rapidly disconnected by the flight computer in case of a fault detection (e.g., gas sensor alarm, communication loss), preventing fault propagation and enabling fail-operative strategies.
Environmental Ruggedness: The ultra-small package and Trench technology offer good resistance to vibration and thermal stress. Its compact size facilitates placement close to the load, reducing trace inductance and improving transient response, which is crucial for the stable operation of sensitive avionics in the dynamic eVTOL environment.
System-Level Design and Application Recommendations
Drive Circuit Design Key Points:
SiC MOSFET Drive (VBP112MC60-4L): Requires a dedicated, high-performance gate driver optimized for SiC, providing strong turn-on/off current capability (+/- 5A typical). Careful attention to gate loop layout minimization and the use of negative turn-off voltage (e.g., -3 to -5V) is mandatory to prevent parasitic turn-on and ensure robust operation.
Dual Low-Voltage Switch Drive (VBGQA3610): A multi-channel gate driver with adequate current capability is recommended. Proper RC snubbing or ferrite beads may be needed at switch nodes to mitigate high-frequency ringing due to very fast edges, especially in parallel configurations.
High-Side P-MOS Drive (VBQG8218): Simple level-shift or charge pump circuits can be used for high-side control if the MCU voltage is lower than the load rail. Incorporating gate-source Zener clamping and series resistance is advised for ESD protection and oscillation damping.
Thermal Management and EMC Design:
Tiered Thermal Design: VBP112MC60-4L must be mounted on a liquid-cooled cold plate. VBGQA3610 requires a thermal via array or direct attachment to a PCB heat spreader connected to the main cooling system. VBQG8218 relies on PCB copper pour for heat dissipation.
EMI Suppression: Utilize low-inductance DC-link capacitor banks near the VBP112MC60-4L. Apply gate resistors and RC snubbers tailored to the switching speed of VBGQA3610. Ensure power and return paths for all switches are tightly coupled (e.g., using plane layers) to minimize loop area and radiated emissions, which is critical for avionics compatibility.
Reliability Enhancement Measures:
Adequate Derating: Operate VBP112MC60-4L at a maximum of 70-80% of its rated voltage under worst-case transients. Ensure the junction temperature of VBGQA3610 is monitored or estimated, with limits set well below the maximum rating.
Redundant and Protected Architecture: Design power paths with VBQG8218 to support redundant power feeds for critical sensors. Implement hardware-based overcurrent protection (e.g., eFuse ICs) on branches controlled by these switches for millisecond-level fault isolation.
Enhanced Protection: Use TVS diodes on all gate drives and at the input of sensitive loads. Conformal coating of PCBs may be necessary to protect against condensation and chemical exposure, depending on the operational environment.
Conclusion
In the design of high-power, safety-critical electrical systems for chemical transport eVTOLs, power MOSFET selection is key to achieving the required specific power, operational reliability, and functional safety. The three-tier MOSFET scheme recommended—spanning high-voltage SiC propulsion, high-density intermediate power conversion, and intelligent low-voltage distribution—embodies the design philosophy of maximum performance, robustness, and intelligence.
Core value is reflected in:
Optimized Propulsion & Efficiency: The SiC-based VBP112MC60-4L enables a lighter, more efficient propulsion inverter, directly extending range and payload capacity. The high-density VBGQA3610 optimizes power conversion for non-propulsive systems, maximizing available energy for flight.
Functional Safety & Fault Management: The independently controllable VBQG8218 switches provide the hardware foundation for implementing robust power distribution networks (PDNs) with isolation capabilities, essential for containing faults and ensuring continuous operation of critical systems.
Rugged System Integration: The selected devices, from the high-power SiC to the miniature load switch, are chosen for their technological advantages and package robustness, supporting reliable operation under the vibrations, temperature cycles, and stringent reliability demands of aerial chemical logistics.
Future Trends:
As eVTOLs evolve towards higher voltages, increased autonomy, and more stringent safety certifications, power device selection will trend towards:
Wider adoption of higher voltage (1700V+) SiC MOSFETs for direct grid charging interfaces or higher serial battery cells.
Integration of smart power switches with embedded current sensing, temperature monitoring, and digital status reporting for enhanced system health monitoring.
Use of GaN HEMTs in high-frequency auxiliary power supplies (APUs) and radio-frequency systems to push power density boundaries further.
This recommended scheme provides a foundational power device solution for chemical transport eVTOL power systems, spanning from the high-voltage battery to the motor phases, and from core DC-DC conversion to intelligent, safety-aware load management. Engineers can refine this selection based on specific voltage levels (e.g., 350V vs. 800V bus), cooling strategies, and the required Safety Integrity Level (SIL) or Design Assurance Level (DAL) to build the robust, high-performance electrical backbone required for the future of specialized low-altitude transport.

Detailed Topology Diagrams

High-Voltage Propulsion Inverter Topology Detail

graph LR subgraph "Three-Phase Inverter Bridge" DC_POS["800V DC Bus Positive"] --> PHASE_U_NODE["Phase U Node"] DC_POS --> PHASE_V_NODE["Phase V Node"] DC_POS --> PHASE_W_NODE["Phase W Node"] subgraph "Phase U Half-Bridge" Q_UH_INV["VBP112MC60-4L
High-Side"] Q_UL_INV["VBP112MC60-4L
Low-Side"] end subgraph "Phase V Half-Bridge" Q_VH_INV["VBP112MC60-4L
High-Side"] Q_VL_INV["VBP112MC60-4L
Low-Side"] end subgraph "Phase W Half-Bridge" Q_WH_INV["VBP112MC60-4L
High-Side"] Q_WL_INV["VBP112MC60-4L
Low-Side"] end PHASE_U_NODE --> Q_UH_INV PHASE_U_NODE --> Q_UL_INV PHASE_V_NODE --> Q_VH_INV PHASE_V_NODE --> Q_VL_INV PHASE_W_NODE --> Q_WH_INV PHASE_W_NODE --> Q_WL_INV Q_UH_INV --> MOTOR_TERM_U["Motor Terminal U"] Q_UL_INV --> GND_INV Q_VH_INV --> MOTOR_TERM_V["Motor Terminal V"] Q_VL_INV --> GND_INV Q_WH_INV --> MOTOR_TERM_W["Motor Terminal W"] Q_WL_INV --> GND_INV end subgraph "SiC Gate Drive System" SIC_DRIVER_UH["High-Side Driver U"] --> Q_UH_INV SIC_DRIVER_UL["Low-Side Driver U"] --> Q_UL_INV SIC_DRIVER_VH["High-Side Driver V"] --> Q_VH_INV SIC_DRIVER_VL["Low-Side Driver V"] --> Q_VL_INV SIC_DRIVER_WH["High-Side Driver W"] --> Q_WH_INV SIC_DRIVER_WL["Low-Side Driver W"] --> Q_WL_INV subgraph "Drive Power Supplies" ISO_PWR_U["Isolated Power Supply U"] ISO_PWR_V["Isolated Power Supply V"] ISO_PWR_W["Isolated Power Supply W"] end ISO_PWR_U --> SIC_DRIVER_UH ISO_PWR_U --> SIC_DRIVER_UL ISO_PWR_V --> SIC_DRIVER_VH ISO_PWR_V --> SIC_DRIVER_VL ISO_PWR_W --> SIC_DRIVER_WH ISO_PWR_W --> SIC_DRIVER_WL PWM_CONTROLLER["PWM Controller"] --> SIC_DRIVER_UH PWM_CONTROLLER --> SIC_DRIVER_UL PWM_CONTROLLER --> SIC_DRIVER_VH PWM_CONTROLLER --> SIC_DRIVER_VL PWM_CONTROLLER --> SIC_DRIVER_WH PWM_CONTROLLER --> SIC_DRIVER_WL end subgraph "Protection & Filtering" DC_LINK["DC-Link Capacitors"] --> DC_POS SNUBBER_NETWORK["RC Snubber Network"] --> PHASE_U_NODE TVS_GATE["Gate TVS Protection"] --> SIC_DRIVER_UH CURRENT_SHUNT["Current Sense Shunt"] --> GND_INV end style Q_UH_INV fill:#e8f5e8,stroke:#4caf50,stroke-width:2px style Q_VH_INV fill:#e8f5e8,stroke:#4caf50,stroke-width:2px style Q_WH_INV fill:#e8f5e8,stroke:#4caf50,stroke-width:2px

Intermediate Voltage DC-DC Converter Topology Detail

graph LR subgraph "Multi-Phase Buck Converter" INPUT_800V["800V DC Input"] --> INDUCTOR_L1["Input Filter Inductor"] INDUCTOR_L1 --> SW_NODE_1["Switching Node 1"] INDUCTOR_L1 --> SW_NODE_2["Switching Node 2"] INDUCTOR_L1 --> SW_NODE_3["Switching Node 3"] subgraph "High-Side Switches" Q_HS1["VBGQA3610 Ch1
High-Side"] Q_HS2["VBGQA3610 Ch1
High-Side"] Q_HS3["VBGQA3610 Ch1
High-Side"] end subgraph "Low-Side Switches" Q_LS1["VBGQA3610 Ch2
Low-Side"] Q_LS2["VBGQA3610 Ch2
Low-Side"] Q_LS3["VBGQA3610 Ch2
Low-Side"] end SW_NODE_1 --> Q_HS1 SW_NODE_1 --> Q_LS1 SW_NODE_2 --> Q_HS2 SW_NODE_2 --> Q_LS2 SW_NODE_3 --> Q_HS3 SW_NODE_3 --> Q_LS3 Q_HS1 --> PHASE_INDUCTOR1["Phase Inductor 1"] Q_HS2 --> PHASE_INDUCTOR2["Phase Inductor 2"] Q_HS3 --> PHASE_INDUCTOR3["Phase Inductor 3"] PHASE_INDUCTOR1 --> OUTPUT_CAP["Output Capacitors"] PHASE_INDUCTOR2 --> OUTPUT_CAP PHASE_INDUCTOR3 --> OUTPUT_CAP OUTPUT_CAP --> OUTPUT_48V["48V/60V Output Bus"] Q_LS1 --> GND_CONV Q_LS2 --> GND_CONV Q_LS3 --> GND_CONV end subgraph "Control & Driving" MULTIPHASE_CTRL["Multi-Phase Controller"] --> GATE_DRV1["Gate Driver 1"] MULTIPHASE_CTRL --> GATE_DRV2["Gate Driver 2"] MULTIPHASE_CTRL --> GATE_DRV3["Gate Driver 3"] GATE_DRV1 --> Q_HS1 GATE_DRV1 --> Q_LS1 GATE_DRV2 --> Q_HS2 GATE_DRV2 --> Q_LS2 GATE_DRV3 --> Q_HS3 GATE_DRV3 --> Q_LS3 OUTPUT_48V -->|Voltage Feedback| MULTIPHASE_CTRL CURRENT_MON["Current Monitoring"] --> MULTIPHASE_CTRL end subgraph "Thermal Management" THERMAL_VIA["Thermal Via Array"] --> Q_HS1 PCB_HEATSPREAD["PCB Heat Spreader"] --> Q_LS1 COOLING_FAN["Cooling Fan"] --> PCB_HEATSPREAD end style Q_HS1 fill:#e3f2fd,stroke:#2196f3,stroke-width:2px style Q_LS1 fill:#e3f2fd,stroke:#2196f3,stroke-width:2px

Intelligent Load Switch & Safety System Topology Detail

graph LR subgraph "Safety-Critical Load Switching Channels" POWER_RAIL["48V Auxiliary Power Rail"] --> LOAD_SWITCH1["VBQG8218
Channel 1"] POWER_RAIL --> LOAD_SWITCH2["VBQG8218
Channel 2"] POWER_RAIL --> LOAD_SWITCH3["VBQG8218
Channel 3"] POWER_RAIL --> LOAD_SWITCH4["VBQG8218
Channel 4"] subgraph "Control Interface" MCU_GPIO["Flight MCU GPIO"] --> LEVEL_SHIFTER["Level Shifter"] LEVEL_SHIFTER --> GATE_CTRL1["Gate Control 1"] LEVEL_SHIFTER --> GATE_CTRL2["Gate Control 2"] LEVEL_SHIFTER --> GATE_CTRL3["Gate Control 3"] LEVEL_SHIFTER --> GATE_CTRL4["Gate Control 4"] end GATE_CTRL1 --> LOAD_SWITCH1 GATE_CTRL2 --> LOAD_SWITCH2 GATE_CTRL3 --> LOAD_SWITCH3 GATE_CTRL4 --> LOAD_SWITCH4 LOAD_SWITCH1 --> AVIONICS_PWR["Avionics Power Rail"] LOAD_SWITCH2 --> COMM_PWR["Communication Power Rail"] LOAD_SWITCH3 --> CHEM_SENSOR_PWR["Chemical Sensor Power"] LOAD_SWITCH4 --> SAFETY_PWR["Safety System Power"] AVIONICS_PWR --> FLIGHT_SENSORS["Flight Sensors"] COMM_PWR --> RADIO_MODULE["Radio Module"] CHEM_SENSOR_PWR --> GAS_SENSORS["Gas Detection Sensors"] SAFETY_PWR --> INTERLOCK_SOL["Interlock Solenoid"] end subgraph "Protection & Monitoring" subgraph "Channel Protection" TVS_LOAD["TVS Diode"] --> AVIONICS_PWR ZENER_GATE["Gate-Source Zener"] --> GATE_CTRL1 SERIES_RES["Series Resistor"] --> GATE_CTRL1 EFUSE["eFuse IC"] --> COMM_PWR end subgraph "Fault Detection" CURRENT_SENSE_LOAD["Current Sense Amplifier"] --> AVIONICS_PWR VOLTAGE_MON["Voltage Monitor"] --> CHEM_SENSOR_PWR COMPARATOR["Comparator"] --> FAULT_SIGNAL["Fault Signal"] CURRENT_SENSE_LOAD --> COMPARATOR VOLTAGE_MON --> COMPARATOR FAULT_SIGNAL --> MCU_GPIO end end subgraph "Redundant Power Architecture" REDUNDANT_RAIL["Redundant Power Rail"] --> LOAD_SWITCH5["VBQG8218
Redundant Channel"] LOAD_SWITCH5 --> REDUNDANT_AVIONICS["Redundant Avionics"] MCU_GPIO --> GATE_CTRL5["Redundant Control"] GATE_CTRL5 --> LOAD_SWITCH5 end style LOAD_SWITCH1 fill:#fff3e0,stroke:#ff9800,stroke-width:2px style LOAD_SWITCH5 fill:#fff3e0,stroke:#ff9800,stroke-width:2px
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