Aircraft PDU Enclosure

Electrical distribution failures in aircraft power systems interrupt critical avionics and flight control equipment threatening mission completion and passenger safety. Aircraft PDU Enclosure provides lightweight housings for power distribution units, solid-state power controllers, and circuit protection devices. 
HY D R O L Y SIS RESIS T ANCE
Material & Grade
  • Aluminum Alloy – 6061-T6, 7075-T6
  • Aerospace-grade aluminum
  • Magnesium Alloy – AZ91D
  • Lightweight high-strength materials
  • Sheet thickness – Up to 3.0mm capable
  • Maximum capable – 600mm (H) x 500mm (W) x 300mm (D)
  • Customizable based on power distribution requirements
  • Anodizing – MIL-A-8625 Type II, Type III
  • Chromate Conversion Coating – MIL-DTL-5541
  • Powder Coating – Aerospace-grade
  • Corrosion-resistant finish
  • Conductive coating provisions
  • CNC Precision Machining (±0.025mm)
  • CNC Laser Cutting
  • TIG Welding (aerospace-grade)
  • CNC Press Brake Forming
  • Busbar mounting provisions
  • Weight reduction optimization
  • Aerospace-grade fasteners (AN/MS standards)
  • Titanium hardware (weight reduction)
  • Arc flash protection provisions
  • Grounding provisions
  • Circuit breaker mounting hardware
  • Self-locking nuts (vibration-resistant)

Product Description

Aircraft-mounted configurations accommodate distribution hardware with external dimensions reaching 600mm while minimizing structural weight penalties. We engineer aerospace-grade aluminum construction balancing electromagnetic compatibility with strict weight limitations critical for aircraft performance. Through organized busbar routing and thermal management, these enclosures enable reliable power distribution supporting commercial and military aviation. 

Mounting Type
  • Aircraft fuselage mounting
  • Avionics bay integration
  • Ceiling/Floor mounting provisions
  • Vibration-isolated mounting
  • Quick-release mechanisms
  • Structural frame attachment
  • Input voltage – 28V DC, 115V AC (400Hz), 230V AC (400Hz)
  • Current capacity – Up to 400A
  • Power rating – Up to 50kW
  • Busbar provisions
  • High-current distribution
  • Multiple voltage outputs
  • Multiple circuit provisions (10-30 outputs)
  • Load management capability
  • Sequential power-up control
  • Individual circuit protection 
  • Remote switching provisions
  • Backup power integration
  • Voltage monitoring 
  • Current sensing provisions 
  • Power quality monitoring 
  • Load status indication 
  • Data bus integration (ARINC 429) 
  • Fault indication systems
  • Circuit breaker provisions (thermal/magnetic) 
  • Solid-state power controller (SSPC) integration
  • Overcurrent protection
  • Short circuit protection 
  • Arc fault detection
  • Ground fault protection
  • ISO 9001:2015 Manufacturing
  • AS9100 (Aerospace Quality Management) 
  • RTCA DO-160 (Environmental Testing)
  • MIL-STD-810 (Environmental Engineering) 
  • SAE AS50881 (Wiring Aerospace Vehicle)
  • FAA TSO certification (application-specific)
  • RoHS Compliant

Technical Advantages

High-current busbar connections require precision torque specifications preventing loose connections that create heat and arc flash hazards. Addressing this critical requirement, silver-plated copper busbars minimize resistance reducing thermal losses during continuous high-power distribution. Thermal interface materials transfer heat from solid-state power controllers to enclosure walls improving convective cooling. 

Sequential power-up control prevents generator inrush current during system startup requiring logic coordination across multiple circuit branches. Microprocessor-based load management sequences circuit closures preventing simultaneous energization that could trip generator current limiters. Moreover, data bus integration enables centralized monitoring transmitting circuit status and fault conditions to cockpit displays. 

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Industry Applications

Commercial Aviation

Houses primary and secondary power distribution units managing 115V AC and 28V DC electrical systems in passenger aircraft.

Military Aircraft

Contains tactical electrical distribution equipment coordinating mission system power in fighter jets and transport aircraft. 

Business Aviation

Protects power distribution modules managing avionics, cabin systems, and galley loads in corporate jets. 

Unmanned Aerial Systems

Secures compact power distribution units supplying payload equipment and flight control systems in military drones. 

Helicopter Operations

Manages electrical distribution in weight-sensitive rotary-wing platforms requiring optimized power system efficiency. 

Aircraft Modernization

Consolidates upgraded power distribution during avionics retrofit programs replacing aging electromechanical contactors. 

Aircraft PDU Enclosure

Designed for Aircraft Power

PDU configurations vary from simple circuit breaker panels to sophisticated systems with solid-state switching and load shedding automation. Frigate manufactures Aircraft PDU Enclosures meeting RTCA DO-160 qualification with complete arc fault and overcurrent testing documentation. 

Vibration-resistant mounting provisions maintain secure installation during flight operations and turbulence preventing connection failures. Quick-release mechanisms enable rapid PDU replacement during line maintenance supporting minimum equipment list compliance. 

Aircraft PDU Enclosure

Having Doubts? Our FAQ

Check all our Frequently Asked Questions

Can silver-plated copper busbars in Aircraft PDU Enclosures minimize resistance reducing thermal losses during continuous high-power distribution?

Silver-plated copper busbars are commonly used to lower contact resistance and manage heat rise under continuous load conditions. Frigate manufactures Aircraft PDU Enclosures with busbar interfaces prepared for silver plating when specified, allowing efficient current transfer while supporting long-duration power distribution requirements. 

How does Frigate integrate thermal interface materials in Aircraft PDU Enclosures transferring heat from solid-state power controllers?

Effective heat transfer from solid-state devices requires controlled mechanical interfaces, and Frigate supports this through – 

  • Machined contact surfaces prepared for thermal pads or greases 
  • Consistent clamping pressure across power device mounting zones 
  • Enclosure layouts that conduct heat toward external mounting structures 

Thermal interface selection and placement are typically adjusted based on controller type and dissipation levels. 

Are microprocessor-based load management systems effective sequencing circuit closures preventing simultaneous energization?

Load sequencing logic is widely used to limit inrush currents and protect upstream power sources. Frigate builds Aircraft PDU Enclosures that accommodate microprocessor-based load management hardware, with internal layouts and mounting provisions aligned to system-level sequencing and protection strategies. 

How does Frigate engineer data bus integration in Aircraft PDU Enclosures enabling centralized monitoring transmitting circuit status?

Centralized monitoring depends on reliable data connectivity, and Frigate enables this by incorporating – 

  • Shielded routing paths for data bus cabling 
  • Connector cutouts aligned to ARINC or proprietary interfaces 
  • Internal separation between power and communication sections 

Bus interface locations and connector types are commonly customized based on aircraft architecture. 

Does vibration-resistant mounting maintain secure installation during flight operations preventing connection failures?

Aircraft vibration environments demand robust mechanical retention, and Frigate addresses this using – 

  • Reinforced mounting points rated for airborne vibration spectra 
  • Hardware retention features preventing fastener loosening 
  • Structural stiffness that limits relative motion between components 

Mounting strategies are adapted based on installation zone and vibration severity. 

How does Frigate address quick-release mechanisms in Aircraft PDU Enclosures enabling rapid PDU replacement supporting MEL compliance?

Rapid replacement capability reduces aircraft downtime, and Frigate supports this through – 

  • Quick-release fastener provisions accessible from service zones 
  • Connector alignment features simplifying reconnection 
  • Mechanical guides that control insertion and removal paths 

Release mechanisms are typically selected based on maintenance access requirements. 

Can arc flash protection provisions contain internal faults preventing external damage to adjacent aircraft systems?

Arc fault containment relies on enclosure strength and controlled venting paths. Frigate manufactures Aircraft PDU Enclosures with structural features and material thicknesses defined to manage internal fault energy, helping limit propagation to surrounding aircraft systems when specified by the protection philosophy. 

How does Frigate validate RTCA DO-160 qualification in Aircraft PDU Enclosures with complete arc fault testing documentation?

Environmental qualification depends on consistent fabrication and traceability. Frigate supports RTCA DO-160 compliance by manufacturing Aircraft PDU Enclosures to defined test configurations and maintaining documentation such as material records, assembly details, and test correlation data required for certification programs. 

Are solid-state power controller integration provisions compatible with load shedding automation in overload scenarios?

Automated load shedding requires coordinated electrical and mechanical integration, and Frigate accommodates this by providing – 

  • Dedicated mounting zones for solid-state power controllers 
  • Wiring separation supporting control and sensing functions 
  • Space allocation for monitoring and protection circuitry 

Controller integration details are typically aligned to the selected load shedding strategy. 

How does Frigate optimize weight reduction in Aircraft PDU Enclosures balancing electromagnetic compatibility with aircraft weight limitations?

Weight optimization is achieved through careful material use and fabrication control, and Frigate applies – 

  • Precision machining to remove non-structural mass 
  • Selective reinforcement only at load-bearing regions 

Weight-saving measures are commonly tailored based on EMC targets and installation constraints. 

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LOCATIONS

Registered Office

10-A, First Floor, V.V Complex, Prakash Nagar, Thiruverumbur, Trichy-620013, Tamil Nadu, India.

Operations Office

9/1, Poonthottam Nagar, Ramanandha Nagar, Saravanampatti, Coimbatore-641035, Tamil Nadu, India. ㅤ

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LOCATIONS

Registered Office

10-A, First Floor, V.V Complex, Prakash Nagar, Thiruverumbur, Trichy-620013, Tamil Nadu, India.

Other Locations

GENERAL ENQUIRIES

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Aircraft PDU Enclosure

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