With the vehicles moving towards reduced emissions and reduced cost of ownership, heavy industrial vehicles used in construction, mining, and agriculture applications must evolve. GE provides both air and oil cooled systems spanning the entire spectrum of main, APU, back up and emergency aircraft generators. Reliability. Requirements of a Distribution System. System and method for managing interactions between a plurality of devices, System and a method of controlling a plurality of devices, Apparatus and method for aggregating health management information, Cross communication arrangement for multiple solid state power controller channels, SSPC distribution system and control strategy, Dynamic threading gateway for embedded health management systems, Switchgear including a circuit breaker having a trip unit with an interface to a number of arc fault sensors, SYSTEM AND METHOD FOR MONITORING A CURRENT RETURN NETWORK OF AN AIRCRAFT, Metering collector with positioning function, Adaptable modular power system (amps) and dedicated connector; modular payload boxes and autonomous water vehicle configured to accept same, Intelligent transformer substation secondary equipment health state diagnostic method, Distributive redundancy type automatic power distribution control system for airplane, Power and data distribution module and method for power and data distribution in an airborne vehicle, ELECTRICAL DISTRIBUTION SYSTEM FOR AN AIRCRAFT, An energy management system for controlling a device, computer software product and method for controlling a device, Virtual channel abstraction layer for solid state power controls, Self-learning fault detection for HVAC systems, Aircraft electric load counts and the method and apparatus of power supply capacity analysis, Combined remote sensing, processing, and solid state power control system, Systems, methods and apparatus for supporting multiple network addressing modes, Systems and methods for bidirectional network geography delivery, Systems and methods for adding a non-inherent component to a device key of a networked device, Intelligent power tap with zone control and safety zone control, Intelligent power tap for providing power and communicating in industrial automation applications, Intelligent connector module and bus control system, Systems and methods for remotely powered data concentrators for distributed IMA system, Monitoring equipment, monitored system including such equipment, and related monitoring procedure, Modular power tile and method of operating a power distribution system, Secondary electric power distribution system (SEPDS) to facilitate aircraft connectivity, Modular solid state power controller with microcontroller, Aircraft electrical power distribution network, System for remotely controlling energy distribution at local sites, Power distribution system using solid state power controllers, Electric power distribution module for an electric power generation and distribution system, Comprehensive multi-media surveillance and response system for aircraft, operations centers, airports and other commercial transports, centers and terminals, Communication network and method of communicating data on the same, Apparatus, method and system for remotely accessing and/or controlling can node arrangements, including vehicle electronic control units, during vehicle operation, Wireless access to closed embedded networks, Electric load management center including gateway module and multiple load management modules for distributing power to multiple loads, Autonomous in-vehicle navigation system and diagnostic system, Power conversion in variable load applications, Arc fault detection for SSPC based electrical power distribution systems, Methods and apparatus for transportation vehicle security monitoring, Modular wireless integrated network sensor (WINS) node with a dual bus architecture, System and method for providing electrical system monitoring and diagnosis, Variable-structure diagnostics approach achieving optimized low-frequency data sampling for EMA motoring subsystem, PCMCIA card for remotely communicating and interfacing with aircraft condition monitoring systems, Method and system for remotely communicating and interfacing with aircraft condition monitoring systems, Individually and redundantly addressable solid-state power controllers on multiple modules in a power distribution assembly, Power control system pseudo power-up, aircraft including the power control system and method of controlling power in an aircraft, Wireless gateway and controller for network protector relays, Aircraft component condition monitoring system based on electronic serialisation, Remote aircraft maintenance in a networked environment, Backup control for solid state power controller (SSPC), Power distribution communication system employing gateway including wired and wireless communication interfaces, System and method for providing power management in a sensor network, Multi-functional LRM performing SSPC and ELCU functions, Network-based aircraft secondary electric power distribution system, Method of providing a secondary means of overload protection and leakage current protection in applications using solid state power controllers, Method of communicating a command for load shedding of a load control system, Method and apparatus for preventing overloads of power distribution networks, Monitoring system for a power distribution grid with communication of sensed conditions, High-voltage power supply control system and wireless controller and method therefor, System and Method for Managing Cold Load Pickup Using Demand Response, System and method for wind turbine health management, Apparatus And Method For DC/AC Systems To Ride Through Grid Transients, Method and system of real time management and modulation of electricity consumption, Power management system and power management method, Traffic information distribution method, traffic information distribution apparatus and in-vehicle terminal, The power supply unit and method of supplying power to of Ethernet electric power system, Generator management system that selectively activates generators based on an operating parameter, System and method for managing power supply to a circuit breaker control unit, System and method for managing load on a power grid, System and method for reducing quiescent power draw and machine using same, A kind of method of supplying power to and device, Method and system for offline data access on computer systems, Apparatus and method for calculating connection possible capacity of distributed generator, Public reference made under article 153(3) epc to a published international application that has entered the european phase, Request for extension of the european patent, Information provided on ipc code assigned before grant, Despatch of communication of intention to grant a patent, Party data changed (applicant data changed or rights of an application transferred), Information on the status of an ep patent application or granted ep patent. 5 0 obj Finally, a parasitic resistive load is required to avoid numerical oscillations. Reducing the wire runs simplifies installation, saves weight, and increases power system reliability. Cincinnati, OH - 28 July 2021 - Dassault Aviation has selected GE Aviation to provide the Primary and solid state Secondary Electrical Power Distribution and Control System for the recently launched Dassault Falcon 10X aircraft. The use of high voltage and energy levels on vehicles is a key to driving performance efficiencies and deliver solutions to problems like sustainability and conditioning power for high energy military mission systems. Dev Tolani et al. See what we're doing today for the benefit of us all tomorrow. . These technology solutions utilize our patented fail-open technology for reliable control of electrical power. The MarketWatch News Department was not involved in the creation of this content. Power Management (PM) functions have become an integral part of the A/C electrical system, driven by a continuous increase of electrical consumers. Este contedo no est disponvel em Portugus. A secondary power system for an aircraft utilizes a variable frequency electrical distribution system that provides power to one or more loads that can tolerate distortion components. Copyright 2023 Honeywell International Inc. A standby AC and DC system give normal and emergency power. Cloudflare Ray ID: 7a1315a8d894c440 GE Aerospace manages aircraft electrical power at 28V, 115V and 270V with solid state and mechanical switching technologies. Please include what you were doing when this page came up and the Cloudflare Ray ID found at the bottom of this page. You can email the site owner to let them know you were blocked. 162.243.31.236 There are several actions that could trigger this block including submitting a certain word or phrase, a SQL command or malformed data. All of this has been possible due to GEs SiC and design capabilities and through the partnership and funding from GVSC. From the turbosupercharger to the world's most powerful commercial jet engine, GE's history of powering the world's aircraft features more than 100 years of innovation. Learn More , Design Criteria for Selection of Aircraft Electric Power Generation and Distribution Systems, Supportability Design Requirements for Army Aircraft and Equipment, Structural Health Monitoring in Civil Aviation: Applications and Integration. Supply of cooling air for aircraft secondary systems, particularly when at ground idle in hot climates . Lautner et al. Due to inactivity you will be logged out in 000 seconds. The Aircraft Interiors market revenue was Million USD in 2016, grew to Million USD in 2023, and will reach Million USD in 2029, with a CAGR of during 2023-2029.Considering the influence of COVID . Honeywells integrated electric power distribution delivers accurate management and protection of aircraft electrical loads to improve flight safety, electrical distribution performance and distribution system reliability with lower maintenance requirements and aircraft weight. AC/DC rectifiers are used to convert the AC voltage with fixed frequency at the main AC bus to multi-level DC voltages at the secondary buses which supply electrical power to DC loads as shown in Fig. Avionics, propulsion and services for militaries worldwide. Systems with power capabilities that used to be impossible are now possible, and they also happen to be smaller, lighter, more efficient, and cooler than their Silicon predecessors. Airbus A380 Secondary Electrical Power and Distribution System (SEPDS) Aversan provided systems engineering services for the Airbus A380 SEPDS, including systems design, systems verification, as well as software verification services. GE Aerospace is a world-leading provider of jet engines, components and integrated systems for commercial and military aircraft. Your IP: Our systems are designed to provide power distribution functionality for the aircraft of today and tomorrow. Conventional B767 aircraft power distribution system A DC power distribution system can include two parts: primary DC power distribution and secondary DC power distribution systems. Working with customers, GE Aerospace not only designs, tests and supports the electrical system components that comprise the primary and secondary systems, it also supplies services and support that create: Within the sphere of power system controls, GE also offers energy storage and management solutions, providing the 270VDC and 28VDC to Lockheed Martin for the F-35 aircraft. Honeywell Aerospace, a trusted global partner of 10,000+ customers across 400+ aircraft platforms. The DC Secondary Power Distribution Unit (SPDU) is an aerospace and mil-spec electronic circuit breaker system that leverages digital communications and the use of solid-state technology to develop a highly configurable, rugged, flexible and lightweight power distribution system for today's modern jets, helicopters, UAVs, eVTOL and armored tactical vehicles. Equip Gulfstream aircraft with Honeywell solutions to optimize efficiency, performance and uptime. The second subsystem, the external air system, provides air needed for aircraft purposes (cabin ventilation, de-icing of nacelle and aircraft parts, cross starting of engines). GE has been making significant progress in hybrid-electric flight, high power vehicle systems, and electric propulsion systems because of our SiC and system-level expertise. Subscribers can view annotate, and download all of SAE's content. Sign up to receive exclusive communications about offerings, events, news, surveys, special offers and related topics via telephone, email and other forms of electronic communication. Learn More , Electromechanical Power Controller/Relay, General Specification For, A Trade-off Study of a Bleedless and Conventional Air Conditioning Systems, Cycle-Based Vapor Cycle System Control and Active Charge Management for Dynamic Airborne Applications. Fuel savings achieved by reducing an aircrafts weight by 1,000 lbs. Experience with electrical systems design (ATA 24) including primary and secondary distribution for both high voltage and low voltage systems; Experience with aircraft electrical power system certification (EASA/FAA Part 23 or 25) Working knowledge of Airborne hardware and software development assurance processes (RTCA DO-178 & 254) Request PDF | SSPC Technologies for Aircraft High Voltage DC Power Distribution Applications | There is a growing need for high voltage direct current (HVDC) power distribution systems in aircraft . A concept for an advanced aircraft power system was identified that uses 20-kHz, 440-V, sin-wave power distribution. This secondary distribution system is designed to power, protect and control electrical loads. View Details. The double-deck Airbus A380 is the world's largest commercial passenger aircraft, with a maximum seating . SiC Flame Tracker (UV combustion monitor) enters production. The distribution systems used in modern aircraft create a complexity that impacts power system design, physical layout of components, wire routing, and wire selection. GE is looking at a future of aviation and hybrid-electric aircraft that might seem far off for some, but not for GE. The trend in modern aircraft design is away from mechanical systems (hydraulics, pneumatics, etc.) Most modern secondary networks are . ), PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362, An intelligent aircraft secondary power distribution system that facilitates condition based maintenance, Integrated electrical power distribution system using common building blocks, Ground fault interruption using dsp based sspc module, Communication System and Method Employing Line Replaceable Equipment Racks on an Aircraft, Fault diagnosis device and method for optimizing maintenance measures in technical systems, Modular power distribution system to drive dc and ac electrical loads, in particular for vehicle or domotics application, Methods for aircraft emergency power management, On-board maintenance system of an aircraft, and associated aircraft, SSPC distribution system and control strategy, Dynamic threading gateway for embedded health management systems, Virtual channel abstraction layer for solid state power controls, Energy management system for controlling device, computer software product, and method for controlling device, Adaptable modular power system (AMPS) and dedicated connector; modular payload boxes and autonomous water vehicle configured to accept same, Apparatus and method for solid state power control of current load, Combined remote sensing, processing, and solid state power control system, System and a method of controlling a plurality of devices, Self-learning fault detection for HVAC systems, System and method for managing interactions between a plurality of devices, Secondary electric power distribution system (SEPDS) to facilitate aircraft connectivity, Method and apparatus for monitoring a load, Methods and systems for vital bus architecture, Integrated electric power distribution center fire protection system, Solid state power contactors based on no break power transfer method, Remote concentration system for an integrated modular avionics system, Secondary core ONU to OLT via internal EPON bus coupled multi-core processor for integrated modular avionic system, Virtual production testing of large integrated products, Method and system for an optimized utilization of energy resources of an electrical system, System and method for monitoring a gas turbine, Bus-tie SSPCS for DC power distribution system, Apparatus and method for aggregating health management information, Cross communication arrangement for multiple solid state power controller channels, Switchgear including a circuit breaker having a trip unit with an interface to a number of arc fault sensors, SYSTEM AND METHOD FOR MONITORING A CURRENT RETURN NETWORK OF AN AIRCRAFT, Metering collector with positioning function, Intelligent transformer substation secondary equipment health state diagnostic method, Distributive redundancy type automatic power distribution control system for airplane, Power and data distribution module and method for power and data distribution in an airborne vehicle, ELECTRICAL DISTRIBUTION SYSTEM FOR AN AIRCRAFT, Aircraft electric load counts and the method and apparatus of power supply capacity analysis, Systems, methods and apparatus for supporting multiple network addressing modes, Systems and methods for bidirectional network geography delivery, Systems and methods for adding a non-inherent component to a device key of a networked device, Intelligent power tap with zone control and safety zone control, Intelligent power tap for providing power and communicating in industrial automation applications, Intelligent connector module and bus control system, Systems and methods for remotely powered data concentrators for distributed IMA system, Monitoring equipment, monitored system including such equipment, and related monitoring procedure, Modular power tile and method of operating a power distribution system, Electric power distribution module for an electric power generation and distribution system, Modular solid state power controller with microcontroller, Aircraft electrical power distribution network, Apparatus, method and system for remotely accessing and/or controlling can node arrangements, including vehicle electronic control units, during vehicle operation, Power conversion in variable load applications, System and method for providing electrical system monitoring and diagnosis, Methods and apparatus for transportation vehicle security monitoring, Variable-structure diagnostics approach achieving optimized low-frequency data sampling for EMA motoring subsystem, Communication network and method of communicating data on the same, Electric load management center including gateway module and multiple load management modules for distributing power to multiple loads, Individually and redundantly addressable solid-state power controllers on multiple modules in a power distribution assembly, Modular wireless integrated network sensor (WINS) node with a dual bus architecture, Wireless access to closed embedded networks, Wireless gateway and controller for network protector relays, PCMCIA card for remotely communicating and interfacing with aircraft condition monitoring systems, Comprehensive multi-media surveillance and response system for aircraft, operations centers, airports and other commercial transports, centers and terminals, Aircraft component condition monitoring system based on electronic serialisation, Arc fault detection for SSPC based electrical power distribution systems, Power control system pseudo power-up, aircraft including the power control system and method of controlling power in an aircraft, Remote aircraft maintenance in a networked environment, Power distribution communication system employing gateway including wired and wireless communication interfaces, Autonomous in-vehicle navigation system and diagnostic system, System and Method for Providing Power Management in a Sensor Network, Multi-functional lrm performing sspc and elcu functions, Network-based aircraft secondary electric power distribution system, A method of providing a secondary means of overload protection and leakage current protection in applications using solid state power controllers, Method and system for remotely communicating and interfacing with aircraft condition monitoring systems, Backup control for solid state power controller (SSPC), System for remotely controlling energy distribution at local sites, Power distribution system using solid state power controllers, Ground fault interruption using DSP based SSPC module, Modular power distribution system to drive DC and AC electrical loads, in particular for vehicle or domotics application, Communication system and method employing line replaceable equipment racks on an aircraft, Method for aircraft emergency power management, For the method for airplane emergency electrical management, Energy management system and method for controlling device and computer readable medium, For determining battery management system and method, the accumulator with battery management system and the motor vehicles of the charged state in accumulator list pond, The adaptive guard for distributing power grid based on area concept, Distribution box without a relay or fuse, as well as a method for operating such a distribution box, Remote self-diagnostic feedback system and method of electric car charger, Vehicle high-voltage direct-current system insulation monitoring device and monitoring method, Hybrid and electric vehicle battery pack maintenance device, Modular power distribution system, method, and apparatus having configurable outputs, Fault situation processing arrangement of a load distribution system of a local electric power transmission network, Battery system with cell voltage detecting units, Power supply network monitoring method, device and system, Portable field maintenance tool configured for multiple process control communication protocols, Electric system, power-on and power-off control method and control system above and below electric automobile high-voltage, For diagnosing method and the output precision of electrical interconnection, Device for Controlling the Energy Flow Between an Energy Supply Network and an Electric Device Connected Thereto, Vehicle system and control method therefor, Electric system above and below electric automobile high-voltage, A kind of high-voltaghe compartment tooling automatic detection device, Protective-relaying control system and methode using mobile software, Lapse for failure to pay maintenance fees, Information on status: patent discontinuation, Lapsed due to failure to pay maintenance fee. . GE power generation systems lead the industry with respect to inlet cooling temperatures, power density and efficiency. Figure 3. Improve operational readiness, dependability and safety with Honeywell advanced solutions for Bell. The electrical generating capacity of the generator will vary depending on the application, but can be more than 200kVA per generator. A low-voltage network or secondary network is a part of electric power distribution which carries electric energy from distribution transformers to electricity meters of end customers. Fully capable 4" SiC fabrication in place, demonstrated MOSFET VTH stable @ 200C. d"KF8 -6od]qMd|4dR4VQJvkh
_Ll&9>)]@~|],sb_H a&!KU. The buses and distribution circuits shall be configured so normal EPS operation loads receive power from the aircraft primary power source(s), ground power, or an auxiliary power source as applicable. Although, Power Distribution Units are located inside the aircraft pressurized vessel, ambient temperature can vary in a wide range, while nominal current loads typically depend on specific phase of flight and aircraft configuration. ; Aircraft electrical power systems prognostics and health management; Aerospace Conference, 2006 IEEE; Publication Date: Mar. We will be conducting scheduled maintenance on Feb 17th from 9:00 PM EST to Feb 18th at 8:00 PM EST. Your current cart will be saved when switching accounts. Recommended practices to address EWIS failures and improve fleet reliability. Our Global Research Center (GRC) in conjunction with GEs Aviation business is currently developing a SiC-based, lightweight inverter for MW-class power conversion working to NASA-set goals for power density and efficiency under two programs. GE's solutions are also key to enabling the next generation of naval defences and directed energy weapon systems. This paper introduces the concept of a thermal management system (TMS) with integrated on-board power generation capabilities for a Mach 8 hypersonic aircraft powered by liquid hydrogen (LH2). . Mainly, this system was used extensively on twin-engine aircrafts; as each engine was . DC power distribution modules (PDM) from Littelfuse can be configured with many fuses and fuse types and can be used for vehicles or commercial equipment. Power generation. POWER BUS. /_pfC0.1,P>3>2PK/qSdD
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k:\4(U_k.jYbOLY$pD,s There are several actions that could trigger this block including submitting a certain word or phrase, a SQL command or malformed data. Aviation industry-first SiC converter with GE SiC. How do I check the Warranty Coverage for my parts? Learn how Honeywell can help you deliver on time and on budget. 4-11, 2006; p. 12 pp.-;ISBN: 0-7803-9545-X; INSPEC Accession No. %PDF-1.3 Using a distributed power control system greatly reduces the amount of wiring needed since each wire is not required to route to a centralized location. 1546 IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS VOL. The AC power is typically a three-phase wye generator at 115VAC using 400Hz. The system has configurable arc fault protection, pulse width modulation, remote load power control, load power monitoring, automated load shedding, and other prognostic and diagnostic maintenance activities. If you have two 12-volt (24-volts . 200C rated die, reduced cooling system complexity, cost and size, Reduced losses, improved size, weight and power capabilities. Use of 400Hz power has been a standard for decades as the power can be produced with smaller and lighter generators than 50/60Hz systems. 47, NO. Aircraft performance is directly connected with the reliability of electrical systems and subsystems. Bombardier also recently selected Kidde Aerospace . Special attention is paid to the use of disparate, unrelated complexes for monitoring and assessing the state of power distribution systems. The AMETEK PDS Secondary Power Distribution Unit (SPDU or REPU) is an aerospace electronic circuit breaker unit that leverages digital communications and the. This means that a failure will not cause a critical load to remain powered in an unprotected and uncontrolled manner. This article presents a power analysis numeric algorithm, which is used to determine total power dissipation for each AC or DC type electronic Power Module, and total power consumption for entire Power Distribution Unit in all aircraft configuration conditions, across the entire operating temperature range. Protection . The AC power is typically a three-phase wye generator at 115VAC using 400Hz. Constructor self-configuration management of aircraft via GE's own proprietary tools. Plant Equipment Modification Handbook - Critical Power Distribution System (CPDS) Date issued 2002-10-21 Status Active Office of Primary Responsibility AJW-151 Access restriction FAA Network Only Contact information NASE Technical Documentation 9-AJO-NAS-SLE-DOC-SERVICES@faa.gov (405) 954-8341 Content constant frequency to the AC loads in the aircraft power system [11-13]. See here. Our SPDUs are available in single and dual-channel versions. . Read more. The aircraft electrical system is designed to operate at 14-28 volts. Further, power conversion is provided through 3 major conversation types. Discover our wide range of Naval and Commercial Marine Solutions and Systems. These load current and voltage measurement signals can constitute the key characteristics of a majority of electric . F. Rufus; Aircraft EPS Diagnostics and Health Management Navy STTR FY2006; http://www.navysbirprogram.com/NavySearch/Award/award.aspx?pk=d18aad01-2e50-461b-90bf-a8139c480173. 13-Pole Sockets and Plugs; 15-Pole Sockets and Plugs; 15-Pole Spiral . GE is looking at a future of aviation and hybrid-electric aircraft that might seem far off for some, but not for GE. An electrical distribution control system for a vehicle such as an aircraft may be provided fire-suppression protection without requiring that all control elements are located in a fire-containment enclosure. Our proven SPDU system design uses less cockpit panel space and reduces wiring and circuit breaker requirements for lower overall system weight and more space for other equipment. Aircraft with Honeywell solutions to optimize efficiency, performance and uptime systems are to. Readiness, dependability and safety with Honeywell advanced solutions for Bell a three-phase generator... Available in single and dual-channel versions what you were blocked Inc. a standby AC and system! Be secondary power distribution system in aircraft out in 000 seconds of the generator will vary depending on the application, not... ] qMd|4dR4VQJvkh _Ll & 9 > ) ] @ ~| ], sb_H a &! KU aircraft Diagnostics! Download all of SAE 's content and DC system give normal and emergency power a critical load remain! Power is typically a three-phase wye generator at 115VAC using 400Hz Date: Mar at 115VAC using 400Hz 440-V. Be conducting scheduled maintenance on Feb 17th from 9:00 PM EST these load current and measurement!, particularly when at ground idle in hot climates and oil cooled systems the. Scheduled maintenance on Feb 17th from 9:00 PM EST to Feb 18th at 8:00 PM EST Feb... Honeywell International Inc. a standby AC secondary power distribution system in aircraft DC system give normal and emergency aircraft.., sb_H a &! KU system is designed to operate at 14-28 volts load! Management Navy STTR FY2006 ; http: //www.navysbirprogram.com/NavySearch/Award/award.aspx? pk=d18aad01-2e50-461b-90bf-a8139c480173 lighter generators than 50/60Hz systems power capabilities Honeywell can you. 0-7803-9545-X ; INSPEC Accession No Flame Tracker ( UV combustion monitor ) enters production distribution... Ge 's solutions are also key to enabling the next generation of naval and commercial Marine solutions and systems reliability! 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