Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 601 - 650 out of 867

Document Document Title
JP5705909B2
The present invention broadly comprises an aircraft motion control auxiliary power unit suspension system device, the aircraft motion control auxiliary power unit suspension system device comprising a first motion control nonelastomeric ...  
JP2015077070A
To provide a solid state primary power switching network for modular equipment centers (MECs) distributing primary power throughout a vehicle.The solid state primary power switching network includes multiple primary power switch network ...  
JP2015074449A
To provide a composite vehicle architecture without a current return network for reducing lightning threats.A plurality of modular equipment centers (MECs) 44 are spatially distributed throughout a vehicle 10. Equipment loads 50 within t...  
JP2015077068A
To provide a plurality of modular equipment centers (MECs) spatially distributed throughout a vehicle servicing equipment loads.Each MEC independently provides localized power and communication to service the equipment loads and each equ...  
JP2015511199A
It is a device for supplying air to the auxiliary power unit (GAP) of an airplane, and is the above-mentioned auxiliary power unit, It has a diesel engine (M) combined with a turbocharger (TC), and is the above-mentioned turbocharger, It...  
JP2014516324A5  
JP2015053848A
To provide a reduced-weight power supply system suitable for use on an aircraft.A universal power converter 15 is configured to receive unregulated DC power from a fuel cell 20. The output of the fuel cell 20 is provided to the input of ...  
JP2015047934A
To provide an electric actuator driving device for an aircraft, which can supply high power to an electric actuator while suppressing upsizing of an electric motor.An aileron driving device 40 includes an electric actuator 41 and a flywh...  
JP2015047935A
To provide an electric power system for an aircraft, which can supply high power to a load while suppressing upsizing of an electric motor and the like.An electric power system 1 for an aircraft includes a high-voltage bus 14 for FCS, wh...  
JP2015043687A
To provide a reliable aircraft engine constant frequency starter/generator.A constant frequency starter/generator 55 for a turbine engine includes a first inverter/converter 56, a second inverter/converter 60, a DC link 58 electrically c...  
JP2015038349A
To provide a performance detection unit for determining that the performance of a fuel oil unit in an APU is in a stable phase, a decline phase, a serious decline phase or a failure phase.The invention relates to a method for performance...  
JP2015038348A
To provide a monitoring method with respect to the failure of turbine vane fracture and rotating shaft blocking.The invention relates to a monitoring method and device with respect to the failure of turbine blade fracture and rotating sh...  
JP2015038347A
To provide a performance detection device of a starter in an auxiliary power unit APU of an aircraft.The invention relates to a detecting method for the performance of a stater in an auxiliary power unit APU. The method comprises the ste...  
JP2015038346A
To provide a monitoring method of a lubricating oil cooler in an auxiliary power unit of an aircraft.The invention relates to a method for performance detection of a lubricating oil cooler in an auxiliary power unit APU, and comprises th...  
JP2015030448A
To provide a method for properly carrying out a load jet in an aircraft to maintain power supply to more pieces of apparatuses.The method for load jet comprises a failure detection step S1 for detecting a failure of a power generator and...  
JP2015025451A
To provide a method and a device for monitoring turbine efficiency of an auxiliary power unit of an airplane.A method for detecting performance of turbine efficiency of an auxiliary power unit APU of an airplane, includes the steps of: a...  
JP2015019566A
To provide a method and apparatus for establishing a validated stable design for a stable electrical power system.An initial design 412 for an electrical power system is established. The initial design 412 for the electrical power system...  
JP2015011987A
To provide a truss interconnect.An interconnect for transferring signals herein includes one or more signal contacts to transfer power or data to or from an integrated truss system. The interconnect may be configured to transfer power or...  
JP2014534122A
It is the present invention for the purpose of optimizing resources required when at least one main engine is lost, in order to continue a flight, Additional generating of the non-promoting power operated continuously aims at reducing al...  
JP2014533624A
The single architecture is used for the present invention and it relates to the optimal recovery of energy in an airplane in a fight level and terrestrial both. For that purpose, the object of the present invention is to collect thermal ...  
JP5634086B2
The present invention relates generally to electrical power distribution, for example, in aircraft. More particularly, according to a first aspect, the present invention relates to a power supply system 100 for power distribution to one ...  
JP2014528233A
[Means for Solution] 2 member device for supporting and holding a bunch (65) of a cable or an electric wire in a channel (60) possesses a support member (10) in which a thin long crevice (16) for cable ties (64) was formed and which has ...  
JP2014502836A5  
JP2014193711A
To provide methods of accurately reading hydraulic fluid levels in tanks regardless of change in the hydraulic fluid levels during movement of the aircraft including taxi, takeoff, landing, and flight.A method 100 of monitoring hydraulic...  
JP2014525873A
An electrical power supply device for an aircraft on the ground, the device including two electricity generators driven by an auxiliary power unit, wherein the first generator is connected by a selective connection/disconnection mechanis...  
JP5597876B2  
JP2014159212A
To provide a lithium battery system for aircrafts or the like which prevents transmission of an impact to the body of the lithium battery body and does not cause ignition.A lithium battery 7 is held to the airframe or an outer case 13 wi...  
JP5568129B2  
JPWO2012137843A1
The gearbox (22) which is a power generator (1) which can control that the front area of the engine for airplanes increases, and is connected with the engine axis of rotation, The input axis (27) which has the axial center which met in t...  
JPWO2012137843A
A gearbox (22) which is a power generator (1) which can control that front area of an engine for airplanes increases, and is connected with the engine axis of rotation, An input axis (27) which has the axial center which met in a dynamo ...  
JP2014516324A
Vehicles, systems, and methods are disclosed for providing and directing first power, such as vehicle generator power, and alternate sources of power. In a particular embodiment, a vehicle includes a power distribution grid that includes...  
JP2014516004A
A chain of components for transmitting electric power of an aircraft includes an auxiliary power unit (APU), main engines and end consumer systems via power networks and electronic connections controlled by a unit. The APU supplies power...  
JP5524850B2
The present invention broadly comprises an aircraft motion control auxiliary power unit suspension system device, the aircraft motion control auxiliary power unit suspension system device comprising a first motion control nonelastomeric ...  
JP2014513511A
A generation method performed by a generator module of an electricity network of an aircraft, the electricity network including a power supply line powered by the generator module, a DC bus powered from the power supply line via a rectif...  
JP2014096978A
To provide a method and apparatus for electrical power system stability optimization.An electrical power system 100 comprising source elements 109 and load elements 111 is simulated to generate impedance data, where the impedance data id...  
JP2014091514A
To provide a ram air turbine generator system that has a decreased number of parts and can increase reliability.A ram air turbine generator system 12 for generating electrical power when exposed to an external airstream of aircraft inclu...  
JP2014078227A
To provide a method for modeling an electrical power system of an aircraft.A method 100 of modeling an electrical power system of an aircraft comprises: among others, identifying electrical characteristics 110, mechanical characteristics...  
JP5450048B2  
JP5421216B2
The network (10) has a three-phase power bus (11) conveying three-phase alternating current (AC) power generated by one direct current (DC)/AC converter (12) that is powered by a DC source of an aircraft. The DC/AC converter is fitted wi...  
JP2014503404A
A method and architecture processing electrical energy regenerated from an aircraft, to address drawbacks posed by customary solutions for dissipating low energy of resistors, conventionally ceramics, which require a significant volume o...  
JP2014502836A
Disclosed are methods, systems and apparatuses for harvesting vibrational energy from vehicles, as well as methods for locating vibrational energy on a vehicle. One harvesting apparatus comprises a vibrational energy harvester coupled to...  
JP2014502835A
A module converting voltage between a high-voltage electrical network and at least one energy storage element an aircraft, the conversion module configured to reversibly convert between a DC voltage of the high-voltage electrical network...  
JP2014501875A
Especially the present invention reduces consumption of electric power in a changes stage, and relates to a method of improving acceleration efficiency of a gas generator of a gas turbine, by [of an operation line / big enough] carrying ...  
JP5385145B2  
JP5385127B2
The device has air conditioning plants (ECS1-ECS4) utilized as emergency electric generators. The plants compress air coming from the exterior of an aircraft e.g. civil transport plane. Air compressors of the plants are driven by electri...  
JP2013545649A
An aircraft system comprising a fuel storage system comprising a first fuel tank capable of storing a first fuel and a second fuel tank capable of storing a second fuel is disclosed herein. The aircraft system further comprises a fuel ce...  
JP5373596B2
A device and a method for emergency electricity supply on board an aircraft, able to supply a part of the aircraft's electrical power circuit. The device includes a synchronous machine with separate excitation, associated with a flywheel...  
JP2013251264A
To provide an electrical power unit that provides electrical power to an electrical component on-board an aircraft in an emergency situation.An electrical power unit provides electrical power to an electrical component 12 on-board an air...  
JP2013512821A5  
JP2013220681A
To provide an auxiliary power system capable of effectively using hot water produced by a fuel cell type auxiliary power supply device.An auxiliary power system has a fuel cell type auxiliary power supply device 2. Hot water X produced w...  

Matches 601 - 650 out of 867