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Matches 501 - 550 out of 744

Document Document Title
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
It is a power supply system (210) provided with two dynamos (216, 218) driven by an auxiliary power unit (220) for terrestrial airplanes, and is the 1st dynamo, It is connected to an airplane network (212) and an electric taxiing network...  
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
航空機用エンジンの前面面積が増大するのを 抑制できる発電装置(1)であって、エンジ ンの回転軸に連結される変速機(22)と、 変速機(22)の出力により駆動される...  
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
The means of transport, system, and method for supplying and drawing the 1st electric power and the sources of alternative electric power, such as means-of-transport dynamo electric power, are indicated. In a certain specific embodiment,...  
JP2014516004A
An object of the present invention is to produce the architecture which can rationalize a series of electric components of an airplane. A series of components for transmitting electric power of an airplane, An end-consumer system (ECS) t...  
JP5524850B2  
JP2014513511A
It is a generation method performed by dynamo module (20) of an electric network (1) of an airplane, and the electric network (1) is, A power source line (3) to which electric power is supplied by the dynamo module (20), A preparation an...  
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  
JP2014503404A
The object of the present invention is to usually cancel a fault by a conventional method of low energy loss by a resistor of ceramics. Mass ceramics and an additional power converter are especially required for this method. In order to ...  
JP2014502836A
A method for accumulating vibrational energy from a vehicle, a system, and not only a device but a method for specifying vibrational energy on a vehicle is indicated. One accumulation apparatus is provided with a vibrational energy harve...  
JP2014502835A
The present invention is a high-pressure electric circuit network of an airplane especially a high-voltage-direct-current network, and at least one energy storage element of the airplane, It is related with a module for changing voltage ...  
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  
JP2013545649A
A fuel storage system (10) provided with the 2nd fuel tank (22) in which the 1st fuel tank (21) and 2nd fuel (12) that can store the 1st fuel (11) can be stored, A fuel cell system (400) provided with a fuel cell (401) which can generate...  
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...  
JP5325367B2
An aircraft gas turbine engine assembly (10), including at least one propelling gas turbine engine (11) comprising a core engine (13) and an exhaust (32). The core engine includes at least one turbine (20) for generating thrust for the a...  
JP5325411B2
An embodiment of the technology described herein is an auxiliary power unit assembly (10). The auxiliary power unit assembly (10) includes an auxiliary power unit being installable in an aircraft (18) having a cabin (22), a duct (28) con...  
JP2013538159A
An aircraft power distribution network comprising first and second galvanically isolated power bus bars, and first and second remote data concentrators (RDCs), each RDC having an input/output interface (I/O) and a power supply, the first...  
JP2013538153A
the present invention more generally adapts sizing of the power supply to the power demand of an airplane to the actual power demand of a cabin pressure control system -- the ratio of an airplane -- it is related with restricting an amou...  
JP2013204432A
To provide a motive power device for an aerial-to-ground vehicle which minimizes weight requiring start-up of the motive power device.A motive power device has a gas turbine 10 for flight in the air, a running motor-driven generator 26 w...  
JP2013191545A
To provide a method for efficiently utilizing electricity and/or byproducts generated by a fuel cell utilized by electrical components that are included in aircraft and require electricity to operate.A heat transfer system includes a fue...  
JP5298027B2
A system and method for switching power sources for an aircraft electric brake system is disclosed. The method removes battery power from electric brake actuator controls during flight until landing gear extension occurs. The method util...  
JP2013169972A
To provide an unmanned aerial vehicle (UAV) capable of obtaining energy from an ascending air current and an operation method of the unmanned aerial vehicle.An unmanned aerial vehicle having a gliding capability is provided which include...  
JP2013168358A
To provide a methods for transferring heat produced by a fuel cell module positioned onboard an aircraft.A power generation system onboard an aircraft includes a fuel cell module configured to produce heat. A loop heat pipe module 218 is...  
JP5275976B2  
JP5269780B2  
JP2013154882A
To broadly provide an aircraft motion control auxiliary power unit suspension system device.An aircraft motion control auxiliary power unit suspension system device includes a first motion control nonelastomeric member (36) and a second ...  
JP2013148085A
To provide an accessory gearbox for a gas turbine engine which provides power to larger generators than conventional engines, yet facilitates nacelle packaging.An engine pylon assembly for a gas turbine engine 10 comprises a core nacelle...  
JP2013529567A
An electricity grid (17) on a plane for an electric device (5b) with which the present invention is located in the surroundings of an engine of an airplane, or the engine, It is fixed in an engine of an airplane and related with an elect...  
JP5231149B2  
JP5230636B2
The system has electrical distribution channels (B) e.g. three phase alternating system, for high power loads and electrical distribution channels (G1) for conventional loads e.g. fuel pump. The distribution channels are separated and ar...  
JP2013124097A
To provide a DC distribution system for aircraft.The system includes a DC system bus 20, which is constructed to carry power from a power supply source 14 to a plurality of electric loads 16. The electric load lies aboard an aircraft 10....  
JP5216146B2  
JP2013523529A
A fire in an airplane is detected and art restored from a fire is indicated in this specification. In such art, it receives from many sensors equipped with sensor data by airplane. It judges about whether sensor data has exceeded a prede...  
JP5205362B2
Methods and systems for providing secondary power to aircraft systems. In one embodiment, an aircraft system architecture for providing power to an environmental control system includes an electric generator operably coupled to a jet eng...  
JP2013513518A5  
JP2013517986A
The present invention is an electric drive airplane (11), and is NH.3NH for providing3A tank (13) of a の sake, and NH3An energy source (15, 17, 19, 19', 35, 37) which uses and changes and generates electric energy, It is related with a...  

Matches 501 - 550 out of 744