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Matches 651 - 700 out of 766

Document Document Title
JP2008532253A
By a present-day airplane, Power for urgent is offered supposing failure of an engine and an oil pressure system using a rum air turbine. This rum air turbine needs complicated and wide range maintenance mechanically from a viewpoint of ...  
JP2008529893A
The 1st bus (24) that the present invention is an electric feed unit for the gas turbine engines of an airplane, and distributes direct current voltage or a volts alternating current to the 1st item of an engine electrical machinery and ...  
JP2008526620A
The present invention relates to use of the energy buffer equipment for supplying energy to the electric consumption apparatus 14 within an airplane, the electric system of an airplane, and the electric power condenser of the buffer elec...  
JP2008521693A
The feed system (100) for the energy supply in an airplane, The engine (101) made to promote an airplane and the fuel cell (102) which supplies electrical energy to an airplane, It has the 1st fuel storage machine (103) that supplies eng...  
JP2008132973A
To provide an auxiliary power unit installable in an aircraft having a cabin, a duct connecting the cabin to the auxiliary power unit, and an airflow control mechanism in the duct.This auxiliary power unit assembly 10 includes the auxili...  
JP2008518828A
This invention is turned to the distributed active flow control ("DAFC") system (220) which maintains the air current which is attached on the wings which are used for an airplane (205) or other same examples of application, and to which...  
JP2008127013A
To provide a power supply system for an aircraft in which an engine section of the aircraft has sufficient electric power utilizable for supplying electric power to an engine and a current consumer build into the peripheral part of the e...  
JP2008114838A
To provide an auxiliary power unit assembly (10) of an embodiment of the technology described in this specification.The auxiliary power unit assembly (10) comprises an auxiliary power unit installable in an aircraft (18) having a cabin (...  
JP2008514485A
The system and method for operating the electric power system of an airplane are indicated. Including the controller by which the electric power system according to one case of the operation of this invention is combined with the auxilia...  
JP2008080934A
To provide a taking-in port door control system for an auxiliary power unit.The auxiliary power unit (APU) (100) is provided with a control device for controlling a position of an APU taking-in port door (138) at starting action of the A...  
JP4068071B2  
JP4044991B2  
JP2008014325A
To provide a method and a system for controlling a continuous variable transmission which does not cause instable control during starting.In this method for controlling the continuous variable transmission 1, the gear ratio of the contin...  
JP2007537084A
Are the fluid pipe system which extracts the laminar flow layer of fluid in the unstable part of a shell, and/or makes fluid blow off an airplane which it has, and a fluid pipe system (26, 19, 18), Using change good eloquence (6, 4), it ...  
JP2007537085A
The present invention relates to the air intake structure which removes the boundary layer in the airplane which has a structure including an air intake side and at least one aerial respiration engine to the critical style domain of a sh...  
JP2007297042A
To provide a power source device in which a large number of electric devices can be power-fed in an aviation engine and/or its environment. The power source device for the aircraft includes first generators (10, 10') driven by the engine...  
JP2007531855A
The gear box (30, 130) which rotates a propeller in the one direction in which it was chosen of the 1st or 2nd direction is offered. The 2nd direction is reverse to the 1st direction. A gear box has the 1st and the gear of the 2nd compos...  
JP2007246083A
To provide a structure for power distribution, reduced in weight more than the conventional structure by utilizing the advantage that specified movable elements are operated in order. In this power distribution structure especially adapt...  
JP2007218253A
To provide an aircraft auxiliary gas turbine for an aircraft which is improved and not for propulsion, and an improved method for operating this kind of engine. The aircraft auxiliary gas turbine engine (10) is not for propulsion and is ...  
JP2007510591A
The method and system which start equipment, such as an airplane driven with a propeller. The system concerning 1 enforcement form of the present invention was connected with the propeller (120), and is equipped with the fixed implement ...  
JP3930413B2
To provide a system capable of supplying power and selectively supplying thrust as required to an aircraft system. This variable cycle boost propulsor system 10 has a core engine 14, a free turbine 30, a fan 34 connected to the free turb...  
JP2007015423A
To provide a power supply system for an airplane 1 of lightweight construction and with a high efficiency.The power supply system S is equipped with main generators GEN1 and GEN2 driven by a propulsive engine 4 of the air plane 1, an aux...  
JP2006518683A
[Subject] The system and method for engine bleeding flow sharing control systems are offered. [Solution means] The bleed air supply pressure power of a control system of receiving bleed air is controlled so that one engine (10) is chosen...  
JP2006518297A
Fire prevention equipment for the oil cooling air (26) in the auxiliary power unit room (10) of an airplane which blocks partially at least that a flame collides with an oil cooling device directly by suiting in case of an indoor fire so...  
JP2006516230A
It is the method and system for providing an airplane system with secondary power. In the one case of the operation, the airplane system architecture for providing an environmental control system with power contains the dynamo combined w...  
JP3803326B2
To provide an auxiliary power device integrally formed with an engine. In the auxiliary power device integrally formed with an engine, the engine 10 has: a high pressure spool including a high pressure compressor 20 connected to a high p...  
JP3793529B2
To integrate environmental control, secondary power and emergency power. An apparatus comprises of a cooling turbine that is coupled to a first rotor of an electromechanical machine and has an input for receiving compressed air or ram ai...  
JP2006062439A
To continuously supply power to apparatuses loaded on a hot-air balloon during flight with a simple structure.The power supply of hot-air balloon for supplying power to apparatuses equipped in the hot-air balloon comprises a thermoelectr...  
JP2006504043A
Equipment for generating water within an airplane using one piece or two or more fuel cells. A complement or completeness is made to substitute for the process currently performed conventionally in the combustion chamber by incorporating...  
JP2005256840A
To provide a method and an apparatus for operating a gas turbine engine used for aircraft propulsion and auxiliary power.An aircraft gas turbine engine assembly (10) contains at least one propelling gas turbine engine (11) equipped with ...  
JP2005507044A
The passivity type cooling system for auxiliary power unit (APU) equipment (10) of an airplane is offered. A system is a thing for the auxiliary power unit which has at least the compressor part (36) and oil cooler (14) of the gas turbin...  
JP2004340148A
To provide a device and a method for decomposition of propellant.The propellant 24 includes ionic salt and additional fuel. A means 42 to decompose most parts of the ionic salt is provided. A means 48 to burn the additional fuel and deco...  
JP2004324639A
To integrate environmental control, secondary power and emergency power.An apparatus comprises of a cooling turbine that is coupled to a first rotor of an electromechanical machine and has an input for receiving compressed air or ram air...  
JP2004232636A
To provide a gas turbine assembly 10 to be used in an aircraft.The gas turbine assembly 10 includes a propulsion gas turbine and an auxiliary power unit 12. The propulsion gas turbine includes a fan 14 and a core engine 11 to generate th...  
JP2004524474A
[Subject] The present invention aims exhaust gas temperature significant at offer of the whirlpool generation equipment which can decrease in number in auxiliary power unit systems, such as a jet engine. [Solution means] In the hand of c...  
JP2004211706A
To provide a device for improving the efficiency and energy output of an electric power device, and its method.The electric power device uses a fuel cell which is constructed to chemically convert combustible fuel into electrical energy....  
JP2003331877A
To provide a method for improving the efficiency and for reducing an exhaust gas in a fuel cell system.In the fuel system wherein air is fed to the negative electrode side and hydrocarbon is fed to the positive electrode side in operatio...  
JP2003304699A
To provide a small-sized light-weight power-generating apparatus which can generate a predetermined power, irrespective of the operating state of a connected prime mover.The power generating apparatus comprises a generator having a rotor...  
JP2003227412A
To provide an auxiliary power device integrally formed with an engine.In the auxiliary power device integrally formed with an engine, the engine 10 has: a high pressure spool including a high pressure compressor 20 connected to a high pr...  
JP2003523298A
(57) The heat source characterized by supplying summary thermal energy, or the flow (30) of a hot exhaust gas, So that electric power may be generated, when thermal energy flows through the above-mentioned thermoelement, at least one 熱...  
JP2003184653A
To provide a system capable of supplying power and selectively supplying thrust as required to an aircraft system.This variable cycle boost propulsor system 10 has a core engine 14, a free turbine 30, a fan 34 connected to the free turbi...  
JP3440287B2
To provide a method and device for driving at constant rate a generator mounted in an aircraft, whereby the generator can be formed into a compact structure having high efficiency and reliability and long life. The AC generator 2 is driv...  
JP2002154490A
To provide a power switching device including an overhead operation console at least having a switching means in an airborne distribution equipment of a helicoputer for switching power from a main distributor to a power consumption devic...  
JP3270845B2
To provide a boundary layer control mechanism for a short takeoff/ landing distance plane without apprehension generating hot circulation while forming a protruded part behind a pilot seat aerodynamically approximated to an optimum shape...  
JP2001334998A
To provide a traveling body with the improved energy efficiency in starting a propulsion engine or in the air-conditioning system in an aircraft.An auxiliary power unit of the aircraft as the traveling body comprises a power source unit ...  
JP2001515825A
(57) In structure including the airplane cabin (10) which has a summary cabin air inlet (20) and a cabin air exit (22), and which can be pressurized, the necessity for engine bleed air in cabin pressurization / ventilation environmental ...  
JP2001234999A
To provide a highly reliable axial force generating device by a simple constitution and to provide a traction transmission using it.This axial force generating mechanism 10 comprises a centrifugal force generating mechanism, a converting...  
JP2001158400A
To provide a method and device for driving at constant rate a generator mounted in an aircraft, whereby the generator can be formed into a compact structure having high efficiency and reliability and long life.The AC generator 2 is drive...  
JP2001130498A
To prevent a hazard by belly landing and a crash accident due to engine trouble. The conventional equipment is exchanged basically with new ones. This operation is performed positively.  
JP2001116499A
To secure initial power by generating electric power in its launching tube in a flying object which gyratingly flies. A self-gyration type initial generator incorporated in an object which gyratingly flies generates electric power by usi...  

Matches 651 - 700 out of 766