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Patent Searching and Data


Matches 701 - 750 out of 1,043

Document Document Title
JP4546537B2  
JP2010529352A
[Subject] The object of the present invention is to provide covering material for silence processing added to a level of the surface of an airplane, and a level of the leading edge especially like an air-intake of Nasser of an airplane. ...  
JP4510634B2
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...  
JP2010522296A
The present invention relates to a device (50) for defrosting an air-intake (24) of gas turbines (10), such as a turbo shaft of a helicopter. The present invention essentially [a device] for air-intakes (24) of a gas turbine contains a m...  
JP2010520410A
An engine for airplanes or an air intake duct of other devices has a warm temperature 防氷 system. the front of an air intake duct is provided with annular outside exterior covering (16) -- annular outside exterior covering -- an insid...  
JP4477497B2  
JP2010519098A
[Subject] The object of the present invention is the sound absorption processing covering material about the position of the surface of an airplane, especially the position of the leading edge like the air-intake of Nasser of an airplane...  
JP2010112952A
To provide an apparatus for optically detecting and identifying liquid waterdrops and ice crystals in the air, including an irradiation part and a detection part.The irradiation part outputs irradiated beams of circularly polarized light...  
JP2010510428A
The object of the present invention is the covering material for silence of an airplane which can cover the leading edge of the air-intake of Nasser of the aggregate for promotion, for example. The structure for silence (32) to which the...  
JP2010510120A
An object of the present invention is the leading edge of an airplane, for example, an air-intake of Nasser (14) of an aggregate for promotion. A powerful porous silence layer which has an open face of a specific ratio toward an inner si...  
JP4422907B2  
JP4424617B2  
JP2010504250A
A system and a method for detecting accumulation of 氷粒 are indicated on these specifications. A method for detecting ice by which a parameter in interior volume of a heated lead pipe is measured is described by one embodiment of illu...  
JP2010502518A
[Means for Solution] Electric heat type defrosting system-oriented temperature monitoring composition is prepared for Surratt 2 of wings of an airplane. Temperature monitoring composition is heater mat 12 of a composite material.11221231...  
JP2009298198A
To energy-savingly achieve ice prevention/removal of a structure body arranged in relative air streams.The ice prevention/removal device is provided with the structure body (wing body) 11; a nano-pin surface part 12 formed over a predete...  
JP2009545481A
[Subject] The present invention provides a device from which existence of a fluid which sank in into an inside of existence of ice which adhered on the surface outside an airplane structure (6), or a certain structure, and/or material of...  
JP2009543729A
A tip constituting part article in which it is heated for airplanes, and a manufacturing method for the same are indicated. This tip constituting part article is provided with a cavity which is provided in an almost middle position of a ...  
JP2009255925A
To provide a system and a method for thermally changing the interface between ice and an object.A system includes a power source configured to be capable of generating a certain amount of power. The amount of power is great enough to mel...  
JP2009214873A
To provide an anti-icing/de-icing system and a method using ultrasonic waves for an external surface of a structure likely to be iced, such as an aircraft wing or engine nacelle, and such a structure incorporating this system.The system ...  
JP2009531595A
According to the present invention, a seal joint joining apparatus (27) is attached to at least one of the branching parts (14, 18, 9) of a heat circulation circuit of shape of a bracket (14), and a possibility of changing into the above...  
JP2009161174A
To provide a heater control architecture for an ice protection system.The heater control architecture for the ice protection includes a first multi-role logic block having a first scheduler to schedule the operation of an array of heater...  
JP2009523637A
According to the present invention, on at least one of the fields (1E, 1I) of a front tip (1), ahead [of a partition (3) ], succeed in an operation so that a flow (EF) of fluid may be changed from laminar flow (EFL) to a turbulent flow (...  
JP4283583B2  
JP2009101990A
To provide a power distribution architecture for an ice protection system so as to effectively distribute by-product dissipation power between a plurality of power distribution units in a manner that optimizes wire weight.In a power dist...  
JP2009096324A
To simplify an air-bleeding system and reduce a load of an engine.This invention relates to an airplane air-bleeding system in which engine bleeding air is adjusted in its temperature and its pressure and supplied to an air-conditioning ...  
JP2009508746A
The invention concerns a system for deicing and/or defogging an aircraft surface ( 4 ) comprising: a temperature sensor ( 5 ) located proximate said surface ( 4 ) and adapted to generate a temperature information (TPT); a computer ( 20 )...  
JP2008545575A
They are conductivity / resistance compound hybrid heater with the strain capability for a pyrogenetic antiice system. The shuttlecock of the rotor of a helicopter is shown. In the embodiment, the shuttlecock of a rotor is arranged by a ...  
JP2008540253A
In the ice coating managerial system for the airplane equipped with at least one rotor (15) which has two or more braids, it has AC electric power supply equipment (13) for supplying AC electric power formed in the portion of the airplan...  
JP2008538602A
The enforcement form of the present invention is characterized by the heat exchange surface which has covering which has surface tension lower than water, in order to flip water and to prevent formation of condensation on the heat exchan...  
JP2008537921A
The defrosting system is equipped with double defrosting system parts in order to realize a redundant system. Generally each of the redundant portion of a system contains the controller, the air data computer, the ice coating speed contr...  
JP2008207792A
To provide a power circuit capable of supplying electric power to an aircraft engine and/or a plurality of electric facilities in its circumference.The power circuit of the aircraft is furnished with an electric power distribution networ...  
JP2008159336A
To provide a freeze preventing and removing device capable of easily and efficiently removing freeze on the surface of an object.A surface side electrode 4 in the shape of a concentric circle is formed on the surface of a glass layer for...  
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...  
JP2008137445A
To realize icing prevention and deicing in the leading edge of an aircraft without energy consumption.This manufacturing method comprises a process (P1) for impregnating at least a fiber in a fiber reinforced composite material with a wa...  
JP2008516849A
風防 (4) of an airplane -- defaut -- in ギング / system which carries out デアイシング, a pair of transparent sheets (8) currently maintained by the relation which separates and meets by a transparent middle layer (14) have re...  
JP4072223B2  
JP4057331B2  
JP2008014880A
To provide a small-sized inexpensive liquid droplet impingement sensor capable of simultaneously and continuously measuring the content and the particle size of liquid droplets, and can be realized using a simple constitution.Two sensor ...  
JP4028981B2  
JP2007537086A
The pressure channels (21) and suction channels (22) are formed between inner wall (29) and perforated outer wall (28) of the wing (1) by partitions (2). The pressure channels (21) with lesser perforated area (B), is connected through a ...  
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...  
JP3985195B2  
JP3977876B2  
JP3973474B2  
JP3959126B2
PURPOSE: To provide an aircraft deicing composition comprising each specific glycol, nonionic surfactant, corrosion inhibitor and water at a specific ratio with a long reicing-protection time and excellent flow properties. CONSTITUTION: ...  
JP3954648B2
A movable sheet overlying a wing is disclosed that creates laminar flow over its exposed surface. The movable sheet serves as an integral, retractable shield for protecting a suction support structure of a wing against contamination, and...  
JP2007521463A
[Solution means] It is the method and equipment for detecting the state where the external ice coating state of a vehicle (100) or ice coating starts. The equipment by one enforcement form of the present invention possesses the temperatu...  
JP2006525122A
[Subject] The labor in the manufacturing process of the bush with a flange which self-lubricous Rajna's ring pasted up, a process, and expense are reduced, and the bush which can maintain the good quality of result products, and its prod...  
JP2006521204A
Strong sparse 氷性 abrasion proof covering (10) can be applied to the airfoil surface (12) by 1 time of 塗工, and defrosting effect on the surface of an airfoil can be achieved. The covering concerned contains the best stratum functi...  
JP2006200334A
To provide an ice thawing device with small power consumption and no danger of fire.For water pipes, the device thaws away ice on water pipes with a tip tool 6 with a built-in ultrasonic wave vibrator 4 fitted on it for directly transmit...  

Matches 701 - 750 out of 1,043