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Matches 601 - 650 out of 1,005

Document Document Title
JP2013163478A
To provide an anti-icing device for a front edge part in an aircraft, configured to reliably and efficiently prevent icing at the front edge of the aircraft with a simple structure.An anti-icing device 40 includes: an extraction air nozz...  
JP2013151647A
To provide a heat storage component for a transport machinery which can easily and surely store heat energy without necessitating any special equipment, and can effectively suppress icing of snow (ice) on a component of the transport mac...  
JP5253587B2  
JP5247168B2  
JP2013529578A
A linkage mechanism to which it shows a flexible cable between two structures. A linkage mechanism is provided with the end face side arm which has the end face side pivot joint which combines the end face side arm with the 1st structure...  
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...  
JP5233037B2  
JP5227320B2  
JP5224607B2  
JP2013124096A
To provide a seal assembly for sealing an aperture in a fixed leading edge for storing a strut of a translating cable device of an electric deicing system so as not to cause aerodynamic drag and undesirable flow disturbances, when the sl...  
JP5205383B2  
JP2013091495A
To detect accumulation of ice particles, and to detect ice particles that are present in sufficient concentration for a sufficient time period.Systems and methods for detecting ice particle accumulation are disclosed herein. In one exemp...  
JP5192035B2  
JP2013505426A
Directions of narrowband irradiation for defrosting or 脱氷 from the surface are provided. This technique is applicable to defrosting of various types, such as defrosting of a windshield, defrosting of airplane wings, and defrosting fo...  
JP5134371B2  
JP2009508746A5  
JP5112335B2  
JP2012533477A
A bus bar system includes a non-conductive substrate having a major surface. At least one conductive bus bar is formed over at least a portion of the major surface. A conductive coating is formed over at least a portion of the bus bar an...  
JP2012532051A
A method and a system for an integrated エゼクタ valve assembly are provided. The 1st valve assembly constituted by integrated エゼクタ valve assembly so that a flow of fluid with comparatively lower pressure from the 1st inlet p...  
JP5083918B2  
JP2012229690A
To provide a flow device adapted to operate as a restrictor and provide a pressure relief capability in the event of an over-pressurization event within a fluid system containing the device.The flow device 50 includes an expandable orifi...  
JP2012526705A
The device which removes ice from a subject (for example, defrosting from the shell of the airplane under flight) contains the actuator assembly which makes a long and slender conductive loop. An actuator corresponds to operation of the ...  
JP2012525476A
A composite structure includes a matrix material and a carbon nanotube (CNT)-infused fiber material that includes a plurality of carbon nanotubes (CNTs) infused to a fiber material. The CNT-infused fiber material is disposed throughout a...  
JP2012166656A
To assure a field of vision from a cockpit in case of emergency.The aircraft includes a camera 21, a display device 31 disposed in the cockpit C of an aircraft body, a final control element 32 which is disposed in the cockpit and starts ...  
JP2012166683A
To surely prevent widow fogging even when a part of a de-fogging device fails.The de-fogging device includes a main de-fogging device and a spare de-fogging device 20. The spare de-fogging device 20 includes a gas tank 21 stored with pre...  
JP2012148716A
To provide an anti-icing apparatus which is simple in configuration and prevents the icing of an aircraft flying in an icing environment, a wing, the aircraft and an anti-icing method.The anti-icing apparatus outputs pressure waves towar...  
JP2012132006A
To provide an article having ice phobic surface, and to provide a method of making and using the article.The article includes: a silicone composition disposed on a surface of the article; and a grease applied to the silicone composition,...  
JP2012514552A
[Subject] A method for removing external freezing of an airplane of enabling quick and reliable freezing removal of an airplane before starting is developed, and it carries out as [be / apparatus which requires structure top expense, hig...  
JP2012513932A
A lamination windshield of a transparent body, for example, an airplane, supervises performance of one or more character of heating arrangement composition of a windshield, for example, and is provided with one or more sensors which gene...  
JP2012513934A
A 防氷 system (200) includes the component-parts surface (202) which has the compound structure containing a composite layer (214), At least one heating element (220) currently formed in an inside of a composite layer (214) is assisted...  
JP2012514289A
A heating system (1) including an energy supply mechanism (5). A base heating machine style of an electric heat type provided with an insulating layer is provided with a base heating layer (10) laid in this, and an electric connection me...  
JP4959320B2  
JP4951616B2  
JP2012512749A
A device for maintaining a cutting edge, e.g. a focused laser beam at a constant distance from a surface of the work piece as the cutting edge imposes a cut line in a coating on the surface of the work piece. The device includes a consta...  
JP4934783B2  
JP4907830B2  
JP2012507424A
In order that the system (10) for cooling the heat exchanger (12) in an airplane may supply engine ブリード air to a process air line (28), the first end has the process air line (28) connected to the engine (16) of an airplane. The ...  
JP2012062049A
To provide a propeller blade having ice-phobic coating which is a passive system capable of improving reliability and maintainability and furthermore reducing both the initial acquirement cost and the maintenance cost during procession.T...  
JP2012507675A
A valve system includes a conduit having a flow of fluid therethrough, and a butterfly valve assembly. The butterfly valve assembly includes a shaft extending obliquely within the conduit, a butterfly disk, and a first bearing assembly p...  
JP2012046151A
To provide an aircraft ice protection system capable of efficiently implementing ice protection and improving aircraft performance such as prevention of decrease in main thrust and improvement in fuel economy, and to provide an aircraft ...  
JP2012505984A
The present invention is a multiplex windowpane unit (100) provided with at least three substrates (10, 20, 30) held together by the frame structure (90), In the multiplex windowpane unit (100) by which at least two middle gas-charging l...  
JP2011183922A
To properly prevent generation of ice adhered to the outside of a wing leading edge part by effectively heating the wing leading edge part, in an anti-icing and deicing device at the wing leading edge part in an aircraft and a main wing ...  
JP2011524300A
The system has pipes (2-4) for conveying gas from a source (1) to a work place (5) i.e. gas outlet. A flow rate determining device (7) determines gas mass flow in the pipes. A pressure determining device (9) determines static pressure in...  
JP4728325B2
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 ...  
JP2011520058A
A front tip structure used with an aerospace plane of this application contains a main part which has the channel surface which appoints a front tip which suited so that it might face in the style of air during an operation, and the inne...  
JP2011519401A
A front tip structure used with an aerospace plane of this application is provided with the following. A main part which has the channel surface which appoints a front tip which suited so that it might face in the style of air during an ...  
JP2011111158A
To quickly detect the presence of supercooled water drops larger than a threshold diameter without depending on an exciting circuit and a measuring circuit.This aircraft (1) includes a fuselage (2) and a detecting device (10). The detect...  
JP2011516344A
The present invention relates to a defrosting system for airplanes which has at least one air delivery means for sending air to at least one heat source and a portion in which an airplane should be defrosted. As compared with a prior art...  
JP2011095264A
To provide a method for reducing de-icing heater error (DHE) in a total air temperature (TAT) probe.Using the method, a nominal DHE function is obtained for a particular type of TAT probe as a nominal DHE function derived from a pluralit...  
JP2011093521A
To provide a thermal icing condition detector to solve problems of a conventional dry thermal sensor.In an icing condition detection system, a circuit 122 provides an output representing impending icing conditions as a function of power ...  

Matches 601 - 650 out of 1,005