Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 601 - 650 out of 1,019

Document Document Title
JP2013256286A
To provide a method and apparatus for accurately detecting an icing condition.An apparatus includes a piezoelectric material 304 and a vibration detector 308. The piezoelectric material 304 has a surface proximate to a surface of a vehic...  
JP2013545061A
The present invention relates to defrosting apparatus for defrosting structural part {170, 270, and 370. A structural part may be completely produced from material of polymers or metal. This apparatus is provided with a power supply (250...  
JP5373894B2
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...  
JP2013233925A
To provide a system that consumes a small amount of energy to prevent and/or remove ice from external surfaces, such as leading edges, of an aircraft.An electro-active polymer (EAP) surface 10 having a plurality of actuators 20 is adapte...  
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...  
JP2013539648A
A holding part and a rotation base material which can be rotated to the holding part, At least one electric appliance (23) held by the rotation base material, A power supply system which can supply electric energy to the electric applian...  
JP5319285B2
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 )...  
JP2013193735A
To provide a method and apparatus for certifying that an aircraft can operate even in not only a normal icing condition but also a supercooled large drop icing condition.An icing condition detection system includes an optional number of ...  
JP2013189073A
To accurately detect whether a unit deicing boot targeted for expansion state detection is in an expanded state, without using a timed circuit.By switching valve output signals to respective electric control valves from OFF to ON at diff...  
JP2013184698A
To provide an icing condition detection system that differentiates normal and supercooled large drop icing states so that an aircraft is certified to operate in the normal icing states but not those that include supercooled large drops.A...  
JP2013173949A
To provide a tape including (a) a single layer including a crosslinked polymer selected from the group consisting of a crosslinked polyurethane, a crosslinked polyurea, and a crosslinked mixed polyurethane/polyurea polymer, and (b) an ad...  
JP5276997B2
A heater control structure for an ice protection system is disclosed that includes a first multi-role logic block having a first scheduler to schedule the operation of an array of heaters and a first controller to control a first group o...  
JP2013163479A
To provide an anti-icing structure for a front edge part in an aircraft, configured to prevent local overheating and reliably and efficiently prevent icing at the front edge of the aircraft with a simple structure.An anti-icing structure...  
JP2013163480A
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 nozzl...  
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  

Matches 601 - 650 out of 1,019