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Patent Searching and Data


Matches 551 - 600 out of 1,005

Document Document Title
JP5868087B2  
JP5860155B2  
JP5844360B2  
JP5831309B2  
JP5829683B2  
JP2015534520A
A Anti-icing system for hemispherical protection housing 1 installed on airplane structure is described. A system is provided with a series of piezoelectric devices installed by boundary 2 of housing 1. A piezoelectric device generates a...  
JP2015503487A5  
JP5792623B2  
JP2015174652A
To control a temperature of a hot spot and a temperature of a cold spot associated with a leading edge housing so as to prevent ice formation in a leading edge of an engine nacelle and so as to minimize thermal strain of materials of the...  
JP2015168425A
To provide passive icephobic systems that resist ice formation in harsh environments.Global icephobic performance of a passive deicing structure may be achieved by including one or more ice nucleating zones 32 that are configured, presel...  
JP2015166239A
To provide a system and method for operating an ice detection and deicing system.An ice detection and deicing system 100 uses changes in magnetic properties of various components 106 caused by temperature changes to detect conditions con...  
JP2015143101A
To overcome the conventional problem that the power supply required to power a wire heating pad type anti-ice or de-ice system is significant, because of the inefficiencies of the resistive heating pad elements, and may not be a feasible...  
JP5745824B2  
JP5744008B2  
JP2015091688A
To provide methods of detecting ice formation on an aircraft, in one aspect.A method comprises disposing an ice detector 100 on an exterior surface 200 of the aircraft, the ice detector comprising a probe surface 110 and a pyroelectric m...  
JP5714040B2  
JP5709369B2  
JP2015054593A
To provide an anti-ice system capable of appropriately actuating an anti-icer even if a switch fails after a pilot sets the switch.An anti-ice system 10 for controlling an operation of an anti-icer 50 installed in an aircraft, an anti-ic...  
JP2015024810A
To provide a system and method advantageous for improving the reliability of aircraft service and reducing the running cost of aircraft.The present invention relates to a system and method for monitoring an aircraft wing anti-icing valve...  
JP2015503487A
An ice detection system (122) is provided with a sensor (148) of the 1st group, and a sensor (170) of the 2nd group. A sensor (148) of the 1st group is positioned in a position of the 1st group of an airplane (100). A sensor (148) of the...  
JP5655069B2  
JP2014534104A
The transparent member of an airplane has an overheating member for removing fog, ice, and snow from the external surface of a transparent member. An overheating member contains the film containing the parallel bus line which opened a pa...  
JP2014531361A
[Subject] A system which applies heat on the surface of an airplane is provided. [Means for Solution] In some embodiments, a warmer is embedded into compound material structure of an airplane. Compound material airplane structure is prov...  
JP2014531722A
An electric system according to overheating of an electric conduction member (for example, heating component of a windshield of an airplane) and/or electric arc generation is provided with the following. The 1st switch in the 1st current...  
JP2014195990A
To provide a structural substrate for an aircraft structure, and a method of manufacturing the same.A structural substrate 300 is made of a multi-layer hybrid composite material, which comprises an outermost layer 302, an intermediate la...  
JP2014172474A
To provide a warning system that can sends a stall warning while taking a flight environment into consideration.A warning system gives a warning when an aircraft may have a stall and includes: a selection part which makes a choice betwee...  
JP5582927B2  
JP2014131906A
To provide an ice detection system capable of differentiating between a normal icing condition and a supercooled large drop icing condition.An embodiment comprises a sensor system 206 and an icing condition detector 208. The sensor syste...  
JP5543634B2  
JP5539871B2  
JP5500453B2  
JP5495134B2  
JP5456764B2  
JP5437853B2  
JP2014019432A
To provide a system and method that allows a heating element to be installed and replaced virtually anywhere, without the need for external equipment or heat sources.The system includes: at least one heating element 16 adapted to be adhe...  
JP5384901B2  
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...  

Matches 551 - 600 out of 1,005