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Matches 551 - 600 out of 1,019

Document Document Title
JP2017013785A
To prevent ice accumulation in a vehicle sensor or a probe.A device configured to prevent ice accumulation includes: at least one wall defining a leading edge; and a pneumatic passage configured to receive a pressurized fluid. The device...  
JP2017002269A
To provide a mixed coating material capable of forming a water-repellent coating film which is reacted and cured at a room temperature and has high durability; and a blade and an ice preventing system capable of efficiently preventing ic...  
JP2016533934A
The present invention relates to a glass panel for an airplane suitable for a semi- orbital flight and an aviation flight, and is this glass panel, An outside panel (1) currently made from polycarbonate or alumino silicate for heat resis...  
JP2016172461A
To attain power saving by performing the proper drive control of a windshield heater.A windshield device 10 comprises: a windshield 11; a heater 12 being equipped at the windshield 11 and generating heat by energization; a dew point temp...  
JP2016526578A
After beforehand only dissociating roughly, without the present invention's collecting the control frozen snow agents for airplanes polluted with the control frozen snow agent for runways depending on the (1) used case in a suitable devi...  
JP2016137890A
To provide a continuously monitored deicing system.The continuously monitored deicing system may have a pneumatic deicer (3) and a signal wire (4) running through the pneumatic deicer. The signal wire may break in response to a failure o...  
JP5932782B2  
JP2016103467A
To provide a structure of an induction heating system in an aircraft induction-heating anti-icing system including a ferromagnetic susceptor, a heating coil and an AC(Alternate Current) power source, which enables uniform heating of a su...  
JP2016094186A
To provide systems for multiple zone heaters for rotor craft and methods for operation.An example system for a rotor craft 100 comprises multiple blades 110, 112, 120, 122 coupled to a rotor 108, 118, and areas of the multiple blades div...  
JP5925561B2  
JP2016064818A
To provide an electro-expulsive de-icing actuator.An apparatus 100 for removing ice from an object (e.g., in-flight ice removal from the skin of an aircraft) comprises: an actuator assembly 101, 102 that forms an elongated electrically c...  
JP5898621B2  
JP2016028953A
To provide a blade structure capable of appropriately preventing icing in an environment exposed to high-speed overcooling water droplets.On a surface of an aircraft blade, a surface of a blade front edge portion predicted to be collided...  
JP5871794B2  
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  

Matches 551 - 600 out of 1,019