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Matches 551 - 600 out of 1,065

Document Document Title
JP6466185B2  
JP6449019B2  
JP6420858B2  
JP6419293B2  
JP2018154021A
To provide a method for manufacturing a resin sheet capable of satisfactorily transferring heat, the resin sheet, a method for manufacturing a structure employing the resin sheet, the structure, and an airframe employing the resin sheet....  
JP2018146363A
To provide a three-dimensional position measuring system and method with which it is possible to measure a measurement object efficiently with high accuracy even in a special environment.The three-dimensional position measuring system co...  
JP6381668B2  
JP6377315B2  
JP6351968B2  
JP6352187B2  
JP6340035B2  
JP6333522B2  
JP2018065551A
To provide an on-board monitoring system that monitors and reports a trend in the performance status of critical components (e.g., electrical deicing heaters) of an aircraft, detects a failure of the critical components in advance, and a...  
JP2018065561A
To provide a method and apparatus taking into account various problems so certifying that an aircraft can operate even not only in a normal icing condition but also in an icing condition including a supercooled large drop.An icing condit...  
JP2018034783A
To provide a deicing system using materials that are conductive and airworthy.Composite airfoils 100 comprise a root section 102 including a first surface. The airfoils comprise an intermediate section 104 having a first surface and coup...  
JP6282400B2  
JP2018020308A
To provide a coating, a coating composition and a method with icing delaying in an aerospace application or the like.A method including one or more coating layers 102 containing first particles 114a, second particles 114c and third parti...  
JP6267329B2  
JP6258328B2  
JP6244276B2  
JP2017206240A
To provide systems and methods for preventing ice formation on prescribed portions of an aircraft, such as engines and wings of the aircraft.An ice prevention system 111 is configured to prevent ice from forming and/or melt ice with resp...  
JP2017171106A
To secure required anti-icing performance while continuing supply of bleed air to an anti-icing device of an aircraft.An anti-icing system 1 includes: a pre-cooler 4 which performs heat exchange between bleed air and outside air; an anti...  
JP2017165403A
To provide an apparatus for providing foreign object debris protection and anti-icing capabilities to an air intake of an aircraft engine.The apparatus includes a frame having at least a portion configured to conduct fluids. A tube is po...  
JP2017165087A
To provide thermoplastic duct segments including integral reinforcing fibers excellent in reduction of weight and cost, in manufacture of duct segments for conveying a fluid.A duct wall includes a sheath of reinforcing fabric incorporati...  
JP2017526799A
This disclosure can reduce the capability of the ice the surface of an object especially an airplane, or other vehicles is frozen, It is related with the use in the production method of polymer which is reactant Shiroki Sun, polyisocyana...  
JP6193691B2  
JP6194201B2  
JP2015024810A5  
JP2017141015A
To provide an anti-icing system that reduces a direct impingement of a high temperature gas stream on an inner surface of an inlet lip of a jet turbine engine for an aircraft.A system 1 includes vanes 56 extending from a bulkhead into an...  
JP2017140965A
To provide an anti-icing device that has a structure which can be made simple and lightweight, and can obtain anti-icing performance adaptively to a movement of a stagnation point without increasing air resistance.The present invention r...  
JP2017136893A
To provide an anti-icing device which has a simple structure and which can acquire anti-icing performance corresponding to displacement of a stagnation point without increasing air resistance.An anti-icing device 10 blows a heating gas t...  
JP2017132456A
To provide propeller blades having an icephobic coating.A propeller blade for rotation about a hub assembly is provided. The propeller blade defines a radial direction along its length from a blade root to a blade tip. The propeller blad...  
JP2017128262A
To provide an icing device capable of keeping pressure of bleeding air in a flow passage of a piccolo tube uniform in its length direction, and making the distance from a bleeding-air injection hole of the piccolo tube to an object of bl...  
JP6170531B2  
JP6169410B2  
JP2017114401A
To provide a pinching sheet capable of keeping the temperature of a structural member at an allowable temperature or lower by suppressing heat conduction from a high temperature duct to the structural member.A pinching sheet 20 according...  
JP2017517584A
The present invention is the method of reducing the ice coating on a substrate, and is an isocyanate * functionality hardening agent to a substrate, It is aimed at the method containing the step which applies a hardenability film formati...  
JP6151751B2  
JP2017105446A
To provide a deicing system for a gas turbine engine and/or an aircraft that does not require pipes for ducting bleed air to one or more surfaces requiring deicing.An embodiment includes a thermal transport bus 102 having a heat exchange...  
JP2017094738A
To provide a device incorporating a liquid-impregnated surface.The invention relates to an article with a liquid-impregnated surface 120, wherein the surface has thereon a matrix 126 of a plurality of solid features, spaced sufficiently ...  
JP2017071386A
To provide a heating element for in-flight de-icing of aircraft which does not damage components being fiber composite structures and requires only small amounts of energy.A heating element 100' includes a carbon fiber material 110' that...  
JP2017510717A
The present invention is the method of manufacturing the surface which flips the water and ice on a metallic board, a) The step which provides a metallic board, the step which grinds the b above-mentioned metallic board, c) The step whic...  
JP2017043352A
To provide, in general, air flow mechanisms, and more specifically, a dynamic resonance system and method for the anti-icing and de-icing of inlet grids.A system includes an inlet grid 110 configured to reduce distortion of an incoming a...  
JP2017030728A
To provide an integrated cooling system for a gas turbine engine and/or an aircraft.A thermal management system 100 for a gas turbine engine and/or an aircraft is provided including a thermal transport bus having a heat exchange fluid fl...  
JP2014131906A5  
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...  

Matches 551 - 600 out of 1,065