| Document |
Document Title |
|
JP3299276B2 |
An anti-icing fluid suitable for ground treatment of aircraft, being a glycol-based, aqueous solution containing a hydrophobe-bearing, macromonomer-containing polymer thickener in an amount of less than about 5 weight %. Thickening occur...
|
|
JP2002516780A |
This invention provides isolated polynucleotides that encode the MurD protein of Pseudomonas aeruginosa. Purified and isolated MurD recombinant proteins are also provided. Nucleic acid sequences which encode functionally active MurD prot...
|
|
JP2002516076A |
This invention provides isolated polynucleotides that encode the MurD protein of Pseudomonas aeruginosa. Purified and isolated MurD recombinant proteins are also provided. Nucleic acid sequences which encode functionally active MurD prot...
|
|
JP2002516224A |
A brush block assembly, for providing stationary mounting of electrically conductive brushes in contact registration with associated slip rings of a rotating interface, comprises a main housing adapted for mounting in proximity to the ro...
|
|
JP3220258B2 |
PURPOSE: To provide a novel device for discharging heating fluid from an anti- ice system, in an air intake of a turbojet engine. CONSTITUTION: A hollow casing for constituting an air intake of a turbojet engine is provided with an outle...
|
|
JP2001517583A |
A thermal de-ice and anti-ice system for aircraft surfaces employs a laminate in which flexible expanded graphite foil is an electrical and heat conducting layer that is disposed below an outer heat conducting layer, with an electrically...
|
|
JP2001253394A |
To provide a helicopter blade deicing device capable of efficiently removing ice clinging to a blade, while avoiding specialization of members and an increase in weight of an airframe.The helicopter blade deicing device comprises flaps 3...
|
|
JP2001247095A |
To provide an aircraft with snow removing equipment capable of shortening snow removing time and capable of efficiently operating takeoff and landing of the aircraft of an airport.A fluid discharge means 20 is arranged on a fuselage 10 f...
|
|
JP3174072B2 |
An anti-icing system for leading edges (12) of an aircraft. Hot compressed air is discharged from a cavity behind the leading edge (12) through a multitude of small holes in the leading edge skin (30) into the airflow impinging on the le...
|
|
JP3108098B2 |
An electrical generator (1) comprising first and second relatively rotatable winding assemblies (5,8), the first winding assembly (5) having a first electrical output for connection to a first electrical load (4) and the second winding a...
|
|
JP2000514756A |
The invention includes system (100) for modifying ice adhesion strength of ice adhered to any object. The system includes an electrode (106) that is electrically insulated from the object (104) and a DC source (109), e.g., a battery, cou...
|
|
JP2000002871A |
To make an aspect ratio of a rib to at least approximately 5:1 in a structure with the rib 22 installed on an anode 24 in a channel member of a PALC(plasma address liquid crystal) panel. As for this channel member, a width of the anode 2...
|
|
JPH11507990A |
The surface of a workpiece is cleaned by generating a steady-state one atmosphere glow discharge plasma above the surface of the workpiece. The use of one atmosphere, uniform glow discharge plasmas generated by a low frequency RF ion tra...
|
|
JPH11500534A |
PCT No. PCT/DE96/00347 Sec. 371 Date Oct. 22, 1997 Sec. 102(e) Date Oct. 22, 1997 PCT Filed Feb. 23, 1996 PCT Pub. No. WO96/26430 PCT Pub. Date Aug. 29, 1996There are proposed a method and a device for ascertaining the surface condition,...
|
|
JPH10300860A |
To surely detect the icing in a part not directly seen with a simple device by lighting a part intended to detect the icing, receiving the reflected light from the intended part, and displaying it on a display part. A light source 1 is m...
|
|
JPH10510627A |
A contaminant detection system includes a transmitter for transmitting a guided wave through the skin at particular resonances, wherein each resonance point utilized will have propagation characteristics sensitive to a condition of inter...
|
|
JPH107096A |
To crack or break the deposited ice on an external plate by providing an inflatable, tubular member below an outer surface of a leading edge formed of the material with the elastic modulus at least not less than the prescribed value, and...
|
|
JPH09328099A |
To eliminate ices from a front end surface by operating or stopping an expanding means having a shape for distorting an outer surface by a fluid under pressure and producing distortion of an chord direction below the front end outer surf...
|
|
JP2692134B2 |
|
|
JP2661905B2 |
An airfoil deicer (10) and method for deicing an airfoil wherein the deicer has an outer skin (12) having an elevated modulus of elasticity and a means for introducing a small deflection into the outer skin thereby creating substantial c...
|
|
JPH09176621A |
To obtain a polymer-thickened deicing composition for an aircraft and an anti-icing composition by mixing a specified (oxy)alkylene glycol with a (meth)acrylic acid homopolymer, a nonionic surfactant, a salt, etc. Thirty-five (35) to 70w...
|
|
JPH09506462A |
An electrically conductive composite heating assembly that has as its foundation an electrically conductive non-woven fiber layer laminated between layers of fiberglass and other dielectric material and has an abrasion resistant outer la...
|
|
JP2612690B2 |
An AC power control apparatus includes a plurality of power supply circuits for generating powers having different maximum values, a switching circuit for, after an AC current is continuously set in a desired turn on control state, alter...
|
|
JPH09504865A |
(57) [Summary] For example, an ice and snow detector with a tubular duct (10) attached to a stand (12) that can be fixed to the outside of a helicopter. Air passes through the duct (10) in the direction of the arrow by the Venturi struct...
|
|
JPH08512192A |
An electrical circuit that provides ground fault protection by compensating for the capacitive leakage current between an electrothermal de-icing system bonded to an aircraft surface. A conductive shield is interposed between the resisti...
|
|
JPH08301197A |
PURPOSE: To prevent decrease in lift and increase in resistance by suppressing shock waves when a double vertical tail aircraft having a cant angle flies in the transonic range. CONSTITUTION: In each side face of the fuselage 20 of an ai...
|
|
JP2552454B2 |
PURPOSE:To execute an electric conduction control without generating a noise, by generating a trigger signal which is started from the head position of an AC waveform generated in some polarity direction and ended sufficiently before the...
|
|
JP2552453B2 |
PURPOSE:To execute a zero level detection by a simple circuit, so that no noise is generated, by shifting an operation start level of a switching element to a zero level. CONSTITUTION:In an AC power control device for heating the glass i...
|
|
JP2512403Y2 |
|
|
JPH0827665B2 |
PURPOSE:To surely turn on a thyristor even under a usual environmental condition, by supplying repeatedly a signal to a gate of the thyristor. CONSTITUTION:A gate signal of a thyristor can be set to an on-state exactly by supplying it no...
|
|
JPH0826304B2 |
A method of minimizing the adherence of ice on substrates which comprises coating said substrates with a polysiloxane composition which changes into a rubbery elastic material in the presence of water or atmospheric moisture which compri...
|
|
JPH0834399A |
PURPOSE: To prevent freezing of a drain pipe by arranging the range of a drain pipe passing through an attachment flange and the range of a drain pipe passing through a fairing in the fairing from below an aircraft, and heating them with...
|
|
JPH07239321A |
PURPOSE: To provide a method for exactly distinguishing various conditions of the water from the medium such as the air and the water where a sensor is installed, detecting the partial change of the water condition in a measurement area ...
|
|
JPH0732041Y2 |
|
|
JPH0758248B2 |
An ice detector of the vibrating element type comprises a tube that vibrates along its longitudinal axis, and is driven by an excitation coil at the natural frequency of the tube is sealed by a diaphragm which has a surface exposed to an...
|
|
JPH0747400B2 |
An electric resistance element (1) in a device for deicing a wing structure such as the wing of an aircraft or the blades of a helicopter, which includes conducting fibers embedded in a composite fiber structure and power supply wires co...
|
|
JPH072199U |
[Purpose] The present invention is to improve the drawbacks of the conventional example, to provide a heat-generating sheet having a heat-generating temperature self-control characteristic by arbitrarily selecting a heat-generating tempe...
|
|
JPH07775B2 |
The invention provides for a deicing composition for use on airplanes, runways, streets, and the like, which deicing composition comprises (a) an alkylene polyol, (b) an anionic surfactant capable of forming a hydrophobic monolayer on th...
|
|
JPH072189A |
PURPOSE: To execute optimum control and to reduce the generation of a work load on a pilot by a method wherein a power from a controlled power source is fed to a heater for deicing a blade by a source control part, the surface temperatur...
|
|
JPH06101368B2 |
An AC power control apparatus including a power circuit for supplying an AC current to a load, and a circuit connected to a power supply, for initiating energization of the load at a zero-cross point of an AC current waveform. A control ...
|
|
JPH06337255A |
PURPOSE: To provide an ice accretion detector for detecting ice accretion on the window of a helicopter quantitatively without effecting adversely on other machines in the helicopter. CONSTITUTION: A pair of electrodes 3a, 3b disposed in...
|
|
JPH0674408B2 |
A composition is described which consists of a microemulsion of oil in a water/glycol solution containing certain thickening agents, emulsifiers, carboxylic acids having from 10 to 18 carbon atoms and alkanolamines to provide the desirab...
|
|
JPH06206593A |
PURPOSE: To improve an engine output and fuel consumption while effectively performing antiicing and deicing of a wing by connecting one end of an antiicing/deicing hydraulic pipe, provided adjacent to the inside of a wing leading edge o...
|
|
JPH06185453A |
PURPOSE: To convert electric energy into useful mechanical work in controlled mode by thermal expansion of a fluid by means of a plurality of electrically activated miniature heaters. CONSTITUTION: A surface having an array of cavities 1...
|
|
JPH0647275B2 |
The present invention relates to the heating of structural materials and more particularly to a structural composite which is electrically conductive and can be electrically heated.
|
|
JPH06502825A |
PCT No. PCT/GB92/01710 Sec. 371 Date Aug. 16, 1993 Sec. 102(e) Date Aug. 16, 1993 PCT Filed Sep. 17, 1992 PCT Pub. No. WO93/06005 PCT Pub. Date Apr. 1, 1993.An aircraft structural component comprising a forward compartment formed by a fo...
|
|
JPH0684576A |
PURPOSE: To easily and inexpensively provide a non-distorting slide ring assembly by forming a base member by positioning the layers of reinforced textile fabric impregnated with resin in superimposing relation, and by adhesively joining...
|
|
JPH068118B2 |
|
|
JPH05345599A |
PURPOSE: To obtain a de-icer of a front edge of an aircraft by partly operating another displacing tube when one of the displacing tubes is expanded, and enlarging an iced surface for distributing a fatigue stress by an increase in bendi...
|
|
JPH0587437B2 |
|
