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JP6491843B2 |
A drain mast (100) includes a first fairing body (102) defining a first fairing wall (104) and a first drain portion (106). A second fairing body (108) defines a second fairing wall (110) and a second drain portion (112). The first and s...
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JP6487559B2 |
Inerting fuel systems and methods for inerting fuel tanks are disclosed. An inerting fuel system may include an air inlet passage to receive inlet air, air separation modules to separate oxygen from the inlet air when received, and air s...
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JP6483690B2 |
A cap for forming a sealed cavity around an end of a fastener protruding from a structure. The cap has: a cap body with an annular base terminating at a rim which surrounds an opening into a central cavity; an annular skirt providing an ...
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JP6479429B2 |
An equipment dry bay is provided. The equipment dry bay includes at least one partition that subdivides the equipment dry bay into a plurality of compartments, wherein the at least one partition includes a plate, and at least one flame a...
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JP6465222B2 |
When a cylinder portion of an innerliner is positioned inside a mouthpiece and when an upper mold and a lower mold are brought together, a projection portion is provided on an outer circumferential member of the lower mold that closes a ...
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JP6463368B2 |
A method and a system for inerting an aircraft fuel tank includes at least one inert gas generator. The device includes at least means of determining the inert gas requirement of the aircraft tank(s) in real-time, means of regulating the...
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JP6452289B2 |
A method, apparatus, and composite fuel tank for manufacturing a structure is provided. A first composite layer and a second composite layer are placed on a mold. The second composite layer and the first composite layer are cured. The fi...
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JP2018537361A |
Some embodiments provide a method for improving the automatic rotation performance of a rotorcraft in an emergency. The method involves receiving an emergency thrust request from a user interface. The method involves sending a start comm...
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JP6430495B2 |
The invention relates to an air-separation device comprising a generally cylindrical casing housing a filtration element including a bundle of hollow oblong fibers forming a membrane, the longitudinal axis of the fibers being parallel to...
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JP6419437B2 |
An engine pylon that is used for supporting an engine, the engine pylon including a pylon body having an upper pylon and a lower pylon. The pylon further includes a fairing that covers the pylon body such that the upper pylon and fairing...
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JP6419724B2 |
A device for mounting and supporting a generally cylindrical or tapered tank, having a main axis X, that includes a pair of first retaining rods for retaining the tank along a vertical axis Z on each of a first and second end of the tank...
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JP6399842B2 |
Systems and methods for sensing gas are isclosed. In one aspect, a system to monitor an output of a gas source comprises a chamber (110) comprising a plurality of input ports (112) to receive inputs from a plurality of gas sources (130),...
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JP6397910B2 |
A connection device is suitable for connecting two tubes to one another, and optionally to a fluid tank for fluid transmission piping of an aircraft or a spacecraft Also disclosed are pipes incorporating said tubes and said device; and a...
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JP6375171B2 |
A method comprises collecting a data set of field characterization measurements at a location inside a reverberant cavity (210) excited by signals having multiple discrete electromagnetic frequencies; and performing a number (n) of circu...
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JP2018115766A |
To provide a method and apparatus for limiting the flow of electric current, induced by an event such as lightning or an electrical fault, along a fluid transport system and allowing static dissipation along the fluid transport system.A ...
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JP6360070B2 |
A cryogenic tank assembly includes a cryogenic tank having an internal volume that is configured to contain liquefied natural gas (LNG). The cryogenic tank includes an inlet and an outlet that are each fluidly connected to the internal v...
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JP6359532B2 |
A filler device for a fluid tank, including: a filler duct; a first stopper, for preventing overfilling of the tank, and a second stopper for preventing fluid from leaving the tank in unwanted manner; a first float mechanically connected...
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JP2018098093A |
To increase a drivable distance while suppressing the upsizing of a mobile unit.A mobile unit 2 comprises a body part 21, a propulsion engine 22, and an energy supply part 3. The propulsion engine 22 propels the body part 21. The energy ...
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JP6342471B2 |
A system for managing thermal transfer in at least one of an aircraft or a gas turbine engine includes a first engine system 202 utilizing an oil for heat transfer. The oil of the first system has a temperature limit of at least about 50...
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JP6339947B2 |
Systems and methods for radiation monitoring with a fuel-based liquid scintillant are disclosed. Fuel-scintillant compositions according to this disclosure may serve dual purposes of a fuel to power an engine and a scintillator to detect...
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JP6335791B2 |
A method and apparatus comprising a first composite layer and a second composite layer in which the second composite layer is associated with the first composite layer. The first composite layer and the second composite layer form a stru...
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JP2018511744A |
A method of using and repairing a seal cap with a structure that includes a seal cap, eg, in some embodiments, a seal cap that may be useful for sealing a fastener that projects into the fuel storage tank of an aircraft. In some embodime...
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JP6312987B2 |
A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is co...
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JP6290259B2 |
The subject of the invention is a device for the in-flight conditioning of equipment of cryogenic circuits of an aircraft, which device includes means for bleeding air from outside the aircraft, means for extracting nitrogen from this ai...
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JP6290904B2 |
A tank for storing liquid configured to withstand overpressures caused by a projectile impact and positioned in a structure. The tank includes an overpressure management device having a layer of polyethylene-based hyperelastic foam. An e...
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JP6283039B2 |
A gas separation module includes at least one inlet port, a plurality of outlet ports, and a plurality of hollow fiber membranes. Individual fibers have a feed end and a product end with a retentate interior side and a permeate exterior ...
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JP6277255B2 |
An aircraft fuel scavenge system incorporates a scavenge pump (30) receiving fuel from a center tank (10) and depositing the fuel in a wing tank (14). A water separator (40) receives fuel through an inlet tube (38) providing a plurality ...
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JP6258356B2 |
A gas separation method includes flowing a gas feed along a feed flow path within a housing directionally from a product end to a feed end of a gas separation membrane. After the feed flow path, the gas feed flows along a membrane flow p...
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JP6254869B2 |
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JP6246476B2 |
A fuel vapor removal method includes removing fuel vapor from ullage (110) of a fuel tank (100) of a vehicle, adsorbing the fuel vapor removed from the ullage (110) onto adsorption media (54) on the vehicle, and desorbing the fuel vapor ...
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JP2017534505A |
The fluid system can include an inlet conduit, which can be placed in the fluid flow path between the fluid source and the fluid destination. The fluid conduit can include a fluid mixing section. The fluid system can include a fluid sepa...
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JP2017530049A |
The present invention uses a suction line (4) and a pump (1) of a pump (1) using at least one diaphragm pump (1) having a pulsating diaphragm that can pulsate between two flanges by the operation of the actuating means. The present inven...
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JP6211091B2 |
A gas separation method includes contacting a membrane filter with gas feed, permeating the gas from the gas feed through the membrane, and producing filtered gas from the filter. The filtered gas is produced from the filter as a result ...
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JP6203991B2 |
An electricity generating apparatus capable of efficiently and safely charging a storage battery in an unmanned aerial vehicle during its flight and an unmanned aerial vehicle equipped with such apparatus. The apparatus is mounted in the...
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JP2017165242A |
To provide a fuel pipe of an aircraft which maintains a fuel in the fuel pipe to a proper temperature while considering the reliability constantly needed in aircrafts.A fuel pipe 2 mounted on an airframe of an aircraft includes: an inner...
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JP6200697B2 |
A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system in an aerospace vehicle. The aerospace vehicle is operated. The fluid transport system in the aerospace vehicle is co...
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JP6181184B2 |
An aircraft fuel tank flammability reduction method includes feeding pressurized air into an air separation module containing a carbon membrane, the air feed exhibiting a normal pressure of no more than 55 psig and the carbon membrane co...
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JP6163041B2 |
Provided is a fuel system that can reduce the amount of fuel in a second tank before the amount of fuel in a first tank. A fuel system includes: a first tank and a second tank that respectively store fuel; a fuel supply pump that supplie...
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JP6140981B2 |
A system for reducing flammability has a heat exchanger (420) that cools ullage from a tank (500), condenses vapors within the ullage, and returns the cooled ullage and vapors to the tank.
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JP2017095095A |
To provide aircraft fuel storage systems which provide safe, efficient and economical storage of cryogenic fuels such as liquefied natural gas (LNG) in combination with other fuel storage systems aboard the aircraft.A cryogenic fuel stor...
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JP6131785B2 |
Two systems of a first pump unit (7a) and a third pump unit (7c) that supply fuel of a fuselage fuel tank (3a), and a second pump unit (7b) and a fourth pump unit (7d) that supply fuel of fuel tanks (3b, 3c) in both right and left wings ...
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JP2017081559A |
To provide an aircraft system using fuel cells with capability to manage heat generated during fuel cell operation.An aircraft system 5 is disclosed including: a fuel storage system 10 comprising a first fuel tank 21 capable of storing a...
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JP6125172B2 |
A method and apparatus for inert gas distribution in a fuel tank, the apparatus comprising a tube (144), an opening (146) in the tube (144), and a valve (156) associated with the opening (146). the tube (144) is configured to carry an in...
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JP6117647B2 |
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JP6110391B2 |
A mounting system for tubular structures within a wing structure provides for positioning of the tubular structure as it passes through wing ribs. The system provides for electrostatic protection from discharges between the rib and the t...
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JP6100461B2 |
An opening portion of a vent member is prevented from being blocked, and thus ventilation is reliably performed. A plurality of opening portions (40A, 40B) are formed in a single vent stringer (20), and thus even in a case where one of t...
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JP6093450B2 |
Cryogenic fuel compositions including a cryogenic fuel and paraxyelene and a dual fuel aircraft system for an aircraft having at least one turbine engine, including a first fuel system for providing a first fuel from a first fuel tank to...
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JP6086701B2 |
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JP2017024001A |
To provide a gas generator that eliminates some of disadvantages of prior art.There is provided a gas generator having a tubular member (10) having high low temperature toughness, where the tubular member (10) has ductile fracture behavi...
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JP6067244B2 |
An aircraft fuel scavenge system incorporates a scavenge pump (30) receiving fuel from a center tank (10) and depositing the fuel in a wing tank (14). A water separator (40) receives fuel through an inlet tube (38) providing a plurality ...
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