123 results about "Cryogenic fuel" patented technology

Turbine engine assemblies including a turbine engine assembly having a turbine core comprising a compressor section, a combustion section, a turbine section, and a nozzle section, which are axially aligned, wherein the combustion section comprises a generally annular case having inner and outer walls, a heat exchanger comprising multiple passages in proximity to at least one of the inner and outer walls, with the passages arranged about at least a portion of the case and in fluid communication with each other such that fluid may flow through the passages and a cryogenic fuel system having a cryogenic fuel tank with a supply line coupled to one of the passages, wherein cryogenic fuel may be supplied from the cryogenic fuel tank, through the supply line, to the passages of the heat exchanger, where the fuel in the passages may be heated by the combustion section. The heat exchanger may be a single or multistage vaporizer.

An apparatus includes a low temperature fuel cell, a high temperature fuel cell or a hydrocarbon reformer, a hydrocarbon fuel supply, an oxygen generator, and a molecular sieve. The oxygen generator separates air to provide oxygen enriched air to the fuel cells and the reformer. Hydrocarbon fuel is provided to the high temperature fuel cell or the reformer, and the exhaust gas thereof may be separated through the molecular sieve, to provide hydrogen enriched gas to the low temperature fuel cell, water, carbon monoxide, and carbon dioxide. The low temperature fuel cell outputs nitrogen gas and high purity water. The emitted carbon oxides and nitrogen oxides are catalytically converted to nitrogen and carbon dioxide being returned to the atmosphere. The process and apparatus are very efficient, produce high purity water and electrical energy, and are environmentally friendly.

System and methods are disclosed for fluid measurements which may be utilized to determine mass flow rates such as instantaneous mass flow of a fluid stream. In a preferred embodiment, the present invention may be utilized to compare an input mass flow to an output mass flow of a drilling fluid circulation stream. In one embodiment, a fluid flow rate is determined by utilizing a microwave detector in combination with an acoustic sensor. The acoustic signal is utilized to eliminate 2 pi phase ambiguities in a reflected microwave signal. In another embodiment, a fluid flow rate may be determined by detecting a phase shift of an acoustic signal across two different predetermined transmission paths. A fluid density may be determined by detecting a calibrated phase shift of an acoustic signal through the fluid. In another embodiment, a second acoustic signal may be transmitted through the fluid to define a particular 2pi phase range which defines the phase shift. The present invention may comprise multiple transmitters / receivers operating at different frequencies to measure instantaneous fuel levels of cryogenic fuels within containers positioned in zero or near zero gravity environments. In one embodiment, a moveable flexible collar of transmitter / receivers may be utilized to determine inhomogenuities within solid rocket fuel tubes.

The present invention relates to the field of electrochemical cells and fuel cells, and more specifically to polymer-electrolyte-membrane fuel cells (PEMFC) and direct methanol fuel cells (DMFC). It is directed to catalyst-coated ionomer membranes ("CCMs") and membrane-electrode-assembl- ies ("MEAs") that contain one or more protective film layers for protection, sealing and better handling purposes. The one or more protective film layers are attached to the surface of said catalyst-coated membranes in such a way that they overlap with a region of the passive non-coated ionomer area, and with a region of the active area that is coated with a catalyst layer. Furthermore, the present invention discloses a process for manufacture of CCMs and MEAs that contain protective film layers. The materials may be used as components for the manufacture of low temperature fuel cell stacks.

This invention relates to electrode substrates for electrochemical cells, particularly low-temperature fuel cells, and processes for their production. Low-cost carbon fiber paper structures are used as precursor for preparation of an all-carbon product that has a high electric conductivity and porosity and can be processed in a continuous reel-to-reel mode. These paper materials are further impregnated and processed to adjust the final product properties. This all-carbon electrode substrate is not brittle thereby avoiding the main disadvantage of the prior art.

A method for synthesizing nanostructured carbon materials having excellent crystallinity and large surface area using inexpensive metal salts and polymeric carbon precursors are disclosed. The synthetic method comprises the formation of nanostructured carbon material—metal—inorganic oxide composite through catalytic graphitization of a polymeric carbon precursor—metal salt—inorganic oxide composite, removal of inorganic oxide using an etchant, and removal of metal through an acid treatment, wherein an inorganic oxide material is added in the reaction mixture in order to increase the surface area of the nanostructured carbon material, and metal salt is used as a graphitization catalyst. The resultant nanostructured carbon materials possess the characteristics of excellent crystallinity and large surface area, where such characteristics are well suited for low temperature fuel cell electrode applications.

A cryogenic fuel tank adapted for attachment to an aerospace vehicle includes an exterior layer of reinforced composite insulating foam. The insulating foam is reinforced with an aramid fiber mesh or a closed cell foam may be reinforced with one or more of carbon nanotubes, graphite whiskers, silicon carbide fibers or graphite fibers. The improved composite insulating structure disclosed herein provides a remedy for insulating material breaking off the large external fuel tank attached to the space shuttle during launch and ascent into space.

An LNG fuel system for gas turbine engine systems is disclosed that allows more efficient management of cryogenic fuels such as LNG to reduce emissions and improve engine efficiency. In one configuration, an intercooled, recuperated gas turbine engine comprises an LNG tank incorporating a liquid-to-vapor LNG fuel circuit in parallel with a vapor fuel circuit. In a second configuration, an alternate vapor fuel circuit is disclosed. In either configuration, the fuel in the liquid fuel circuit is vaporized and heated by the engine's intercooler or by both the engine's intercooler and / or a heat exchanger on the exhaust. In another configuration, both the fuel in the liquid-to-vapor LNG fuel circuit and the vapor fuel circuit are heated by a heat exchanger on the exhaust.

A cryogenic fuel tank assembly 10 is provided comprising a cryogenic fuel tank wall 22. A foam assembly 24 is affixed to the cryogenic fuel tank wall 22, the foam assembly 24 having an inner surface 30 and an outer surface 32. A first solid film 40 bonded to the outer surface 32 to provide a uniform outer bonding surface 42. A thermal protection system assembly 38 is bonded to the uniform outer bonding surface 42.

A cryogenic fuel tank assembly 10 is provided comprising a cryogenic fuel tank wall 22. A foam assembly 24 is affixed to the cryogenic fuel tank wall 22, the foam assembly 24 having an inner surface 30 and an outer surface 32. A first solid film 40 bonded to the outer surface 32 to provide a uniform outer bonding surface 42. A thermal protection system assembly 38 is bonded to the uniform outer bonding surface 42.

A method for producing a supercritical cryogenic fuel (SCCF) includes dissolving a hydrogen gas in fuel value proportions into a supercritical hydrocarbon fluid. The method is performed by placing a hydrogen gas and a hydrocarbon fluid at a pressure greater than the critical pressure of the hydrocarbon, placing the hydrogen gas and the hydrocarbon fluid at a temperature below or approximately equal to the critical temperature of the hydrocarbon forming the supercritical hydrocarbon fluid, and then mixing to dissolve the hydrogen gas into the supercritical hydrocarbon fluid. A system for performing the method includes a vortex mixer configured to turbulently mix the hydrogen gas and the supercritical hydrocarbon fluid. The supercritical cryogenic fuel (SCCF) produced by the method and the system includes the supercritical hydrocarbon fluid with a selected mole fraction of the hydrogen gas dissolved therein.

The invention relates to the method for fast preparing the nano catalyst used for the fuel cell and the sensor. The active constituent (monocomponent or polycomponent) is deioxidized or oxidized uniformly (no phase splitting) only one time, adhered to the surface of the carrier by using the microwave adjust and control technique. The chemical reactions are induced and controlled by the microwave. The drying procedure and unartificial smashing procedure are completed at the same time. The invention possesses the features of the small granule of the catalyst, even distributed, high electrochemical activity. The catalyst with the capacity of the active matter more than 40% can be prepared once by the single kettle.

A solid oxide fuel cell device that includes an elongate substrate having a first end and an opposing second end with a length therebetween, a cold zone along a first portion of the length adjacent the first end, and a hot reaction zone along a second portion of the length adjacent the second end. The hot reaction zone is configured to be heated to an operating reaction temperature, and the cold zone is configured to remain at a low temperature below the operating reaction temperature. A fuel inlet and air inlet are each positioned in the cold zone and coupled to respective elongate fuel and oxidizer passages that extend through the hot reaction zone within the elongate substrate in parallel and opposing relation to respective fuel and air outlets adjacent the first end. An anode and a cathode are each positioned adjacent a respective fuel and oxidizer passage in the hot reaction zone within the elongate substrate and each is electrically coupled to a respective first and second exterior contact surface on the elongate substrate in the cold zone. A solid electrolyte is positioned between the anode and cathode, and negative and positive electrical connections are made to the respective first and second exterior contact surfaces. A fuel cell system is also provided incorporating a plurality of the fuel devices with their hot reaction zones positioned in a hot zone chamber and their cold zones extending outside the hot zone chamber. A heat source is coupled to the hot zone chamber to heat the reaction zones to the operating reaction temperature. Fuel and air supplies are coupled outside the hot zone chamber to the cold zones for supplying fuel and air flows into the respective fuel and oxidizer passages. A method of making a solid oxide fuel cell device is also provided in which fluid anode and cathode materials are flowed into passages followed by liquid removal to thereby form anodes and cathodes in the passages.

The invention discloses a double preheating and heat-accumulating energy-saving boiler using low-calorie fuels, comprising a furnace body. Two or a plurality of burners are arranged in the furnace body; each burner is provided with a high-temperature combustion-air inlet and a high-temperature fuel inlet; the high-temperature combustion-air inlet and the high-temperature fuel inlet are connected with an air heat-accumulating chamber and a fuel heat-accumulating chamber respectively; and a plurality of burners are adopted for combustion and smoke venting in turn. Firstly, the recovery of waste heat is conducted through the air / fuel heat-accumulating chamber during exhausting smoke, as a result, the loss of heat-energy is reduced and the combustion efficiency is improved; secondly constant-temperature combustion-air and low-temperature fuels are preheated and mixed by the air heat-accumulating chamber and the fuel heat-accumulating chamber for combustion, and as a result, the combustion temperature is increased; thirdly, a plurality of burners adopt periodical reversing combustion, and as a result, the local high-temperature area in the combustion chamber is eliminated, the temperature in the combustion chamber is distributed more evenly, and the service life of the furnace is prolonged.

A fuel feeding system for storing liquefied gas and feeding gaseous fuel to be used in a piston engine, which fuel feeding system includes at least two cryogenic fuel tank arrangements having a first tank arrangement and a second tank arrangement in connection with each other. The fuel feeding system includes a gaseous fuel feed line connected at its first end to at least one piston engine, in which system the first tank arrangement is provided with a pressure build-up system having a first heat exchanger unit. The inlet of the heat exchanger unit is connected to a bottom section of the first tank arrangement the outlet of which is connectable to the top section of the first tank arrangement. The first tank arrangement and the second tank arrangement are both pressure vessels, and the first tank arrangement is selectively connectable to the fuel feed line by a gas line extending from an outlet in the top section of the first tank arrangement.

A fuel tank mounting system for movable machine is disclosed. The mounting system may include a fuel tank connected to a frame of the movable machine in such a manner as to allow vertical motion of the tank relative to the frame. The fuel tank may be mounted to the frame using a spring and / or a shock absorber. The fuel tank may be a cryogenic fuel tank for storage of liquid natural gas. The shock absorbers may be tunable so that the level of dampening provided by the shock absorber is tailored to the type of machine and the specific mode of operation of the machine.

A system for desulfurizing hydrocarbon fuel for a reformer and SOFC stack in an SOFC system. The system comprises a liquid phase desulfurizer for low-temperature desulfurization of an amount of liquid fuel ahead of reformer / stack startup and for continuous removal of large refractory sulfur-containing compounds from low-temperature fuel thereafter during operation of the reformer / stack,and gas phase desulfurizer for continuous high-temperature desulfurization of a stream of vaporized hydrocarbon fuel downstream of the liquid phase desulfurizer. The gas phase desulfurizer may be either upstream or downstream of the reformer.

A reservoir safely accommodates a fuel using a barrier layer, which at least partly separates the contact areas of the reservoir and / or contact elements to be protected. The barrier layer is formed of a fire-proof medium which displaces volatile and ignitable fuel having a density less than the density of the fire-proof medium, providing a chemical-physical separation of hydrogen from the air surrounding the reservoir. In vehicles, particularly aircraft, safe operation may be improved by application of the barrier in the reservoir. In one embodiment, there is an additional reservoir filled with an inert material that surrounds the hydrogen reservoir.

A tool for draining and refilling a vehicle tank for cryogenic fuel, wherein the tool when in position for use has a vertical direction and includes a heat exchanger and a cooling tank, the cooling tank having an upper portion and a lower portion as viewed in the vertical direction of the tool and including a fuel outlet having at least one outlet valve, the fuel outlet being connected to a first fuel conduit and second fuel conduit via the at least one outlet valve, wherein the first fuel conduit includes an arrangement for connecting the first fuel conduit to an inlet on the heat exchanger, and wherein the second fuel conduit includes an arrangement for connecting the second fuel conduit to an inlet on a vehicle tank, the cooling tank further including an inlet, the inlet being connected to a fuel inlet conduit via a check valve and the fuel inlet conduit including an arrangement for connecting the inlet to an outlet from the heat exchanger, or to an outlet from a vehicle tank, and the outlet of the heat exchanger including an arrangement for connecting to an inlet on a vehicle tank, and a system and method for draining and refilling a vehicle tank.

The invention provides a fuel cell micro high-efficiency thermo-operated self-circulating cooling system, comprising: bipolar plate whose inner cavity is provided with microchannel evaporator, and condenser tube, where the condenser tube is connected with the microchannel via inlet and outlet micro check valves having one-way turn-on function, and there is circulating cooling medium inside the condenser tube and the microchannel, and according to the requirement for cooling and heat discharge, the condenser tube is also provided with heat radiation fins, and connected with cooling working medium storage cylinder. And it has good heat radiation effect, simpler structure and higher total utilization ratio of cell stack, and applies to low temperature fuel cell stacks such as PEMFC, and DMFC.

Turbine engine systems are described. The turbine engine systems include a combustor arranged along a core flow path of the turbine engine, a cryogenic fuel tank configured to supply a fuel to the combustor, a fuel supply line having a first flow supply line and a second flow supply line, the first flow supply line fluidly connecting the cryogenic fuel tank to the combustor through a first core flow path heat exchanger, and the second flow supply line fluidly connecting the cryogenic fuel tank to the combustor through a second core flow path heat exchanger, and a flow controller arranged along the fuel supply line and configured to respectively control a flow of fuel into the first flow supply line and the second flow supply line.

An aircraft having a turbine engine having a bleed air output line, a cryogenic fuel system having a cryogenic fuel tank for storing cryogenic fuel and a supply line operably coupling the tank to the turbine engine, and an on board inert gas generating system (OBIGGS) fluidly coupled to the bleed air output and having a nitrogen rich stream output line and an oxygen rich stream output line.

A fuel cell power plant system includes the ability to operate an enthalpy recovery device even under cold conditions. A bypass arrangement allows for selectively bypassing one or more portions of the enthalpy recovery device under selected conditions. In one example, the enthalpy recovery device is completely bypassed under selected temperature conditions to allow the device to freeze and then later to be used under more favorable temperature conditions. In another example, the enthalpy recovery device is selectively bypassed during a system startup operation. One example includes a heater associated with the enthalpy recovery device. Another example includes preheating oxidant supplied to one portion of the enthalpy recovery device.

A system in one embodiment includes a detection unit, a boil-off auxiliary power unit, and a controller. The detection unit is configured to detect a characteristic of a boil-off gas stream from a cryotank configured to hold a cryogenic fluid. The boil-off auxiliary power unit is configured to receive the boil-off gas stream and use the boil-off gas stream to provide auxiliary power to a vehicle system. The controller is configured to acquire information from the detection unit corresponding to the characteristic; determine, using the information acquired from the detection unit, an available boil-off auxiliary energy that is available from the boil-off auxiliary power unit; determine a mode of operation of the vehicle system; determine a required auxiliary energy for the vehicle system; and to operate the auxiliary power unit based on the available boil-off auxiliary energy, the mode of operation, and the required auxiliary energy.

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 the turbine engine and a second fuel system for providing a cryogenic fuel composition and having a second fuel tank storing LNG and fluidly coupled to the turbine engine, an additive tank storing additives and fluidly coupled to the turbine engine and a mixing device configured to create the cryogenic fuel composition.

A low-temperature fuel cell assembly including of a low-temperature fuel cell (1) in combination with a sweeping gas circuit (2) for at least the anode part thereof. The fuel gas is prepared by filtering via a semi-permeable wall (5) and the yield from this process is increased by employing sweeping gas. This sweeping gas is obtained by producing it in the sweeping gas circuit (2). During operation some of the sweeping gas is continuously discharged and fresh sweeping gas is continuously produced. With this arrangement it is possible to use hydrogen as fuel gas. Sweeping gas is obtained by injecting air (8) and combusting (9) the oxygen contained therein with hydrogen. It is also possible to perform a methanisation reaction starting from hydrogen as fuel gas by providing CO / CO2 as a result of which the sweeping gas is methane.