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WO/2016/086322A1 |
Disclosed is a fireproof wall comprising a boiler wall that is formed by a tube wall (1) consisting of tubes (11) joined by connecting pieces (12), and comprising a fireproof protective lining (2) which is arranged in front of the boiler...
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WO/2016/083632A1 |
The invention relates to a heat radiation chamber for boilers, consisting of parallel bars which are equidistant from each other, attached to two rings and supported on legs. Said chamber is arranged inside the combustion chamber of boil...
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WO/2016/071305A1 |
The invention relates to a metal element (12) for anchoring an anti-erosion coating that is intended to be fastened alone in an isolated manner to a metal wall or assembled with other identical anchoring elements. The anchoring element (...
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WO/2016/062581A1 |
The invention relates to a heat shield element (1) comprising a wall (2) having a hot side (3) and an opposing cold side (4), a peripheral edge (5) having an inner side (6) and an outer side (7), and a securing device (8) arranged substa...
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WO/2016/059117A1 |
The invention relates to a boiler or furnace (10) for combustion of fuel in an air staged combustion mode, comprising an enclosure (12) having walls (16) defining a combustion chamber (14), of which walls (16) at least a part is provided...
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WO/2016/050535A1 |
The invention relates to a heat shield element (50) for a heat shield (24) of a combustion chamber (10), comprising a hot side (32) which can be exposed to hot gas, an opposite cold side (34), and peripheral sides (36a, 36b); the heat sh...
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WO/2016/050830A1 |
The present invention relates to refractory tile systems for covering an internal wall of a high temperature furnace or boiler, comprising a base tile having a front face and a back face, and a shielding tile having a front face and a ba...
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WO/2016/048466A1 |
A sensor assembly (120) for a flame sensor apparatus (110) includes a photodiode that generates a current. The sensor assembly (120) includes a seal assembly supporting the photodiode. The seal assembly includes an inner conductor defini...
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WO/2016/036379A1 |
An acoustically dampened gas turbine engine having a gas turbine engine combustor (12) with an acoustic damping resonator system is disclosed. The acoustic damping resonator system (14) may be formed from one or more resonators (16) form...
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WO/2016/036380A1 |
An acoustically dampened gas turbine engine having a gas turbine engine combustor (12) with an acoustic damping resonator system (10) is disclosed. The acoustic damping resonator system (10) may be formed from one or more resonators (16)...
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WO/2016/024006A1 |
A burner device (190) comprising an air intake, a burner head (192) including an ignition device, a body section (196) defining a fluid flow channel between said air intake and said burner head (192), and a gas injector (205) for injecti...
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WO/2016/003300A1 |
A combustion chamber for a gas-fired heat exchanger according to the invention, open on one side and fitted with a burner, is characterised in that there is a space (3) formed between its inner jacket (2) and its outer jacket (1) to acco...
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WO/2016/001463A1 |
The invention relates to a burning grate (8) for biomass burners that has in the surface thereof a plurality of perforations, in the form of holes (12) and slots (13), to allow combustion air from the lower zone (33) of the combustion ch...
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WO/2015/193220A1 |
The invention relates to carburetor heads (1) for partial oxidation of gaseous and liquid carburetion substances and to a method for partial oxidation of gaseous and liquid carburetion substances. The carburetor head (1) has a protection...
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WO/2015/185695A1 |
The invention relates to a heat protection assembly (2, 30) for a charging installation (1) of a metallurgical reactor. In order to increase the lifetime of a heat protection shield in a charging installation of a metallurgical reactor, ...
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WO/2015/187007A1 |
Refractory lining of a tube wall (2) for an incinerator, comprising at least four refractory tiles (3) of ceramic material, which are arranged next to and above one another, wherein the tiles at their rear side, which is facing the tube ...
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WO/2015/173548A1 |
A device for the flameless oxidation of fuel, for example comprising a flameless oxidation burner, is described. The device comprises a first conduit to convey a fluid fuel phase to a first outlet and direct a primary jet comprising the ...
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WO/2015/158441A1 |
The invention relates to a refractory ceramic batch composition for producing an unshaped refractory ceramic product; to the use of a batch composition of this type for lining metallurgical melting vessels; and to a metallurgical melting...
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WO/2015/155391A1 |
The invention relates to a fire protection device for metal fireplaces, capable of making use of heat and of the type that comprises an auxiliary double pipe together with an insulating head and a hot air outlet head. The device has been...
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WO/2015/155733A1 |
A combustor (2) for a liquid propellent motor (1) has an elongated hollow tubular casing (4) having an inner wall (12) delimiting a combustion chamber (8) for the liquid propellent and an outlet nozzle (11) for the combustion products, a...
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WO/2015/147932A2 |
A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a major dilution passage having a lip and a first seal boss. The liner panel also includes a minor dilution passage having a second seal b...
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WO/2015/147929A2 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall, which includes a shell, a heat shield and an annular body. The body at least partially defines a first aperture through the shell and t...
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WO/2015/147938A2 |
A combustor wall assembly has a heat shield and a supporting shell with a cooling cavity defined therebetween. A grommet generally includes a wall defining a dilution hole isolated from the cooling cavity, and a flange projecting radiall...
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WO/2015/142411A2 |
An article such as a heat shield panel includes a substrate and a multi-layered coating supported on the substrate. The multi-layered coating can include alternating layers of different ceramic material compositions having individual thi...
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WO/2015/129082A1 |
Provided are a structure for a burner having exceptional corrosion resistance, heat resistance, and wear resistance, and a wet bottom furnace equipped with the burner. The burner is provided with a burner body installed by being passed t...
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WO/2015/129083A1 |
Provided is a method for preventing peeling of molten slag and solid phase slag in a wet bottom furnace, in order to protect the furnace wall. In this wet bottom furnace, a ceramic film (11) having a contact angle of 90 degrees or less w...
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WO/2015/122281A1 |
Provided is a burner tile which has favorable fire resistance, heat resistance, wind corrosion resistance, and thermal shock resistance. A burner tile (1E) is formed from an inorganic fiber molded body and has a burner-use main hole (3E)...
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WO/2015/122950A2 |
A structure is provided for a turbine engine. The structure includes a shell with a first surface, and a heat shield with a textured second surface and a textured third surface. The texture of a portion of the second surface is different...
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WO/2015/116360A1 |
A heat resistant panel has a bulkhead and a swirler adjacent a combustion chamber. The heat resistant panel comprises an inner panel for facing the combustion chamber and defining a first exit port at an upstream end thereof configured t...
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WO/2015/116269A2 |
An assembly for a turbine engine includes a combustor wall. The combustor wall includes a shell, a heat shield and an annular land. The heat shield is attached to the shell. The land extends vertically between the shell and the heat shie...
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WO/2015/117137A1 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall including a shell and a heat shield. The combustor wall defines first and second cavities between the shell and the heat shield. The hea...
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WO/2015/117139A1 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall with a shell and a heat shield. The combustor wall defines a quench aperture therethrough. The combustor wall also defines a cavity betw...
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WO/2015/116937A1 |
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a cone shaped pin.
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WO/2015/110316A1 |
The invention relates to a silo combustion chamber (10) for a gas turbine (1), comprising a cylindrical flame tube (34) which is provided with a cylindrical casing (44) on the tube outer face, thereby forming a gap (45). A first base sur...
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WO/2015/112221A2 |
A combustor for a turbine engine is provided that includes a combustor wall. The combustor wall includes a shell and a heat shield, which is attached to the shell. One or more cooling cavities are defined between the shell and the heat s...
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WO/2015/112216A2 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall, which includes a shell and a heat shield. The heat shield includes a base and a plurality of panel rails. The panel rails are connected...
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WO/2015/112220A2 |
A combustor wall is provided for a turbine engine. The combustor wall includes a shell and a heat shield that is attached to the shell. The heat shield includes a rail and a cooling element connected to the rail in a cavity. The cavity e...
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WO/2015/108584A2 |
An annular grommet is provided for a wall assembly of a combustor section of a gas turbine engine. The annular grommet includes a wall that at least partially defines a chamber. A wall assembly within a gas turbine engine includes a line...
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WO/2015/101887A1 |
The present invention concerns an unshaped product comprising a particulate mixture consisting of: - a coarse fraction, representing more than 50% and less than 91% of the particulate mixture, in mass percentage, and consisting of partic...
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WO/2015/103357A1 |
A liner panel is provided for use in a gas turbine engine. The liner panel includes an intermediate rail that extends from a cold side of a liner panel. The liner panel also includes a multiple of heat transfer augmentors, which generall...
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WO/2015/102736A2 |
A combustor for a turbine engine includes an inner liner panel with a multiple of inner dilution passages. The multiple of dilution passages includes a repeating pattern of a first major inner air passage, a minor inner air passage, and ...
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WO/2015/100346A1 |
A combustor component defining a dilution hole configuration for a combustor wall assembly of a gas turbine engine has first and second dilution holes that communicate radially with one-another and with respect to respective centerlines ...
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WO/2015/095759A1 |
A thermal mechanical dimple array for combustor liners of gas turbine engines are located at known hot spots along the liner to reduce stress and minimize cracking. Such arrays have indentations in the liners at the hot spots that act to...
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WO/2015/090578A1 |
In a mobile warm air heating apparatus (1) comprising a movable housing (2) and an electrically operated fan (7) for sucking and introducing ambient air into the housing (2), the waste heat from a burner (10) heats the introduced air, an...
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WO/2015/094430A1 |
A liner panel for use in a gas turbine engine. The liner panel has a hot side and a cold side. The liner panel includes a rail extending from the cold side and a multiple of studs extending from the cold side. At least one of the multipl...
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WO/2015/088467A1 |
The invention relates to heating devices and can be used in heating systems. A long-burning boiler includes a housing having a double wall, a combustion chamber, two air ducts having independent outer apertures with slide-gates, a boiler...
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WO/2015/084450A2 |
A case is provided for a gas turbine engine. The case includes a wall defining a through-hole. The case also includes first and second pockets adjacent to, and on opposite sides, of the through hole. A method of reducing stress in a case...
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WO/2015/085065A1 |
An assembly is provided for a turbine engine. A combustor wall of the turbine engine assembly includes a shell, a heat shield and an annular body engaged with the shell and the heat shield. The annular body extends through the combustor ...
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WO/2015/084444A1 |
A wall assembly is provided for a gas turbine engine. This wall assembly includes a support shell with a contoured region; and a multiple of liner panels mounted to the support shell. At least one of the multiple of liner panels includes...
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WO/2015/085080A1 |
An assembly is provided for a turbine engine. This turbine engine assembly includes a combustor wall. The combustor wall includes a shell, a heat shield and an annular body. The body extends laterally between an inner surface and an oute...
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