Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 151 - 200 out of 6,186

Document Document Title
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...  
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...  
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...  
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...  
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, ...  
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 ...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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)...  
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...  
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...  
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...  
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...  
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...  
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.  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
WO/2015/077592A1
A multi-walled structure is provided for a turbine engine. This structure includes a shell with a textured first surface, and a heat shield with a second surface. The heat shield is attached to the shell. The first and the second surface...  
WO/2015/070953A1
The invention relates to a furnace wall arrangement of an industrial furnace having a furnace wall and having at least one protective element which is composed of fire-resistant material and which is fastened at one end to an inner face ...  
WO/2015/074052A1
A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a first liner panel side edge between a liner panel aft edge and a liner panel forward edge. The liner panel also includes a second liner ...  
WO/2015/066585A1
A reflective pilot light viewer is disclosed. The reflective pilot light viewer has an attachment flange securable to a water heater tank by fasteners. The reflective pilot light viewer also has a viewing segment joined to the attachment...  
WO/2015/065579A1
A liner panel within a gas turbine engine includes a perimeter rail that defines a first height from a cold side. The liner panel also includes an intermediate rail that defines a second height from the cold side, where the second height...  
WO/2015/054115A1
A combustor wall is provided for a turbine engine and includes a combustor shell and a heat shield. The heat shield is attached to the shell with first and second cavities extending between the shell and the heat shield. The first cavity...  
WO/2015/054244A1
A combustor wall is provided for a turbine engine. The combustor wall includes a shell, a heat shield and a combustion chamber. The heat shield is connected to the shell by a bonded connection, and defines a portion of the combustion cha...  
WO/2015/051136A1
An electrically enhanced combustor includes bilayer insulation. A thermal insulator protects an electrical insulator from high temperatures that could cause the electrical insulator to become at least somewhat electrically conductive.  
WO/2015/050592A2
A liner panel is provided for a combustor of a gas turbine engine. The liner panel includes a multiple of heat transfer augmentors. At least one of the multiple of heat transfer augmentors includes a depression, where the depression incl...  
WO/2015/050879A1
A combustor wall is provided for a turbine engine. The combustor wall includes a combustor shell and a combustor heat shield that is attached to the shell. The heat shield includes a first panel and a second panel that sealingly engages ...  

Matches 151 - 200 out of 6,186