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Patent Searching and Data


Matches 151 - 200 out of 6,146

Document Document Title
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 ...  
WO/2015/047472A2
A liner panel for use in a combustor of a gas turbine engine includes a substrate with a hot side and a cold side; a bond coat on at least one of the hot side and the cold side of the substrate; and a convective feature on the cold side ...  
WO/2015/044413A1
The invention relates to a heat shield (20, 40) with a support structure (22) and a number of heat shield blocks (24, 42, 44, 56, 56a) which are arranged substantially over the entire surface of the support structure such that expansion ...  
WO/2015/047509A2
A liner panel for use in a combustor of a gas turbine engine includes a nozzle includes an inner periphery along an axis. The inner periphery includes a flow guide around the axis. A wall assembly for use in a combustor of a gas turbine ...  
WO/2015/039074A1
A combustor of a gas turbine engine includes a multiple of liner panels mounted to the support shell, at least one of the multiple of liner panels includes a first impingement cavity that operates at a first pressure and a second impinge...  
WO/2015/038293A1
A combustor includes a liner and a support. The liner includes first and second spaced apart liner walls defining a combustion chamber therebetween, and an end wall joining the first and second liner walls at a forward end. The support i...  
WO/2015/039075A1
A wall assembly for use in a combustor of a gas turbine engine includes a transverse structure with at least one effusion passage that extends at an angle α therethrough. The effusion passage includes an inlet in an outer periphery of a...  
WO/2015/034861A1
A heat shield for a combustor includes a ring shaped body including a central opening defining a radially inner edge of the ring shaped body. The ring shaped body is at least partially made of a ceramic material. The heat shield includes...  
WO/2015/033679A1
A duct wall surface structure wherein, in a flue which carries a solid-gas two-phase flow and is formed by a duct made of steel plates, and is equipped with hoppers, the solid particle trapping efficiency in the hoppers is improved, ther...  
WO/2015/031816A1
A wall assembly for a combustor of a gas turbine engine is provided. The wall assembly includes a support shell with a contoured region to define at least one convergent passage between the support shell and a multiple of liner panels. A...  
WO/2015/022222A1
The invention relates to a heat shield (30) for a combustion chamber (25). The heat shield comprises a support structure (32), a number of heat shield elements, and at least one Helmholtz resonator (48), wherein the heat shield elements ...  
WO/2015/023576A1
One exemplary embodiment of this disclosure relates to a gas turbine engine including a plate, a frame attached to the plate, and a panel. The panel is supported by the frame.  
WO/2015/023339A2
A liner panel for a combustor of a gas turbine engine includes a multiple of heat transfer augmentors which extend from a cold side thereof. At least one of the multiple of heat transfer augmentors includes a first heat transfer augmenta...  
WO/2015/023733A1
An apparatus (8) for dampening acoustic pressure oscillations of a gas flow contained in part by a combustor wall of a gas turbine engine combustor (14). The apparatus (8) includes at least one resonating tube (10) with a closed end, an ...  
WO/2015/011623A1
A sintered refractory product having the form of a block and consisting- of a granulate formed by all the grains having a size larger than 100 μm, referred to as "coarse grains", and - a matrix binding said coarse grains and consisting ...  
WO/2015/007252A1
Method of gas combustion in industrial furnaces using a burner provided with an injector (1) and a shaped piece (2), wherein the injector (1) consists of either an inner gas nozzle (11) equipped with a main regulation valve (111) or of t...  
WO/2015/007743A1
A method of gas combustion in industrial furnaces, especially in glass furnaces or furnaces for metal melting,by the help of a multi nozzle burner with controllable flow of nozzles of fuel gas and additional gas, where the essence of the...  
WO/2015/001517A1
A tile for covering combustion chambers, in particular for gas turbine energy production power plants, is provided with a main body (23), which extends along a longitudinal axis (B) and is provided with: • a main face (24), which faces...  
WO/2015/002686A2
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 hemi-spherical protuberance.  

Matches 151 - 200 out of 6,146