| Document |
Document Title |
|
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.
|
|
WO/2014/207207A1 |
The invention relates to a heat shield (2) with a support structure (28) and a number of heat shield blocks (20, 22), said heat shield blocks being secured to the support structure (28) and having a cold side (26) facing the support stru...
|
|
WO/2014/200588A2 |
A combustor of a gas turbine engine includes an additively manufactured liner panel with a heat transfer augmentation feature.
|
|
WO/2014/197045A2 |
A liner assembly for a combustor of a gas turbine engine according to one disclosed non-limiting embodiment of the present disclosure includes a grommet with a multiple of grommet cooling passages.
|
|
WO/2014/187659A1 |
The invention relates to a heat shield tile (10), which can be detachably arranged on a bearing structure of a heat shield (120) by means of at least one retaining element. The heat shield tile has a cold side (1) facing the bearing stru...
|
|
WO/2014/189556A2 |
A heat shield for a combustor of a gas turbine engine includes a first edge with a first set of cantilevered members and a second edge with a second set of cantilevered members.
|
|
WO/2014/173568A1 |
The invention relates to a heat shield block (30) for a heat shield (20, 22) of a gas turbine (1), which heat shield block can be detachably fastened to a supporting structure (24) by means of at least one retaining element (26, 28). The...
|
|
WO/2014/173660A1 |
The present invention relates to a combustion system of a flow engine comprising at least one combustion chamber, a shared manifold (18) to feed a flow medium via at least two injectors to the at least one combustion chamber and at least...
|
|
WO/2014/168383A1 |
The present invention provides a flameless combustion industrial furnace, using reverse air injection technique, which is capable of enhancing combustion efficiency and solving a problem of an acidic gas at the same time by injecting air...
|
|
WO/2014/162074A1 |
The method of the invention comprises a premix burner formed by a group of premix nozzles (2) disposed in a circle of diameter DB around a central nozzle (4) disposed on a central axis A of the burner (1) and intended to create a radial ...
|
|
WO/2014/155889A1 |
This heat storage-type exhaust gas purification device is provided with: a combustion chamber which burns and decomposes components contained in exhaust gas; heat storage chambers which each have one end connecting to the combustion cham...
|
|
WO/2014/158252A1 |
An improved fastening system (42) and method overcomes traditional thermal mismatch that occurs with standard fastener systems that are employed in extreme temperature environments. The fastening system (42) could employ a metallic faste...
|
|
WO/2014/143971A1 |
An apparatus, system, and method for heating fluidic material includes a sleeve positioned within a housing, with at least a portion of at least one heating element passing through the sleeve and an annulus defined by an exterior surface...
|
|
WO/2014/133615A1 |
An improved seal assembly (42) for use with a combustion liner assembly is employed with a gas turbine engine (10) so as to control fluid flow. The seal assembly has a bi-metal sealing member (44) that is affixed to a first surface that ...
|
|
WO/2014/131876A1 |
The invention relates to a damping device (50) for a gas turbine, said damping device having: • - at least one Helmholtz resonator (23) and • - at least one duct (53), • - wherein the Helmholtz resonator has a resonator housing (27...
|
|
WO/2014/127307A1 |
A perforated flame holder and burner including a perforated flame holder provides reduced oxides of nitrogen (NOx) during operation. The perforated flame holder includes a pattern of elongated apertures extending between a proximal and a...
|
|
WO/2014/116929A1 |
A fired heater unit is disclosed having a radiant section having a high emissivity coating therein. The fired heater unit also includes a burner for mixing fuel and preheated air to produce flue gas to be used in heating operations withi...
|
|
WO/2014/104625A1 |
The present invention relates to a gas boiler, including: a burner that combusts a pre-mixed gas and has a burner flange formed in the circumferential direction; a gas supply chamber in which the upper portion of the burner is received a...
|
|
WO/2014/099193A1 |
Two or more unipolar voltage generation systems may apply respective voltages to separate but complementary electrodes. The complementary electrodes may be disposed substantially congruently or analogously to one another to provide bipol...
|
|
WO/2014/091269A1 |
The invention relates mainly to a refractory material in contact with a coated metallic element (2). The invention also relates to a lining made from such a refractory material and to installations that may include such a lining. The inv...
|
|
WO/2014/087045A1 |
An arrangement comprising a thermal device (100) and a surface (150) reflecting and/or scattering electromagnetic radiation (215) in the inner part of the thermal device (100). The arrangement also comprises a source (210) of electromagn...
|
|
WO/2014/083016A1 |
The invention relates to the use of unfired, carbon carrier-free refractory products, particularly shaped by pressing or unshaped, and containing binders and granules of said refractory materials that form a ceramic bond at temperatures ...
|
|
WO/2014/074369A1 |
An acoustically dampened gas turbine engine having a combustor with an acoustic damping system is disclosed. The acoustic damping system may be formed from an acoustic damping body having at least one orifice configured to receive a comb...
|
|
WO/2014/071016A1 |
A diagnostic tool and method of spectroscopic analysis of fuel combustion in a combustion chamber of an internal combustion engine. The method carried out by the diagnostic tool includes the steps of: (a) introducing a mixture of fuel, a...
|
|
WO/2014/065187A1 |
The present invention is provided with: an outer casing (15) inserted into a high-temperature furnace, the outer casing (15) being formed having a bottomed cylindrical shape, a cooling water supply port (23) through which cooling water (...
|
|
WO/2014/064300A1 |
The invention relates to a vertical boiler that operates with solid fuels such as, for example, biomass, coal, wood, etc. The boiler comprises a furnace divided into two sections, namely: a lower section in which partial combustion of th...
|
|
WO/2014/064474A1 |
The present invention relates to an insert unit for improving the burning efficiency of gas burners, which contains a burner stone (1) that can be connected to the gas burner, where the burner stone (1) has a flow channel (2), and the bu...
|
|
WO/2014/061453A1 |
Provided is a fluidized bed combustor capable of lengthening the life of a thermometer even when a protective tube is made from an inexpensive material identical to that of the prior art. This fluidized bed boiler (100) is equipped with ...
|
|
WO/2014/048829A1 |
A combustion plant (10) for the combustion of a fuel, having a combustion chamber wall (12) which surrounds a combustion chamber (11), wherein at least one sensor device (13) is arranged so as to extend through the combustion chamber wal...
|
|
WO/2014/044654A2 |
The invention relates to a device (20, 29, 48, 64) for cooling a supporting structure of a heat shield (33, 60). With the device for cooling a supporting structure of a heat shield, scaling of the supporting structure due to the intake o...
|
|
WO/2014/044673A2 |
The invention relates to a retaining element (22, 54) for retaining a heat shield block on a supporting structure (43), comprising at least one fastening section (23) that can be fastened to the supporting structure and at least one reta...
|
