Patents
Sitemap › F23 - Combustion apparatus; Combustion processes › F23R - Generating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers › F23R 3 - Continuous combustion chambers using liquid or gaseous fuel
Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092)
10/2014
10/21/2014US8863526 Fuel injector
10/21/2014US8863525 Combustor with fuel staggering for flame holding mitigation
10/21/2014US8863524 Burner
10/21/2014US8863523 System for supplying a working fluid to a combustor
10/16/2014US20140305128 Method for operating a combustion chamber and combustion chamber
10/14/2014US8857739 Air-cooled swirlerhead
10/14/2014US8857190 Heat shield element, in particular for lining a combustion chamber wall
10/14/2014US8857189 Gas turbine combustion burner
10/09/2014WO2014165084A1 A sensor housing
10/09/2014WO2014164429A1 Check valve for propulsive engine combustion chamber
10/09/2014WO2014163669A1 Combustor assembly for a gas turbine engine
10/09/2014US20140298814 Catalytic combustion air heating system
10/09/2014DE102014104454A1 Turbomaschinensystem mit einfachem Kreisprozess und Kraftstoffkondfitionierungssystem Turbomachinery system with simple cycle and Kraftstoffkondfitionierungssystem
10/09/2014DE102014104317A1 Lufterhitzungssystem mit katalytischer Verbrennung Air heating system with catalytic combustion
10/08/2014EP2786074A2 Device to lower nox in a gas turbine engine combustion system
10/07/2014US8851402 Fuel injection for gas turbine combustors
10/07/2014US8851401 Flat fan air assist injectors
10/07/2014US8850822 System for pre-mixing in a fuel nozzle
10/07/2014US8850821 System for fuel injection in a fuel nozzle
10/07/2014US8850819 Swirler, fuel and air assembly and combustor
10/07/2014US8850788 Burner including non-uniformly cooled tetrahedron vortex generators and method for cooling
10/02/2014WO2014160299A1 Combustor panel with increased durability
10/02/2014WO2014158252A1 Bi-metal fastener for thermal growth compensation
10/02/2014WO2014158243A1 Multi-passage diffuser with reactivated boundry layer
10/02/2014WO2014154931A1 Method and apparatus for burning hydrocarbons and other liquids and gases
10/02/2014WO2014154401A1 Gas turbine combustion chamber having secondary air flaps
10/02/2014US20140290259 Combustion systems and combustion system components for rotary ramjet engines
10/02/2014US20140290258 Method for the arrangement of impingement cooling holes and effusion holes in a combustion chamber wall of a gas turbine
10/02/2014US20140290257 Impingement cooling mechanism, turbine blade and cumbustor
10/02/2014US20140290256 Impingement cooling mechanism, turbine blade and combustor
10/01/2014EP2784394A1 Combustor and gas turbine
10/01/2014EP2784393A1 Gas turbine combustion chamber with secondary air flaps
10/01/2014EP2783159A1 Combustion chamber
09/2014
09/30/2014CA2625330C Combustor liner with improved heat shield retention
09/30/2014CA2577527C Turbine engine combustion chamber with tangential slots
09/30/2014CA2577523C Turbine engine annular combustion chamber with alternating attachments
09/25/2014WO2014152875A1 Gas turbine engine architecture with nested concentric combustor
09/25/2014WO2014150474A1 Gas turbine transition inlet ring adapter
09/25/2014WO2014150437A1 Gas turbine combustor exit piece with hinged connections
09/25/2014WO2014149288A1 Catalyst comprising oxygen storage component for treatment of gas turbine exhaust gases
09/25/2014WO2014149190A1 System and method for fuel blending and control in gas turbines
09/25/2014WO2014149108A1 Shell and tiled liner arrangement for a combustor
09/25/2014WO2014149081A1 Counter swirl doublet combustor
09/25/2014WO2014149078A1 Auxetic stucture with stress-relief features
09/25/2014WO2014148567A1 Combustor and gas turbine
09/25/2014WO2014148166A1 Combustor and gas turbine
09/25/2014WO2014147325A1 Injection system for a combustion chamber of a turbine engine, comprising an annular wall having a convergent inner cross-section
09/25/2014US20140283525 Two-branch mixing passage and method to control combustor pulsations
09/25/2014US20140283524 Nozzle system and method for starting and operating gas turbines on lowbtu fuels
09/25/2014US20140283522 Multi-injector micromixing system
09/25/2014DE102014100571A1 Düsensystem und Verfahren zum Start und Betrieb von Gasturbinen mit niedrigenergetischen Kraftstoffen Nozzle system and method for starting and operating gas turbines with low-energy fuels
09/25/2014DE102007004864C5 Brennkammer einer Gasturbine und Verbrennungssteuerverfahren für eine Gasturbine Combustor of a gas turbine and combustion control method for a gas turbine
09/24/2014EP2781838A1 Gas turbine combustor
09/24/2014EP2780636A1 Turbomachine combustor assembly and method of operating a turbomachine
09/24/2014EP2780635A2 Combustion chamber for a gas turbine and gas turbine as well as a method
09/23/2014US8839628 Methods for operating a gas turbine engine apparatus and assembling same
09/23/2014US8839626 Gas turbine combustor including a transition piece flow sleeve wrapped on an outside surface of a transition piece
09/23/2014US8839624 Combustion device of a gas turbine including a plurality of passages and chambers defining helmholtz resonators
09/18/2014WO2014143239A1 Lean azimuthal flame combustor
09/18/2014WO2014143209A1 Gas turbine engine combustor liner
09/18/2014WO2014141830A1 Fuel spray nozzle
09/18/2014WO2014141825A1 Combustor and gas turbine
09/18/2014WO2014141397A1 Gas turbine combustor
09/18/2014WO2014139738A1 Jet burner with cooling duct in the base plate
09/18/2014WO2014139715A1 Cooled composite sheets for a gas turbine
09/18/2014US20140260319 Combustor support assembly for mounting a combustion module of a gas turbine
09/18/2014US20140260316 Gas turbine transition inlet ring adapter
09/18/2014US20140260315 System having multi-tube fuel nozzle with floating arrangement of mixing tubes
09/18/2014US20140260313 Micro-mixer/combustor
09/18/2014US20140260309 System and method for fuel blending and control in gas turbines
09/18/2014US20140260305 Lean azimuthal flame combustor
09/18/2014US20140260303 Methods relating to downstream fuel and air injection in gas turbines
09/18/2014US20140260302 DIFFUSION COMBUSTOR FUEL NOZZLE FOR LIMITING NOx EMISSIONS
09/18/2014US20140260300 Air diffuser for combustor
09/18/2014US20140260298 Combustor for gas turbine engine
09/18/2014US20140260297 Combustor for gas turbine engine
09/18/2014US20140260296 Slinger combustor
09/18/2014US20140260282 Gas turbine engine combustor liner
09/18/2014US20140260281 Auxetic structure with stress-relief features
09/18/2014US20140260280 Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine
09/18/2014US20140260279 Hot gas path duct for a combustor of a gas turbine
09/18/2014US20140260278 System for tuning a combustor of a gas turbine
09/18/2014US20140260277 Flow sleeve for a combustion module of a gas turbine
09/18/2014US20140260275 Flow sleeve assembly for a combustion module of a gas turbine combustor
09/18/2014US20140260273 Continuous combustion liner for a combustor of a gas turbine
09/18/2014US20140260271 System Having a Multi-Tube Fuel Nozzle
09/18/2014US20140260269 Systems and apparatus relating to downstream fuel and air injection in gas turbines
09/18/2014US20140260268 Micromixing cap assembly
09/18/2014US20140260267 Combustor end cover with fuel plenums
09/18/2014US20140260266 Combustor for gas turbine engine
09/18/2014US20140260265 Combustion chamber for a gas turbine and burner arrangement
09/18/2014US20140260262 Systems and apparatus relating to downstream fuel and air injection in gas turbines
09/18/2014US20140260260 Combustor for gas turbine engine
09/18/2014US20140260259 Multi-zone combustor
09/18/2014US20140260258 System for providing a working fluid to a combustor
09/18/2014US20140260257 Annular wall of a combustion chamber with improved cooling at the level of primary and/or dilution holes
09/18/2014DE102014103453A1 Systeme und Verfahren bezüglich der stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen Systems and procedures with respect to the downstream fuel and air injection in gas turbines
09/18/2014DE102014103088A1 System zur Steuerung der Flussrate eines komprimierten Arbeitsfluids zu einem Brennstoffinjektor eines Brenners System for controlling the flow rate of a compressed working fluid to a fuel injector of a burner
09/18/2014DE102014103087A1 System zur Zuführung von Brennstoff zu einer Brennkammer System for supplying fuel to a combustion chamber
09/18/2014DE102014103086A1 Systeme und Verfahren zur stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen Systems and methods for the downstream injection, fuel and air in gas turbines
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