Matches 1 - 14 out of 14


Match Document Document Title
US20150121886 GAS TURBINE ENGINE AFTERBURNER  
An afterburner is disclosed for use with a gas turbine engine and, in one form, is structured to receive a bypass air. The afterburner can be situated in a bypass duct and can be a toroidal...
US20090056340 AUGMENTOR WITH TRAPPED VORTEX CAVITY PILOT  
A gas turbine engine augmentor includes an annular trapped vortex cavity pilot having a cavity forward wall, a cavity radially outer wall, and a cavity aft wall, an annular cavity therebetween,...
US20090178414 FLAME HOLDER FOR MINIMIZING COMBUSTOR SCREECH  
A flame holder for an augmentor includes geometry to produce large radial variations in heat release to prevent coupling with modes within the exhaust duct that produce combustor screech. A...
US20070125086 DEVICE FOR ATTACHING A FLAME-ARRESTOR ARM TO AN AFTERBURNER CASING AND AFTERBURNER COMPRISING SUCH A DEVICE  
The invention relates to a device for attaching an afterburner to a turbojet casing (C), the afterburner comprising a flame-arrestor arm (1) comprising two longitudinal legs (7,8). According to...
US20140360197 AFTERBURNER AND AIRCRAFT ENGINE  
An aircraft engine includes an afterburner which has a flame stabilizer. The flame stabilizer maintains a flame generated from a mixed gas of a combustion gas and air. The flame stabilizer...
US20090260366 FLAME HOLDER FOR AN AFTERBURNER DUCT OF A JET ENGINE WITH A SPACER SHOE, AFTERBURNER DUCT, AND JET ENGINE COMPRISING AN AFTERBURNER DUCT  
The invention relates to a flame holder (10) for an afterburner duct of a jet engine, comprising an arm (100) in the form of a gutter forming a cavity, a shield (110) for protecting the cavity of...
US20110067407 FLAME-HOLDER DEVICE COMPRISING AN ARM SUPPORT AND A HEAT-PROTECTION SCREEN THAT ARE IN ONE PIECE  
A flame-holder device for the afterburning of a bypass turbojet, said turbojet comprising first and second internal annular casings, defining a passageway for a main flow, and an external annular...
US20100218505 AFTERBURNER CHAMBER FOR A TURBOMACHINE  
An afterburner chamber (10) comprising a burner ring (64) having housed therein an annular fuel strip (28) that is pierced by orifices (32, 34) and that is mounted inside an annular thermal...
US20170089300 AFTERBURNER AND AIRCRAFT ENGINE  
The present embodiment improves the durability of an afterburner and yet suppresses a reduction in the engine efficiency of an aircraft engine. A ring-shaped cooling channel through which cooling...
US20160305665 AFTERBURNER AND AIRCRAFT ENGINE  
The present embodiment sufficiently ensures the ignition stability and the flame-holding property of an afterburner while suppressing a reduction in the efficiency of an aircraft engine. A flame...
US20160169520 INJECTOR APPARATUS WITH REHEAT COMBUSTOR AND TURBOMACHINE  
Embodiments of the present disclosure provide an apparatus including: a first injector located on a surface of a turbine nozzle of a turbine stage positioned downstream of a reheat combustor,...
US20160169519 INJECTOR APPARATUS AND REHEAT COMBUSTOR  
Aspects of the present disclosure provide an apparatus including: an injector in fluid communication with an aft section of a reheat combustor in a power generation system, the aft section being...
US20160169518 INJECTING APPARATUS WITH REHEAT COMBUSTOR AND TURBOMACHINE  
Embodiments of the present disclosure provide an apparatus comprising: a reaction chamber positioned between a first turbine stage of a power generation system and a turbine stage of the power...
US20160069298 VARIABLE ORIFICE JET FOR A TURBINE ENGINE  
A fuel delivery system is provided for a turbine engine. This fuel delivery system includes a variable orifice jet configured to spray fuel received from a spray bar fuel conduit. The variable...

Matches 1 - 14 out of 14