REHEAT ASSEMBLY FOR A GAS TURBINE ENGINE

FUEL SYSTEM WITH ELECTRIC GENERATOR INTEGRATED BOOST STAGE

PROPULSION SYSTEM FOR JET NOISE REDUCTION

AIR RECUPERATED ENGINE WITH AIR REINJECTION

Duplex Turbine Guide Vane Assembly

FLAME-HOLDER DEVICE FOR A TURBOJET AFTERBURNER, COMPRISING THREE-BRANCHED ARMS

Fuel injection device for a turbojet engine afterburner

Diffusion cone for the rear part of a jet engine incorporating a flame-holder ring at the trailing edge

Aircraft power plant with detonation combustion tube

Propulsion system with synergistic pusher type propeller

MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM

Duplex Turbine Guide Vane Assembly

MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM

Augmented drive of compressors via differential and multistage turbine

Trailing edge fuel injection enhancement for flame holding mitigation

Afterburner structure with self-excited sweeping oscillating fuel injection nozzles

PROPULSION SYSTEM FOR JET NOISE REDUCTION

Confluence structure of a primary stream and a secondary stream in a bypass turbine engine

REHEAT ASSEMBLY FOR GAS TURBINE ENGINE

Reheat assembly

Jet engine for aircraft

Multi-mode combined cycle propulsion engine

Systems and methods for spraying fuel in an augmented gas turbine engine

Augmented drive of compressors via differential and multistage turbine

Electric heating systems and methods for gas turbine engines and jet engines

Confluence structure of a primary stream and a secondary stream in a bypass turbine engine

Systems and methods for spraying fuel in an augmented gas turbine engine

Electric heating systems and methods for gas turbine engines and jet engines

Afterburner strut with integrated fuel feed lines

Multistage gas turbine engine with differential drive of compressor

Augmented drive of compressors via differential and multistage turbine

MICRO-TURBINE GAS GENERATOR AND PROPULSIVE SYSTEM

Gas turbine engine shaft break mitigation

Vertical lift single engine vehicle system

HIGH SPEED PROPULSION SYSTEM WITH INLET COOLING

Combustion section and fuel injector assembly for a heat engine

Afterburner system for turbofan engine

Gas turbine engine with a unitary structure and method for manufacturing the same

Auxiliary device for three air flow path gas turbine engine

VARIABLE AREA EXHAUST MIXER FOR A GAS TURBINE ENGINE

Pressure zone spraybars

Jet engine with plasma-assisted afterburner having Ring of Resonators and Resonator with Fuel Conduit in Dielectric

Jet engine with plasma-assisted afterburner having Ring of Resonators and Resonator with Fuel Conduit

Jet engine with plasma-assisted afterburner having Resonator with Fuel Conduit

Jet engine with plasma-assisted afterburner

Combustor for a micro-turbine gas generator

Gas turbine engine with selective flow path

Aerospace turbofan engines

TRAILING EDGE BOX AND FUEL SPRAYBAR WITH INTERNAL PASSAGES

CAVITY SWIRL FUEL INJECTOR FOR AN AUGMENTOR SECTION OF A GAS TURBINE ENGINE

Coupling method and structure for a propulsion system hot section

COMBUSTION SYSTEM WITH INJECTOR ASSEMBLY INCLUDING AERODYNAMICALLY-SHAPED BODY AND/OR EJECTION ORIFICES

Spraybar face seal retention arrangement

Asymmetric load compensation system

Gas turbine engine including a re-heat combustor and a shaft power transfer arrangement for transferring power between low and high pressure shafts

Gas turbine exhaust cooling system

Augmentor vane assembly of a gas turbine engine with an additively manufactured augmentor vane

Flame-holder device

Tuned mass damper for tubes

Engine aft section structure

GAS TURBINE ENGINE

Gas turbine engine afterburner

Afterburner and aircraft engine

Thrust increasing device

Gas turbine engine with selective flow path

Afterburner and aircraft engine

Asymmetric load compensation system

Gas turbine engine and an airflow control system

Gas turbine engine and blocker door assembly

Pivoting stowable spray bar

Gas turbine engine system for modulating flow of fan by-pass air and core engine air

Gas turbine engine convergent/divergent nozzle with unitary synchronization ring for roller track nozzle

Variable orifice jet for a turbine engine

Reverse core gas turbine engine with high temperature third stream

Gas turbine engine systems and methods involving enhanced fuel dispersion

Carbureted fuel injection system for a gas turbine engine

High speed propulsion system with inlet cooling

Auxiliary device for three air flow path gas turbine engine

Variable area exhaust mixer for a gas turbine engine

Antagonist antibodies against EphB3

Gas turbine engine afterburner

GAS TURBINE AND GAS TURBINE AFTERBURNER

Mixing arrangement for mixing a fuel with a stream of oxygen containing gas

Cavity swirl fuel injector for an augmentor section of a gas turbine engine

Alignment system and methodology to account for variation in a gas turbine engine

Turbine engine alignment assembly

FLEXIBLE COMBUSTOR BRACKET

Coupling with one-piece plural nipples

Igniter for a turbomachine and mounting assembly therefor

Turbomachine flow control device

Spraybar face seal retention arrangement

Engine hot section vane with tapered flame holder surface

Method of using an afterburner to reduce high velocity jet engine noise

Apparatuses and systems with vertically and longitudinally offset mounting flanges

Leaf spring damper for a turbine engine fuel delivery system

Transition piece aft frame with fuel injection apertures

Augmentor spray bar with tip support bushing

Gas turbine engine and reheat system

Gas turbine engine systems and related methods involving thermally isolated retention

Device for mixing fuel and air of a jet engine

SYSTEM AND METHOD FOR CONTROLLING A GAS TURBINE ENGINE AFTERBURNER

THRUST AUGMENTED GAS TURBINE ENGINE

Flade discharge in 2-D exhaust nozzle

Side-initiated augmentor for engine applications

Combustor added to a gas turbine engine to increase thrust

Device for attaching a flame-holder arm to an afterburner housing

FLAME-HOLDER DEVICE COMPRISING AN ARM SUPPORT AND A HEAT-PROTECTION SCREEN THAT ARE IN ONE PIECE

MASKING ARRANGEMENT FOR A GAS TURBINE ENGINE

Augmentor pilot

Systems and methods involving reduced thermo-acoustic coupling of gas turbine engine augmentors

Gas turbine engine systems and methods involving enhanced fuel dispersion

Gas Turbine Burner and Method of Operating a Gas Turbine Burner

Gas turbine engine systems and related methods involving thermally isolated retention

Turbine engine valve assembly and method of assembling the same

Flame holder for minimizing combustor screech

Purged flameholder fuel shield

Gas turbine engine reheat fuel system

Media mixing insert for turbine blade in turbine engine

Brazed joint between a titanium-based metal part and a ceramic part based on silicon carbide (SIC) and/or carbon

Valve assembly for a gas turbine engine

Brazed joint between a metal part and a ceramic part

Joint between a metal part and a ceramic part based SiC and/or C

Out-flow margin protection for a gas turbine engine

Ceramic-encased hot surface igniter system for jet engines

Method and apparatus for assembling a flameholder for an augmenter

Segmented trapped vortex cavity

Turbine engine tailcone resonator

Augmentor variable vane flame stabilization

Valve assembly for a gas turbine engine

Device for mounting an air-flow dividing wall in a turbojet engine afterburner

Augmentor pilot nozzle

Structural track support of spraybars/tubing

Fixed nozzle thrust augmentation system

Plasma torch for ignition, flameholding and enhancement of combustion in high speed flows

Monobloc flameholder arm for an afterburner device of a bypass turbojet

Acoustic liner with bypass cooling

Architecture for an acoustic liner

IGNITER FOR INTERNAL COMBUSTION ENGINES OPERATING OVER A WIDE RANGE OF AIR FUEL RATIOS

Self powdered missile turbojet

Supersonic missile turbojet engine

Fladed supersonic missile turbojet

Acoustic dampers

Compact swirl augmented afterburners for gas turbine engines

Augmenter swirler pilot

Combustion device

Method and apparatus for detecting the presence of flame in the exhaust path of a gas turbine engine

Method and apparatus for providing an afterburner fuel-feed arrangement

Rocket augmentation for combined cycle turboaccelerator jet engine

Ventilation channels in an afterburner chamber confluence sheet

Method and apparatus for gas turbine engines

Retractable afterburner for jet engine

Method of improving the ignition performance of an after-burner device for a bypass turbojet, and an after-burner device of improved ignition performance

Device for fixing a burner ring in an afterburner combustion chamber of a turbojet engine

Ablative afterburner

Augmentor with axially displaced vane system

Turbo rocket with real carnot cycle

Igniter for internal combustion engines operating over a wide range of air fuel ratios

Method and system for failure accommodation of gas generator fuel metering system

Rotary injector

De-ice system and apparatus for turbine engines