SHROUD OF GAS TURBINE ENGINE AND METHOD OF MANUFACTURING THEREOF

WINDAGE COVER THAT COVERS FASTENERS COUPLING A RING GEAR ASSEMBLY TO AN OUTPUT SHAFT

Gas turbomachine diffuser assembly with radial flow splitters

Windage cover that covers fasteners coupling a ring gear assembly to an output shaft

Turbine engine component with deflector

Rotor and turbo machine including same

Connection device for a turbocharger, and turbocharger

Lubricant nozzle for a planetary gear set speed reducer of a turbomachine

Turbine stator blade cooled by air-jet impacts

Cooling passages for gas turbine engine component

Turbine engine with a seal

Blade/vane cooling passages

Inter-turbine ducts with flow control mechanisms

Assembly comprising a lubricating wheel and lubricant nozzles for a planetary gear speed reducer of a turbomachine

Double wall turbine gas turbine engine vane with discrete opposing skin core cooling configuration

Fluid collection gutter for a geared turbine engine

Double wall turbine gas turbine engine blade cooling configuration

Support rail truss for gas turbine engines

Inter-turbine ducts with flow control mechanisms

Strip seal axial assembly groove

Turbine for a turbine engine

Sealing structure for turbines, and turbine and gas turbine having the same

Turbine engine component with deflector

Turbine engine duct

Pin to reduce relative rotational movement of disk and spacer of turbine engine

Mounted ceramic matrix composite component with clamped flange attachment

Gas turbomachine diffuser assembly with radial flow splitters

Variable nozzle unit and variable displacement-type turbocharger

Blade comprising a shank, provided with a depressed portion

Floating, non-contact seal with angled beams

Dual walled component for a gas turbine engine

Component for a turbine engine with a hole

Seal device for turbine, turbine, and thin plate for seal device

Shrouded blade of a gas turbine engine

Film-cooled gas turbine component

Rotor with overhang at blades for a locking element

Seal-plate anti-rotation in a stage of a gas turbine engine

Hybrid exhaust nozzle

Method of manufacturing a component of a turbomachine, component of a turbomachine and turbomachine

Diffuser part for a gas turbine

Turbine shroud with clamped flange attachment

TURBINE COMPONENT THERMAL BARRIER COATING WITH CRACK ISOLATING ENGINEERED SURFACE FEATURES

Turbofan bypass air cooled oil cooler fairings

Gas turbine diffuser outer diameter and inner diameter wall strips for turbine exhaust manifold pressure oscillation reduction

Composite fan inlet blade containment

Gas turbine blade with corrugated tip wall

Mounting arrangement for variable stator vane

Cooled component

Knife edge with increased crack propagation life

Rotor and gas turbine engine including same

Method and apparatus for variable exhaust nozzle exit area

Turbocharger bearing housing oil groove

Turbine bucket closure assembly and methods of assembling the same

Cooled airfoil trailing edge and method of cooling the airfoil trailing edge

Turbine casing false flange flow diverter

Damping device for being situated between a housing wall and a casing ring of a housing of a thermal gas turbine

Liquified fuel backup fuel supply for a gas turbine

Component cooling channel

Nozzle with guiding devices

Reheat burner arrangement having an increasing flow path cross-section

Component having cooling channel with hourglass cross section

Components with cooling channels and methods of manufacture

COMPONENTS WITH COOLING CHANNELS AND METHODS OF MANUFACTURE

HOLLOW FAN BLADE RIB GEOMETRY

Blade outer air seal assembly leading edge core configuration

Device for reducing the noise emitted by the jet of an aircraft propulsion engine

Cable-actuated variable area fan nozzle with elastomeric seals

ROTOR ASSEMBLY FOR GAS TURBINES

STATOR-ROTOR ASSEMBLIES WITH FEATURES FOR ENHANCED CONTAINMENT OF GAS FLOW, AND RELATED PROCESSES

Component cooling channel

METHOD OF FABRICATING A COMPONENT USING A TWO-LAYER STRUCTURAL COATING

Cooled component wall in a turbine engine

Sealing device

Cooled conduit for conveying combustion gases

LEAF SEALS

NON-CIRCULAR PINS FOR CLOSURE GROUP ASSEMBLY

Systems and methods for passively directing aircraft engine nozzle flows

DUAL-FLOW TURBINE ENGINE FOR AIRCRAFT WITH LOW NOISE EMISSION

Gas turbine blade and gas turbine having the same

Method for improving the sealing on rotor arrangements

COMPLIANT PLATE SEAL WITH SELF-CORRECTING BEHAVIOR

Turbine airfoil cooling system with divergent film cooling hole

Nozzle with guiding elements

Rocket engine nozzle system

Methods and apparatus for mixing fluid in turbine engines

Compliant plate seals for turbomachinery

Systems and methods for passively directing aircraft engine nozzle flows

Compliant plate seal with an annular ring for turbomachinery and methods of assembling the same

Compliant plate seals for turbomachinery

Compliant plate seals for turbomachinery

Gas turbine blade shroud

Method and device for reducing engine noise

Refractory metal core cooling technologies for curved leading edge slots

Eductor swirl buster

Turbine heat shield with ribs

Turbine nozzle with trailing edge convection and film cooling

Turbine blade turbulator cooling design

Airfoil with three-pass serpentine cooling channel and microcircuit

Method and device for reducing engine noise

Square ultra thrust reverser system

Component and turbine assembly with film cooling

Aircraft with gas turbine engine having outer bypass elements removed