INSTRUMENTED STATOR WITH EXTENDED INTERNAL PASSAGES

PRESSURE SENSOR MANIFOLDS FOR HIGH TEMPERATURES

Stationary blade segment, gas turbine, and method for producing stationary blade segment

FLUID PUMPS

PRE-CERAMIC THERMAL BARRIER FOR GAS TURBINE ENGINE COMPONENTS

Guide vane assembly for an aircraft turbine engine

Radial turbine nozzle and method for assembling the same

Ram-air duct system

Vane arc segment formed of fiber-reinforced composite

Rigid bar for electrically connecting a machine in an aircraft turbine engine

Fluid pumps

Fluid pumps

Variable geometry thruster

Vane arc segment formed of fiber-reinforced composite

Turbomachine equipped with an embedded electric machine having a segmented and movable stator

Method to produce a ceramic matrix composite with controlled surface characteristics

Wheel of a fluid flow machine

WALL DEPOSITION

Blade tip clearance assembly with geared cam

Turbine stator outer shroud cooling fins

Measurement system, rotary machine and measurement method for the same

Compressor section of gas turbine engine including shroud with serrated casing treatment

Cooling Of Rotor And Stator Components Of A Turbocharger Using Additively Manufactured Component-Internal Cooling Passages

Planetary gearbox assembly for a turbine engine

DE-ICING SYSTEM

Method for Distributing Relative Gap Parameters of Large-Scale High-Speed Rotary Equipment Components Based on Eccentricity Vector Following Measurement and Adjustment

Nacelle cowl hinge

Compressor case clearance control logic

Reduced leakage air seal

Multi-layer coating for a flow surface of an aircraft component

Wheel of a fluid flow machine

Non-contact seal with resilient biasing element(s)

Catch assembly for controlling opening of a door

Vacuum pump, spiral plate provided in vacuum pump, rotating cylinder and method for manufacturing spiral plate

Continuously compression molding a composite body with a complex geometry

Turbine exhaust structure of particular design

TURBINE ENGINE SHROUD

Turbine engine with a seal

Balancing system and method for turbomachine

Electrical machine

Rotatable component for turbomachines, including a non-axisymmetric overhanging portion

Turbine engine with component having a cooled tip

Cooling arrangement for a turbine casing of a gas turbine engine

Blade ring segment for turbine section, turbine section having the same, and gas turbine having the turbine section

Aft frame assembly for gas turbine transition piece

Methods for manufacturing composite components

STRUCTURAL FRAME INTEGRATED WITH VARIABLE-VECTORING FLOW CONTROL FOR USE IN TURBINE SYSTEMS

Turbine ring sector having an environmental barrier doped with an electrically-conductive element

Ceramic matrix composite airfoil repair

Non-contact seal with resilient biasing element(s)

Method for coating a component for the hot gas duct of a turbomachine

Steam turbine cooling unit

Hydrostatic non-contact seal with weight reduction pocket

Vane assembly and gas turbine including the same

Turbocharger having a meridionally divided turbine housing and a variable turbine nozzle

Ring-shaped compliant support

Airfoil with tie member and spring

Stator assembly for a gas turbine engine

Variable geometry thruster

Shroud for a gas turbine engine

Method for manufacturing a preform made of woven reinforcement fibers having a variable cross-section

Internal cooling of stator vanes

Sliding gear actuation for variable vanes

Gas turbine engine with a cooling fluid path

Converging flow joint insert system at an intersection between adjacent transitions extending between a combustor and a turbine assembly in a gas turbine engine

Wheel space purge flow mixing chamber

Method of monitoring rubbing between a rotary party and a stationary part in a rotating turbomachine, monitoring arrangement and turbomachine

Five-degree-of-freedom adjustment and positioning method and apparatus for assembly/measurement of rotor and stator of aircraft engine

Turbine component surface cooling system with passive flow modulation

Method for forming components using additive manufacturing and re-melt

Energy damping system for gas turbine engine stationary vane

Gimbal tube systems for tangential onboard injectors

GAS TURBINE LAMINATE SEAL ASSEMBLY COMPRISING FIRST AND SECOND HONEYCOMB LAYER AND A PERFORATED INTERMEDIATE SEAL PLATE IN-BETWEEN

Retention system for gas turbine engine assemblies

Turbine shroud block removal apparatus

Gas turbine engine exhaust mixer

Diffuser for a gas turbine

Shroud segment retainer

Ultra-High Efficiency Gas Turbine (UHEGT) with Stator Internal Combustion

Gas turbine engine anti-icing system

Structural frame integrated with variable-vectoring flow control for use in turbine systems

Aerodynamic track fairing for a gas turbine engine fan nacelle

Ring-shaped compliant support

Low leakage multi-directional interface for a gas turbine engine

Turbine stage for a turbine engine

Assembly fixture for a stator vane assembly

Gas turbine shroud assemblies

Compressor stator with contoured endwall

Gas turbine engine exhaust mixer

Bearing housing shroud

Assembly fixture with wedge clamps for stator vane assembly

Gas turbine stator vane

Assembly fixture for a stator vane assembly

Compressor casing treatment for gas turbine engine

Gas turbine vane with cooling channel end turn structure

Axial flow compressor, gas turbine system having the axial flow compressor and method of modifying the axial flow compressor

Guide vane for a gas turbine

Gas turbine

Turbine section architecture for gas turbine engine

Gas turbine engine exhaust mixer

Stator blade segment of a thermal turbomachine, associated production method and also thermal turbomachine

Turbine blade and diaphragm construction

Turbocharger with sliding piston assembly

Anti-rotation lock

Temperature tolerant vane assembly

Guide vane

Gas turbine engine stator vane stage

Airfoil profile for a turbine nozzle