Fan casing for a gas turbine engine

Gas turbine having a peripheral ring segment including a recirculation channel

Turbomachine casing including a device for preventing instability during contact between the casing and the rotor

Fan section

Ring structure of metal construction having a run-in lining

Method for restoring a radial clearance between the stator and rotor parts of a turbogenerating set

Vane with integral inner air seal

ABRADABLE MATERIAL COMPOSITION, A THERMOMECHANICAL PART OR CASING INCLUDING A COATING, AND A METHOD OF FABRICATING OR REPAIRING A COATING PRESENTING SAID COMPOSITION

Apparatus and method for coating a compressor housing

Rim seal for a gas turbine engine

Rotating member and method for coating the same

Gas turbine with a compressor with self-healing abradable coating

Turbine Blade With Recessed Tip

Method of manufacturing a turbomachine element and device obtained in this way

Blade outer air seal

Composite containment casings

Composite containment casings having an integral fragment catcher

Methods for making composite containment casings

Abradable labyrinth tooth seal

Run-in coating for gas turbines and method for producing same

Method for producing a contoured gap, and turbo-engine comprising contoured gap

Blade outer air seal with improved thermomechanical fatigue life

Systems and methods involving abradable air seals

Turbine blade with a cover plate and a protective layer applied to the cover plate

Segmented thermal barrier coating

Angled honeycomb seal between turbine rotors and turbine stators in a turbine engine

Method for producing abrasive tips for gas turbine blades

Patterned reduction of surface area for abradability

Abradable CMC stacked laminate ring segment for a gas turbine

Ring seal for a turbine engine

GAS TURBINE ENGINE WITH INTEGRATED ABRADABLE SEAL

Seal Arrangement and Method for Manufacturing a Sealing Body for a Seal Arrangement

Compressor rotor

Abradable component for a gas turbine engine

Ceramic matrix composite abradable via reduction of surface area

Steam turbine

Active retractable seal for turbo machinery and related method

Method for microstructure control of ceramic thermal spray coating

Turbine blade tip and shroud clearance control coating system

Methods and apparatus for fabricating a fan assembly for use with turbine engines

Dysprosia stabilized zirconia abradable

Ceramic matrix composite turbine engine components with unitary stiffening frame

Ternary carbide and nitride thermal spray abradable seal material

Methods and apparatus for fabricating turbine engines

Fan case abradable

RIM SEAL FOR A GAS TURBINE ENGINE

Rotor blade and method of fabricating same

Seal between relatively moveable members

High-temperature layered system for dissipating heat and method for producing said system

Abradable labyrinth tooth seal

RUB COATING FOR GAS TURBINE ENGINE COMPRESSORS

Device for attaching ring sectors around a turbine rotor of a turbomachine

Steam-cooled gas turbine bucker for reduced tip leakage loss

Turboengine and method for adjusting the stator and rotor of a turboengine

Turbine friendly abradable material

Thermal spray compositions for abradable seals

Gas turbine component

Thermally compliant turbine shroud mounting assembly

Fan rotor design for coincidence avoidance

Abradable material composition, a thermomechanical part or casing including a coating, and a method of fabricating or repairing a coating presenting said composition

Ceramic abradable material with alumina dopant

Abradable seal between a turbine rotor and a stationary component

Composite blade

Inlet coating for gas turbines

Process for producing a compressor

Gas turbine engine component having bypass circuit

Methods and apparatus for maintaining rotor assembly tip clearances

Gas turbine engine blade tip clearance apparatus and method

Gas turbine engine blade tip clearance apparatus and method

Removable abradable seal carriers for sealing between rotary and stationary turbine components

Pattern for the surface of a turbine shroud

Pattern for the surface of a turbine shroud

Rotor-stator device having an abradable coating film

Thermal spray composition and method of deposition for abradable seals

Low-mid turbine temperature abradable coating

Cellular materials

Thermal spray compositions for abradable seals

Cellular materials

Thermal spray compositions for abradable seals

Thermal spray compositions for abradable seals

Cantilevered stator stage

Gas turbine engine component having bypass circuit

Seal assembly for turbine, bucket/turbine including same, method for sealing interface between rotating and stationary components of a turbine

Inter-fluid seal assembly and method therefor

Gas turbine engine and method of producing the same

Rotating member and method for coating the same

7FAstage 1 abradable coatings and method for making same

Turbine shroud segment

Outer air seal (OAS) assembly for a gas turbine engine

Air seal for a turbine engine

Method and apparatus for ceramic matrix composite turbine shroud assembly

Gas turbine engine with fan track liner having triply periodic minimal surface reinforcement

Blade outer air seal with graded coating

Blade outer air seal with machinable coating

Advanced thermally conductive lightweight elastomeric seal

Abradable material and design for jet engine applications

Gas turbine engine component with copper oxide coating

Airfoil tip cleaning and assessment systems and methods

Aircraft with ram air turbine disk with generator having blade shroud ring integrated magnets

Turbine engine fan track liner with outer flange case mounting

System for addressing turbine blade tip rail wear in rubbing and cooling

Engine with cooling passage circuit for air prior to ceramic component

Blade containment device

Abradable composite material and method of making the same

Additive manufacturing of abradable mesh structure on ring segment surface

Turbine abradable layer with nested loop groove pattern

Turbine abradable layer with progressive wear zone terraced ridges

Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface

Turbine abradable layer with progressive wear zone multi depth grooves