Nozzle with Widely-Spaced Thrust Chambers, Engine Including the Nozzle, and Vehicle Including the Engine

ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED HEAT SHIELD

ATMOSPHERIC RE-ENTRY VEHICLE WITH SKEWED BASE HEAT SHIELD

EXHAUST DUCT FOR GAS TURBINE ENGINE

Non-axisymmetric heat shield, a nozzle defined at least partially by the heat shield, an engine including the nozzle, and a vehicle including the engine

Annular aerospike nozzle with widely-spaced thrust chambers, engine including the annular aerospike nozzle, and vehicle including the engine

FLOW SPLITTER

Seals for managing thermal distortion in a turbomachine and methods for building the same

Intermediate casing for a gas turbine engine

Gas turbine engine rotor assembly and method of using same

De-icing device for an air intake of an aircraft turbojet engine nacelle

Non-axisymmetric end wall contouring with forward mid-passage peak

BLADE FOR A GAS TURBINE ENGINE

Gas turbine engine rotor disc retention assembly

Ported shroud system for turboprop inlets

Compressor diffuser with diffuser pipes varying in natural vibration frequencies

Compressor diffuser with diffuser pipes having aero-dampers

NON-SYMMETRIC FAN BLADE TIP CLADDING

Flow mixer with a changing thickness

Blade for a gas turbine engine

Two-dimensional supersonic nozzle thrust vectoring using staggered ramps

Fan housing for reduced noise

Component for a turbine engine with a cooling hole

Bearing device and exhaust turbine turbocharger

Bushing arranged between a body and a shaft, and connected to the shaft

Flight vehicle air breathing propulsion system with isolator having obstruction

Variable nozzle mechanism and variable displacement type exhaust turbocharger

Asymmetric vane assembly

Planet-carrier for an epicyclic gearing and epicyclic gearing provided with such a planet carrier

NON-AXIALLY SYMMETRIC TRANSITION DUCTS FOR COMBUSTORS

Asymmetric load compensation system

Diffuser for a turbine engine and method of forming same

Unsymmetrical turbofan abradable grind for reduced rub loads

Turbine engine part with non-axisymmetric surface

Composite blade, comprising a leading-edge reinforcement made of another material

Inducer and pump

Blade outer air seal surface

Process of forming and a seal for an engine

Blade with a platform and a hollow bumper

Turbine nozzle having non-axisymmetric endwall contour (EWC) and profile

Turbine nozzle having non-axisymmetric endwall contour (EWC)

Turbine bucket having non-axisymmetric endwall contour and profile

Thrust reverser with asymmetric vane geometry

Gas turbine engine with short inlet and mistuned fan blades

Rotationally symmetrical part for a turbine engine rotor, and related turbine engine rotor, turbine engine module, and turbine engine

Housing for air cycle machine compressor

Impeller for an exhaust gas turbocharger

Compressor airfoil with compound leading edge profile

Asymmetric diffuser opening for film cooling holes

AXISYMMETRIC OFFSET OF THREE-DIMENSIONAL CONTOURED ENDWALLS

Nosecap

Variable area turbine vane row assembly

Extruded profile for manufacturing a blade of an outlet guide vane

Non-axisymmetric fan flow path

Exhaust duct

Air blower and outdoor unit

Plate for metering flow

Turbomachine blade tip shroud

Multi-lobed cooling hole

Gas turbine engine rotor disk-seal arrangement

Asymmetric fan nozzle in high-BPR separate-flow nacelle

Damper mass distribution to prevent damper rotation

Methods and apparatus for passive thrust vectoring and plume deflection

Turbomachine blade tip shroud

Rotor and gas turbine engine including a rotor

Device for locking a nut

Non-axisymmetric fixed or variable fan nozzle for boundary layer ingestion propulsion

Steam turbine nozzle segment having transitional interface, and nozzle assembly and steam turbine including such nozzle segment

Methods and apparatus for passive thrust vectoring and plume deflection

Functionally asymmetric two-sided turbocharger wheel and diffuser

Sirocco fan and air conditioner having same

Stator vane row

Bushing arranged between a body and a shaft, and connected to the body

Bushing arranged between a body and a shaft, and connected to the shaft

Blade outer air seal surface

Non-axisymmetric rim cavity features to improve sealing efficiencies

Bypass duct with angled drag links

Cooling hole with asymmetric diffuser

Turbomachine blade tip shroud

Non axis-symmetric stator vane endwall contour

Torque frame and asymmetric journal bearing for fan drive gear system

Vane assembly for a gas turbine engine

Centrifugal compressor having an asymmetric self-recirculating casing treatment

Rotor of an axial compressor stage of a turbomachine

Apparatus, method, and system for separating particles from a fluid stream

Exhaust system for steam turbine

Asymmetrical rotor blade slot attachment

Coupling element segments for a rotor of a turbomachine

Steam valve and generator set

Exhaust duct for gas turbine engine