TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL

TURBINE ENGINE WITH A BLADE ASSEMBLY HAVING A DOVETAIL

TURBOMACHINE FOR A FLIGHT PROPULSION DRIVE

SYMMETRICAL TWO-PIECE HOLLOW-VANE ASSEMBLY JOINED VIA BRAZING ALONG AIRFOIL CENTERLINE

GAS TURBINE ENGINE

Fan housing, fan and operating system having a fan

Engine components with cooling holes having tailored metering and diffuser portions

Contoured endwall for a gas turbine engine

TURBINE WHEEL ASSEMBLY WITH PLATFORM RETENTION FEATURES

Turbine rotor blade assembly

TRREN exhaust nozzle-M-spike turbo ram rocket

Spline for a turbine engine

SPLINE FOR A TURBINE ENGINE

Spline for a turbine engine

SPLINE FOR A TURBINE ENGINE

Flight vehicle air breathing propulsion system with isolator having obstruction

Apparatus for transferring energy between a rotating element and fluid

Centrifugal Pump Blade Profile

Fuel distribution device, gas turbine engine and mounting method

Low wear radial flow impeller device and system

Engine components with cooling holes having tailored metering and diffuser portions

Cooling features with three dimensional chevron geometry

Housing element for an intermediate turbine housing

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

Reversible blade rotor seal with protrusions

Asymmetric diffuser opening for film cooling holes

Extruded profile for manufacturing a blade of an outlet guide vane

Turbine blade cooling structure

Plate for metering flow

Apparatus for transferring energy between a rotating element and fluid

Double-jet type film cooling structure

Accessory gearbox with internal layshaft

Gas turbine engine steam injection manifold

Bipedal damper turbine blade

Cast integrally bladed rotor with bore entry cooling