Inventor

CLEMENTS JEFFREY DONALD

US59 patents

⚠️ This page may combine multiple inventors who share the name “CLEMENTS JEFFREY DONALD”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

CLEMENTS JEFFREY DONALD

GEN ELECTRIC

High tip speed gas turbine engine

High fan up speed engine

Counter rotating turbine with reversing reduction gearbox

Counter rotating turbine with reversing reduction gear assembly

Inlet pre-swirl gas turbine engine

Inlet pre-swirl gas turbine engine

Inlet pre-swirl gas turbine engine

Methods and apparatus for supplying cooling airflow in turbine engines

Torque monitoring device for a gas turbine engine

Supersonic single-stage turbofan engine

Aircraft and direct drive engine under wing installation

Counter rotating power turbine with reduction gearbox

Gas turbine engine

Counter rotating turbine with reversing speed reduction assembly

Method and system for mounting an aircraft engine

Interdigitated turbine engine air bearing and method of operation

Air bearing and thermal management nozzle arrangement for interdigitated turbine engine

Interdigitated counter rotating turbine system and method of operation

Interdigitated turbine engine air bearing cooling structure and method of thermal management

Three spool gas turbine engine with interdigitated turbine section

Two spool gas turbine engine with interdigitated turbine section

Turbine frame and bearing arrangement for three spool engine

Counter rotating turbine with reversing reduction gearbox

Gas turbine engine

Thermal structure for outer diameter mounted turbine blades

Turbine spider frame with additive core

Bleed valve assembly for a gas turbine engine

Bleed valve assembly for a gas turbine engine

Turbine engine with airfoil having high acceleration and low blade turning

Gas turbine engine with interdigitated turbine and gear assembly

Turbine incorporating endwall fences

Turbine engine and method of cooling thereof

Blended wing aircraft

Gas turbine engine with forward swept outlet guide vanes

Aircraft and direct drive engine under wing installation

High fan tip speed engine

Rotatable torque frame for gas turbine engine

Gas turbine engine

Interturbine frame for gas turbine engine

Turbine incorporating splitters

Gas turbine engine

Turbine engine with airfoil having high acceleration and low blade turning

Fuel leak combustion assembly for igniting a gaseous fuel leaking from a potential leak location

High temperature gas turbine engine

Gas turbine engine

CLEMENTS JEFFREY DONALD

Turbine assembly with end-wall-contoured airfoils and preferenttial clocking

Turbine nozzle with contoured band

PANDEY VIDHU SHEKHAR

Curved platform turbine blade

Banked platform turbine blade

GENERAL ELECTRIC COMPANY

Blended wing aircraft