Inventor

MORTON JEFFREY T

US42 patents

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

MORTON JEFFREY T

UNITED TECHNOLOGIES CORP

Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor

Combustor panel endrail interface

Directional cooling arrangement for airfoils

Turbine blade with tip vortex control and tip shelf

Internally cooled engine components

Float wall combustor panels having airflow distribution features

Combustor liner panel end rail with diffused interface passage for a gas turbine engine combustor

Turbine blade cooling hole arrangement

Turbine blade with contoured fillet

Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor

Combustor liner panel and rail with diffused interface passage for a gas turbine engine combustor

Blade outer air seal including cooling trench

Impingement cooling arrangement for airfoils

Airfoils having tapered tip flag cavity and cores for forming the same

Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor

Mateface for blade outer air seals in a gas turbine engine

Directional cooling arrangement for airfoils

Impingement cooling arrangement for airfoils

Woven skin cores for turbine airfoils

Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor

Gas turbine engine component with a cooling circuit having a flared base

RTX CORP

Telescoping guide vane for aircraft propulsion system

Turbine airfoil having cooling hole arrangement

Thermal management assembly for an aircraft propulsion system

Non-uniform and bi-tri stator spacing for swirl recovery vane (SRV) open rotor engines

Open rotor variable pitch blade with retracting inboard trailing edge

Translatable guide vanes for aircraft propulsion system

Thermal management system for gas turbine engine with open propulsor

Variable guide vane for aircraft propulsion system

SRV open rotor with core inlet forward of rotor

Open rotor with fixed guide vane/stator

Bifurcation integrated electrical system for hybrid aircraft propulsion system

Differential driven open rotor with brake

Open rotor aircraft propulsion system with bypass flowpath

Gas turbine engine with thermal management

AFT gear based engine with heat recovery system

Continuous flow fuel system

Open rotor aircraft propulsion system with bypass flowpath

Suction enabled post shutdown combustor cooling and core ventilation

RAYTHEON TECH CORP

Turbine blade cooling hole arrangement

Turbine blade trailing edge cooling feed

Turbine engine tip clearance control system with thrust bearing