Inventor

CLUM CAREY

US68 patents

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

CLUM CAREY

UNITED TECHNOLOGIES CORP

Chevron trip strip

Gas turbine engine component having engineered vascular structure

Self-modulated cooling on turbine components

Angled rail holes

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Leading edge hybrid cavities and cores for airfoils of gas turbine engine

Hot section engine components having segment gap discharge holes

Combustor panel cooling arrangements

Double wall turbine gas turbine engine blade cooling configuration

Aft flowing serpentine cavities and cores for airfoils of gas turbine engines

Leading edge hybrid cavities and cores for airfoils of gas turbine engine

Airfoil cooling

Tangential on-board injectors for gas turbine engines

Chevron trip strip

Cooling for gas turbine engine components

Airfoil having serpentine core resupply flow control

Turbine blade including balanced mateface condition

Dirt collector system

Trip strip and film cooling hole for gas turbine engine component

Airfoil having forward flowing serpentine flow

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Panel burn through tolerant shell design

Coriolis optimized U-channel with root flag

Airfoil having impingement leading edge

Coriolis optimized u-channel with platform core

Double wall turbine gas turbine engine blade cooling configuration

Airfoil having internal hybrid cooling cavities

Airfoil cooling circuit

Component having a dirt tolerant passage turn

Gas turbine engine component with film cooling hole

Airfoil cooling circuit

Tip cooling design

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Film cooling hole arrangement for gas turbine engine component

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine

Trailing edge pressure and flow regulator

Airfoil having impingement leading edge

Cooling configuration for a component

Conduit cooling system and method of supplying cooling fluid to a conduit

Gas turbine engine airfoil

Film hole with protruding flow accumulator

RAYTHEON TECH CORP

Leading edge hybrid cavities for airfoils of gas turbine engine

Panel burn through tolerant shell design

Airfoil having internal hybrid cooling cavities

Trailing edge pressure and flow regulator

Double wall turbine gas turbine engine blade cooling configuration

RTX CORP

Apparatus and method for mitigating airflow separation around engine combustor

Apparatus and method for mitigating particulate accumulation on a component of a gas turbine engine