Inventor

CUNHA FRANK J

US68 patents

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

CUNHA FRANK J

UNITED TECHNOLOGIES CORP

Turbine airfoil with enhanced heat transfer

Turbine element

Airfoil trailing edge cooling

Microcircuit cooling for a turbine blade

Turbine airfoil platform cooling circuit

Airfoil with three-pass serpentine cooling channel and microcircuit

Method and apparatus for cooling an airfoil

Airfoil with supplemental cooling channel adjacent leading edge

Turbine element

Impingement cooling of large fillet of an airfoil

Microcircuit airfoil mainbody

Airfoil with large fillet and micro-circuit cooling

Microcircuit cooling for a turbine airfoil

Film cooled multi-walled structure with one or more indentations

Cooling a quench aperture body of a combustor wall

Combustor liners with U-shaped cooling channels

Combustor bulkhead assembly

Microcircuits for small engines

Cooling for combustor liners with accelerating channels

Turbine engine multi-walled structure with internal cooling element(s)

Film cooling a combustor wall of a turbine engine

Grommet assembly and method of design

Cooling a quench aperture body of a combustor wall

Turbine engine multi-walled structure with cooling element(s)

Combustor quench aperture cooling

Cooling an aperture body of a combustor wall

Gas turbine engine combustor liner assembly with convergent hyperbolic profile

Gas turbine engine component with vascular cooling scheme

Microcircuit cooling for gas turbine engine combustor

Combustor wall with tapered cooling cavity

Heat shield panels with overlap joints for a turbine engine combustor

Stepped heat shield for a turbine engine combustor

Combustor wall aperture body with cooling circuit

Gas turbine engine combustor liner panel

Heat shield panels with overlap joints for a turbine engine combustor

Nozzle guide for a combustor of a gas turbine engine

Combustor wall assembly for a turbine engine

CUNHA FRANK J

Microcircuit cooling for gas turbine engine combustor

Gas turbine engine combustor

Distributed cooling for gas turbine engine combustor

Gas turbine engine combustor with integrated combustor vane having swirler

Gas turbine engine combustor with integrated combustor vane

Combustor liner with improved film cooling

Combustor liner with decreased liner cooling

Multi-stage amplification vortex mixture for gas turbine engine combustor

Combustor liner with reduced cooling dilution openings

Combustor liner with convergent cooling channel

SIEMENS WESTINGHOUSE POWER

Gas turbine row #1 steam cooled vane

Cooled turbine vane with endcaps

RAYTHEON TECH CORP

Cooling an igniter body of a combustor wall