Inventor

MORRISON JAY A

US70 patents

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

MORRISON JAY A

SIEMENS ENERGY INC

Attachment for ceramic matrix composite component

Multivane segment mounting arrangement for a gas turbine

Wavy CMC wall hybrid ceramic apparatus

Stacked laminate bolted ring segment

Stacked laminate fiber wrapped segment

Hollow CMC airfoil with internal stitch

Ceramic matrix composite wall with post laminate stitching

CMC with multiple matrix phases separated by diffusion barrier

Subsurface inclusion of fugitive objects and methodology for strengthening a surface bond in a hybrid ceramic matrix composite structure

Cooling arrangement for CMC components with thermally conductive layer

Method of forming CMC component

SIEMENS POWER GENERATION INC

Ceramic matrix composite vane with chordwise stiffener

Lamellate CMC structure with interlock to metallic support structure

Stacked laminate CMC turbine vane

Ceramic matrix composite airfoil trailing edge arrangement

Stacked lamellate assembly

Tabbed ceramic article for improved interlaminar strength

Ceramic material having ceramic matrix composite backing and method of manufacturing

CMC component and method of fabrication

In-situ formed thermal barrier coating for a ceramic component

Method of manufacturing a hybrid structure

Hybrid structure using ceramic tiles and method of manufacture

MORRISON JAY A

Grid ceramic matrix composite structure for gas turbine shroud ring segment

CMC wall structure with integral cooling channels

Methodology and tooling arrangements for increasing interlaminar shear strength in a ceramic matrix composite structure

Interlocked CMC airfoil

Process for making a wall with a porous element for component cooling

Method of joining ceramic parts and articles so formed

Gusset with fibers oriented to strengthen a CMC wall intersection anisotropically

Turbine vane with high temperature capable skins

SIEMENS WESTINGHOUSE POWER

Hybrid ceramic material composed of insulating and structural ceramic layers

High temperature erosion resistant, abradable thermal barrier composite coating

Ceramic composite vane with metallic substructure

Ceramic matrix composite gas turbine vane

Ceramic matrix composite having improved interlaminar strength

Composite structure formed by CMC-on-insulation process

CAMPBELL CHRISTIAN X

Turbine engine airfoil and platform assembly

Turbine airfoil with a compliant outer wall

Turbine airfoil with dual wall formed from inner and outer layers separated by a compliant structure

Gas turbine vane platform element

LEE CHING-PANG

Method of fabricating a nearwall nozzle impingement cooled component for an internal combustion engine

Two stage serial impingement cooling for isogrid structures

MERRILL GARY B

Subsurface inclusions of objects for increasing interlaminar shear strength of a ceramic matrix composite structure

Compressible ceramic seal

ALBRECHT HARRY A

Cooling systems for stacked laminate CMC vane

KELLER DOUGLAS A

Ceramic matrix composite attachment apparatus and method

MIKRO SYSTEMS INC

Cooling module design and method for cooling components of a gas turbine system

HSU JOHAN

Cooling arrangement for a turbine component

CHARRON RICHARD C

Assembly for directing combustion gas

JAMES ALLISTER W

Joining mechanism with stem tension and interlocked compression ring