Jay A. Morrison
85Patents
30h-index
53Co-inventors
87Inventor score
Filing activity: Mar 27, 1998 → Jun 1, 2016
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6514046B1 | Ceramic composite vane with metallic substructure | Mechanical Engineering; Lighting; Heating | 159 | Expired |
| US6648597B1 | Ceramic matrix composite turbine vane | Mechanical Engineering; Lighting; Heating | 145 | Expired |
| US6709230B2 | Ceramic matrix composite gas turbine vane | Emerging Cross-Sectional Technologies | 131 | Expired |
| US6197424A | Use of high temperature insulation for ceramic matrix composites in gas turbines | Emerging Cross-Sectional Technologies | 121 | Expired |
| US6758653B2 | Ceramic matrix composite component for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 112 | Expired |
| US7666475B2 | Method for forming interphase layers in ceramic matrix composites | Chemistry; Metallurgy | 99 | Active |
| US6235370A | High temperature erosion resistant, abradable thermal barrier composite coating | Emerging Cross-Sectional Technologies | 89 | Expired |
| US6733907B2 | Hybrid ceramic material composed of insulating and structural ceramic layers | Emerging Cross-Sectional Technologies | 83 | Expired |
| US6746755B2 | Ceramic matrix composite structure having integral cooling passages and method of manufacture | Emerging Cross-Sectional Technologies | 81 | Expired |
| US7824152B2 | Multivane segment mounting arrangement for a gas turbine | Mechanical Engineering; Lighting; Heating | 78 | Active |
| US6013592A | High temperature insulation for ceramic matrix composites | Chemistry; Metallurgy | 77 | Expired |
| US7950234B2 | Ceramic matrix composite turbine engine components with unitary stiffening frame | Mechanical Engineering; Lighting; Heating | 71 | Active |
| US7093359B2 | Composite structure formed by CMC-on-insulation process | Emerging Cross-Sectional Technologies | 63 | Expired |
| US7435058B2 | Ceramic matrix composite vane with chordwise stiffener | Mechanical Engineering; Lighting; Heating | 61 | Expired |
| US6641907B1 | High temperature erosion resistant coating and material containing compacted hollow geometric shapes | Emerging Cross-Sectional Technologies | 61 | Expired |
| US6617013B2 | Ceramic matrix composite having improved interlaminar strength | Emerging Cross-Sectional Technologies | 56 | Expired |
| US7874059B2 | Attachment for ceramic matrix composite component | Emerging Cross-Sectional Technologies | 55 | Active |
| US7153096B2 | Stacked laminate CMC turbine vane | Emerging Cross-Sectional Technologies | 50 | Expired |
| US7247002B2 | Lamellate CMC structure with interlock to metallic support structure | Mechanical Engineering; Lighting; Heating | 42 | Expired |
| US8118546B2 | Grid ceramic matrix composite structure for gas turbine shroud ring segment | Emerging Cross-Sectional Technologies | 39 | Active |
| US8257809B2 | CMC wall structure with integral cooling channels | Emerging Cross-Sectional Technologies | 39 | Active |
| US7066717B2 | Ceramic matrix composite airfoil trailing edge arrangement | Emerging Cross-Sectional Technologies | 39 | Expired |
| US8231354B2 | Turbine engine airfoil and platform assembly | Emerging Cross-Sectional Technologies | 37 | Active |
| US8061977B2 | Ceramic matrix composite attachment apparatus and method | Mechanical Engineering; Lighting; Heating | 36 | Active |
| US7247003B2 | Stacked lamellate assembly | Mechanical Engineering; Lighting; Heating | 36 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.