Mark Eugene Noe
33Patents
18h-index
55Co-inventors
84Inventor score
Filing activity: Jul 13, 1990 → Jun 27, 2019
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6325593A | Ceramic turbine airfoils with cooled trailing edge blocks | Emerging Cross-Sectional Technologies | 103 | Expired |
| US6884026B2 | Turbine engine shroud assembly including axially floating shroud segment | Mechanical Engineering; Lighting; Heating | 96 | Expired |
| US6733235B2 | Shroud segment and assembly for a turbine engine | Emerging Cross-Sectional Technologies | 83 | Expired |
| US6893214B2 | Shroud segment and assembly with surface recessed seal bridging adjacent members | Mechanical Engineering; Lighting; Heating | 72 | Expired |
| US6895757B2 | Sealing assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor | Mechanical Engineering; Lighting; Heating | 69 | Expired |
| US6904757B2 | Mounting assembly for the forward end of a ceramic matrix composite liner in a gas turbine engine combustor | Mechanical Engineering; Lighting; Heating | 52 | Expired |
| US6895761B2 | Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor | Mechanical Engineering; Lighting; Heating | 50 | Expired |
| US6821085B2 | Turbine engine axially sealing assembly including an axially floating shroud, and assembly method | Mechanical Engineering; Lighting; Heating | 48 | Expired |
| US6554563B2 | Tangential flow baffle | Emerging Cross-Sectional Technologies | 48 | Expired |
| US6808363B2 | Shroud segment and assembly with circumferential seal at a planar segment surface | Mechanical Engineering; Lighting; Heating | 37 | Expired |
| US8943835B2 | Gas turbine engine combustor with CMC heat shield and methods therefor | Emerging Cross-Sectional Technologies | 37 | Active |
| US5281084A | Curved film cooling holes for gas turbine engine vanes | Mechanical Engineering; Lighting; Heating | 28 | Expired |
| US6920762B2 | Mounting assembly for igniter in a gas turbine engine combustor having a ceramic matrix composite liner | Mechanical Engineering; Lighting; Heating | 27 | Expired |
| US7052234B2 | Turbine vane collar seal | Emerging Cross-Sectional Technologies | 24 | Expired |
| US6775985B2 | Support assembly for a gas turbine engine combustor | Mechanical Engineering; Lighting; Heating | 22 | Expired |
| US6398501B1 | Apparatus for reducing thermal stress in turbine airfoils | Mechanical Engineering; Lighting; Heating | 20 | Expired |
| US9410437B2 | Airfoil components containing ceramic-based materials and processes therefor | Emerging Cross-Sectional Technologies | 19 | Active |
| US6261054A | Coolable airfoil assembly | Emerging Cross-Sectional Technologies | 19 | Expired |
| US8206096B2 | Composite turbine nozzle | Emerging Cross-Sectional Technologies | 16 | Active |
| US10774008B2 | Ceramic matrix composite articles | Emerging Cross-Sectional Technologies | 16 | Active |
| US10017425B2 | Methods and materials for forming in-situ cavities for silicon-based ceramic matrix composite components | Emerging Cross-Sectional Technologies | 15 | Active |
| US10393381B2 | Unitary flow path structure | Emerging Cross-Sectional Technologies | 12 | Active |
| US10378770B2 | Unitary flow path structure | Emerging Cross-Sectional Technologies | 12 | Active |
| US10371383B2 | Unitary flow path structure | Emerging Cross-Sectional Technologies | 12 | Active |
| US8714932B2 | Ceramic matrix composite blade having integral platform structures and methods of fabrication | Emerging Cross-Sectional Technologies | 11 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.