Issued Patents All Time
Showing 1–2 of 2 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 4523603 | Air intake control for an adjustable air inlet, particularly two-dimensional oblique shock diffuser for gas turbine jet engines for the propulsion of high performance aircraft | — | 1985-06-18 |
| 4467600 | System for controlling the thrust nozzle adjustment of dual cycle gas turbine jet propulsion engines | — | 1984-08-28 |