Tindell; Runyon H.
Patent Applications and Registrations
Patent applications and USPTO patent grants for Tindell; Runyon H..The latest application filed is for "thin inlet lip design for low drag and reduced nacelle size".
- Tindell; Runyon H. - Old Bethpage NY
| Patent | Date |
|---|---|
| Thin inlet lip design for low drag and reduced nacelle size Grant 6,179,251 - Tindell , et al. January 30, 2 | 2001-01-30 |
| Low drag inlet design using injected duct flow Grant 5,934,611 - Tindell , et al. August 10, 1 | 1999-08-10 |
| Blockerless thrust reverser Grant 5,904,320 - Tindell May 18, 1 | 1999-05-18 |
| Blockerless thrust reverser Grant 5,713,537 - Tindell February 3, 1 | 1998-02-03 |
| Blown boundary layer control system for a jet aircraft Grant 5,447,283 - Tindell September 5, 1 | 1995-09-05 |
| Flight control augmentation inlet device Grant 4,979,699 - Tindell December 25, 1 | 1990-12-25 |
uspto.report is an independent third-party trademark research tool that is not affiliated, endorsed, or sponsored by the United States Patent and Trademark Office (USPTO) or any other governmental organization. The information provided by uspto.report is based on publicly available data at the time of writing and is intended for informational purposes only.
While we strive to provide accurate and up-to-date information, we do not guarantee the accuracy, completeness, reliability, or suitability of the information displayed on this site. The use of this site is at your own risk. Any reliance you place on such information is therefore strictly at your own risk.
All official trademark data, including owner information, should be verified by visiting the official USPTO website at www.uspto.gov. This site is not intended to replace professional legal advice and should not be used as a substitute for consulting with a legal professional who is knowledgeable about trademark law.
| 