loadpatents
Patent applications and USPTO patent grants for Drela; Mark.The latest application filed is for "system and method for reducing the noise of pusher type aircraft propellers".
Patent | Date |
---|---|
System and method for reducing the noise of pusher type aircraft propellers Grant 8,622,334 - Drela , et al. January 7, 2 | 2014-01-07 |
System And Method For Reducing The Noise Of Pusher Type Aircraft Propellers App 20120292441 - Drela; Mark ;   et al. | 2012-11-22 |
System and method for controlling engine RPM of a ducted fan aircraft Grant 7,364,115 - Parks , et al. April 29, 2 | 2008-04-29 |
System and method for controlling engine RPM of a ducted fan aircraft App 20060097107 - Parks; Robert ;   et al. | 2006-05-11 |
Flyer assembly Grant 6,576,880 - Martorana , et al. June 10, 2 | 2003-06-10 |
Flyer Assembly App 20030089820 - Martorana, Richard T. ;   et al. | 2003-05-15 |
Flyer assembly Grant 6,392,213 - Martorana , et al. May 21, 2 | 2002-05-21 |
High-G compact folding wing Grant 6,260,798 - Casiez , et al. July 17, 2 | 2001-07-17 |
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.