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Indianapolis, IN, United States of America

Von David Baker

USPTO Granted Patents = 11

Average Co-Inventor Count = 1.6

ph-index = 6

Forward Citations = 244(Granted Patents)

Company Filing History:

Allison Advanced Development Company

Rolls-royce Corporation

Rolls-royce North American Technologies Inc.

4. 1 out of 832,880

Other

patents

Years Active: 2001-2019

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11 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 10443539 - Hybrid exhaust nozzle (2019-10-15),

2. 10371093 - Aircraft nozzle with a variable nozzle area of a second flow path (2019-08-06),

3. 9896191 - Fluid-vectoring system (2018-02-20),

4. 8769959 - Nozzle with an adjustable throat (2014-07-08),

5. 8459036 - Aircraft nozzle having actuators capable of changing a flow area of the aircraft nozzle (2013-06-11),

6. 7793504 - Nozzle with an adjustable throat (2010-09-14),

7. 6668542 - Pulse detonation bypass engine propulsion pod (2003-12-30),

8. 6606854 - Exhaust mixer and apparatus using same (2003-08-19),

9. 6584764 - Propulsion module (2003-07-01),

10. 6382559 - Thrust vectoring mechanism (2002-05-07),

11. 6318668 - Thrust vectoring techniques (2001-11-20),

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