| Patent Number |
Title Of Patent |
Date Issued |
| 8127533 |
System and method for power production using a hybrid helical detonation device |
March 6, 2012 |
| The system and method described herein uses a hybrid pulsed detonation engine (PDE) system to drive a turbine that powers an electric generator. The combustion chamber of the PDE is shaped in a helical form, so that the external length of the section is reduced, while maintaining the |
| 7958732 |
Internal detonation reciprocating engine |
June 14, 2011 |
| A method of rotating a crank shaft and in internal detonation engine are provided. The internal detonation engine comprises a deflagration to detonation transition section. The deflagration to detonation transition section is connected to a main cylinder, which houses a piston. Inducing |
| 7907038 |
Electromagnetic flow control, methods and uses |
March 15, 2011 |
| Actuation for control of surfaces is provided through use of a conducting material comprising electrolyte particles electrically charged with electromagnetic fields in boundary layers. Interactions of the electrically charged particles with electromagnetic fields in boundary layers a |
| 7340903 |
Scalable power generation using a pulsed detonation engine |
March 11, 2008 |
| A scalable power generator is described. A scalable, portable pulsed detonation engine is coupled to a turbine which drives a generator and using commonly available fuels, electric energy is provided. Additional embodiments incorporate a mechanical compressor at the intake of the pul |
| 6857261 |
Multi-mode pulsed detonation propulsion system |
February 22, 2005 |
| A multi-mode propulsion system for potential application to hypersonic and aerospace planes. The system can employ various propulsion modes at various points in time, with the propulsion system employed at a given point in time being selected according to the velocity of the inlet ai |
