SUPERSONIC RAMJET COMBUSTOR BASED ENGINES

Brand Owner (click to sort) Address Description
RAMGEN RAMGEN POWER SYSTEMS, INC. 11808 Northup Way Suite W-190 Bellevue WA 98005 Supersonic ramjet combustor based engines for mechanical power generation or electrical power generation;
RAMGEN RAMGEN POWER SYSTEMS Suite W-190 11808 Northup Way Bellevue WA 98005 Supersonic ramjet combustor based engines for mechanical power generation or electrical power generation;
RAMGEN 11808, INC. 11808 NORTHUP WAY, SUITE W-180 BELLEVUE WA 98005 Supersonic ramjet combustor based engines for mechanical power generation or electrical power generation;
RAMGEN RAMGEN POWER SYSTEMS, INC. 11808 Northup Way Suite W-190 Bellevue WA 98005 Supersonic ramjet combustor based engines for mechanical power generation or electrical power generation;
RAMGEN POWER SYSTEMS RAMGEN POWER SYSTEMS, INC. 11808 Northup Way Suite W-190 Bellevue WA 98005 Supersonic ramjet combustor based engines for mechanical power generation or electrical power generation;POWER SYSTEM;The drawing is lined for the colors red and blue.;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. A ramjet powered device that utilizes a novel swirl generator for rapidly and efficiently atomizing, vaporizing, as necessary, and mixing a fuel into an oxidant. The swirl generator converts an oxidant flow into a turbulent, three-dimensional flowfield into which the fuel is introduced. The swirl generator effects a toroidal outer recirculation zone and an inner central recirculation zone, both of which are configured in a backward-flowing manner that carries heat and combustion byproducts upstream where they are employed to continuously ignite a combustible fuel/oxidizer mixture in adjacent shear layers and stabilizes flame propagation and accelerates combustion throughout the entire combustor. The swirl generator provides smooth combustion with no instabilities and minimum total pressure losses and enables significant reductions in the L/D ratio of the combustor. Other benefits include simplicity, reliability, wide flammability limits and high combustion efficiency and thrust performance.