Abstract: Internal combustion engines, both compression ignition (CI) and spark ignition (SI), four cycle and turbocharged, are defined with the proposed patented modifications to improve environmental acceptability. Thermal efficiency has been more than doubled at the maximum power design point. The CI engine 75.8 percent and the SI engine 72.7 percent. The particulates (smoke), nitrus oxide, and carbon monoxide have been reduced to a trace for both engine types. With the improved thermal efficiency the carbon dioxide produced per horsepower is less than half of the current designs. Exhaust noise and obnoxious smell has been eliminated for both engine types. These predicted improvements are based on the use of existing fuels. A byproduct of the design will be the recovery of the distilled water resulting from the products of combustion. A fuel tank is defined which collects the condensed water and varies the fuel storage volume to that required for the remaining fuel.

Abstract: A propulsion/control system for aircraft of the vertical takeoff and landing type having a body without wings or tail and relying entirely on fluid streams for effecting liftoff, propulsion, and control. The body has an air duct with an inlet adjacent the rear end and a downwardly directed outlet at each side, an engine driven fan being disposed in the duct at the inlet and a cascade of adjustable vanes at each outlet. Operation of the fan causes air to flow into the inlet, through the duct, and issue in streams from the outlets, the reaction of such streams imparting lifting and flight forces to the body. By adjusting the cascades of vanes, the effects of the forces can be varied to control the movement of the body. To further control the movement and stability of the body in the air, additional adjustable elements may be provided.