MX2015007616A - Improvements in the unidirectional propulsion of a nozzle. - Google Patents

Abstract

The invention refers to improvement in a conventional nozzle, which is characterized in that it produces a driving motion and a perpendicular lifting motion in each one of the two equal portions into which it is divided, so that when it is applied to a rocket the ejection position is changed from vertical to horizontal. The invention refers to improvements in the conventional wings, these wings being changed by rectangular nozzles, through which the gas flow is performed in a horizontal manner, the forward resistance being reduced, improving the fuel saving and the aircraft speed, making possible the construction of supersonic, practical, affordable aircrafts with a reduced landing and taking-off tracks. The invention also refers to improvement in the conventional blades of a helicopter rotor, which are changed by rectangular nozzles, where the gas flow is performed in a horizontal manner instead of downwards, being able to be operated in an open or close cycle without expelling gases to the exterior. The invention refers to improvements in the straight wings, these being changed by circular nozzles having an inlet in the center or peripheral area thereof, also being characterized in that they are symmetric and lack of driving force. The invention refers to improvements in the hovercrafts, where the semi nozzles, rectangular or circular nozzles provide lift and forward motion. The invention refers to improvements in the conventional nozzle, which is characterized in that the gaseous or liquid flow, upon flowing through the semi nozzle, or rectangular or circular nozzles, produces the lift and the forward motion, and may be part of the turboprop engines, hydraulic and wind generators.