VECTORED-THRUST PROPULSOR

A jet propulsor, for use in vehicles or other devices moving in a three-dimensional gaseous or liquid medium such as air or water, has a joint chamber and at least four flow passages which are connected to the chamber with one of their ends, have independently controllable reversible pressure units...

Full description

Saved in:
Bibliographic Details
Main Author IVANOV VLADIMIR E
Format Patent
LanguageEnglish
Published 14.08.2014
Subjects
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
Online AccessGet full text

Cover

More Information
Summary:A jet propulsor, for use in vehicles or other devices moving in a three-dimensional gaseous or liquid medium such as air or water, has a joint chamber and at least four flow passages which are connected to the chamber with one of their ends, have independently controllable reversible pressure units inside, and are provided with independently controllable nozzles on their other ends. The propulsor pumps gas or liquid from the environment through itself and, because of reaction forces, provides for simultaneously and independently controlled thrust and thrust moment in terms of their value/strength and direction. Spatial control of the thrust vectoring and conditional thrust moment vector can be provided for in the spatial range of a full solid angle.
Bibliography:Application Number: US201114234073