RU2011142930A

RU2011142930A - ROTARY-TURBINE INTERNAL COMBUSTION ENGINE

Info

Publication number: RU2011142930A
Application number: RU2011142930/06A
Authority: RU
Inventors: Евгений Алексеевич Несмеев
Original assignee: Евгений Алексеевич Несмеев
Priority date: 2011-10-24
Filing date: 2011-10-24
Publication date: 2013-04-27

Abstract

Роторно-турбинный двигатель внутреннего сгорания, содержащий корпус и находящийся в нем с зазором роторы сжатия и малый ротор, кинематически связаны между собой шестернями, находящимися в собственном корпусе и жестко закрепленными на оси вращения соответствующего ротора, при этом ротор сжатия представляет собой объединенные вместе цилиндры, системы подачи воздуха в камеру сгорания, впрыска топлива, воспламенения топливной смеси, отвода выхлопных газов, а также систему охлаждения корпуса и роторов, отличающийся тем, что крайние торцы лопастей ротора сжатия обработаны под кривизну области его вращения с учетом необходимого зазора, а малый ротор представляет собой цилиндр с полостями, имеющими несколько радиусов обработки, включающие обработку под радиус обработки лопасти ротора сжатия и радиус, обеспечивающий минимизацию зазора при прохождении выступов, образованных областями вращения малого ротора и ротора сжатия, помимо этого, конструкция двигателя включает в себя компрессор, роторы которого находятся на одних валах с роторами двигателя.A rotary-turbine internal combustion engine containing a housing and a compression rotors and a small rotor located in it with a gap, are kinematically interconnected by gears located in their own housing and rigidly fixed on the axis of rotation of the corresponding rotor, while the compression rotor is cylinders combined together, systems for supplying air to the combustion chamber, fuel injection, ignition of the fuel mixture, exhaust gas removal, as well as a cooling system for the housing and rotors, characterized in that the extreme ends of the compression rotor blades are processed for the curvature of the area of its rotation, taking into account the required clearance, and the small rotor is is a cylinder with cavities having several processing radii, including processing for the processing radius of the compression rotor blade and the radius that minimizes the clearance when passing the protrusions formed by the areas of rotation of the small rotor and the compression rotor, in addition, the engine design includes a compressor, rotors which are located on the same shafts with the engine rotors.

Claims

A rotary-turbine internal combustion engine, comprising a housing and a compression rotor and a small rotor located in it with a gap, are kinematically connected to each other by gears located in their own housing and rigidly fixed to the axis of rotation of the corresponding rotor, while the compression rotor is a joint cylinder systems for supplying air to the combustion chamber, fuel injection, ignition of the fuel mixture, exhaust gas exhaust, as well as the cooling system of the housing and rotors, characterized in that the extreme ends of the mouths of the compression rotor are processed according to the curvature of the region of its rotation, taking into account the necessary clearance, and the small rotor is a cylinder with cavities having several machining radii, including processing under the radius of processing of the compression rotor blade and a radius that minimizes the gap when passing protrusions formed by small rotation regions rotor and compression rotor, in addition, the engine design includes a compressor, the rotors of which are located on the same shafts with the rotors of the engine.