RU2012109607A

RU2012109607A - METHOD FOR CREATING MOTION POWER FOR MOVING A VEHICLE AND TURBOREACTIVE ENGINE FOR ITS IMPLEMENTATION

Info

Publication number: RU2012109607A
Application number: RU2012109607/11A
Authority: RU
Inventors: Юрий Васильевич Дробышевский; Сергей Николаевич Столбов
Original assignee: Юрий Васильевич Дробышевский; Сергей Николаевич Столбов
Priority date: 2012-03-14
Filing date: 2012-03-14
Publication date: 2013-09-20

Abstract

1. Способ создания движущей силы для перемещения транспортного аппарата, включающий ввод воздуха и создание азимутально и аксиально движущегося его потока, создание струи со скоростью более чем вдвое большей, азимутальной скорости потока, эжекцию в струю дополнительного объема воздуха, нагрев потока, формирование им вращающего момента вала, отличающийся тем, что до нагрева, часть воздуха отводят от оси вала азимутально и радиально, горячий поток выводят азимутально и аксиально, передают импульс и момент вращения потока дополнительно подведенному радиально от оси воздуху и затем формируют вращающий момент вала и тянущее усилие двигателя.2. Реактивный двигатель, включающий компрессор и турбину выполненные на общем валу и содержащие винты со структурой профилей с крыловыми элементами, камеру сгорания, выполненную азимутальной, венцы с лопатками, размещенные перед и за камерой сгорания, отличающийся тем, что лопатки входного венца камеры сгорания выполнены продольными перед турбиной, за камерой сгорания размещена камера эжекторного смешения потоков, винт компрессора и турбины выполнен заедино в виде продольных плоскостей, содержащих участки центробежные и участки со структурой профилей с крыловыми элементами.3. Реактивный двигатель по п.2. отличающийся тем, что он имеет дополнительный винт, который размещен на общем валу за турбиной, крыловые элементы структуры профилей на кромке лопасти винта ориентированы радиально так, что задняя кромка каждого профиля изогнута по движению потока.1. A method of creating a driving force for moving a transport apparatus, including introducing air and creating an azimuthally and axially moving flow thereof, creating a jet with a velocity of more than twice the azimuthal flow velocity, ejecting an additional volume of air into the jet, heating the flow, generating torque shaft, characterized in that before heating, part of the air is removed from the shaft axis azimuthally and radially, the hot stream is removed azimuthally and axially, an impulse and the moment of rotation of the stream are transmitted additionally under introduced radially from the axis of the air and then form the torque of the shaft and the pulling force of the engine. 2. A jet engine including a compressor and a turbine made on a common shaft and containing screws with a structure of profiles with wing elements, a combustion chamber made of azimuth, crowns with blades placed in front of and behind the combustion chamber, characterized in that the blades of the inlet crown of the combustion chamber are made longitudinal before a turbine, an ejector mixing chamber is located behind the combustion chamber, the screw of the compressor and turbine are made integrally in the form of longitudinal planes containing centrifugal sections and sections with a structure round profiles with wing elements. 3. The jet engine according to claim 2. characterized in that it has an additional screw, which is located on a common shaft behind the turbine, the wing elements of the profile structure on the edge of the rotor blades are oriented radially so that the trailing edge of each profile is curved by the flow.

Claims

1. A method of creating a driving force for moving a transport apparatus, including introducing air and creating an azimuthally and axially moving flow thereof, creating a jet with a velocity of more than twice the azimuthal flow velocity, ejecting an additional volume of air into the jet, heating the flow, generating torque shaft, characterized in that before heating, part of the air is removed from the shaft axis azimuthally and radially, the hot stream is removed azimuthally and axially, an impulse and the moment of rotation of the stream are transmitted additionally under conducted radially from the axis of the air and then form the torque of the shaft and the pulling force of the engine.

2. A jet engine comprising a compressor and a turbine made on a common shaft and containing screws with a profile structure with wing elements, a combustion chamber made of azimuth, crowns with blades placed in front of and behind the combustion chamber, characterized in that the blades of the inlet crown of the combustion chamber are made longitudinal in front of the turbine, behind the combustion chamber there is an ejector mixing chamber, the screw of the compressor and turbine is made integrally in the form of longitudinal planes containing centrifugal sections and sections with Keturah profiles Krylov elements.

3. The jet engine according to claim 2. characterized in that it has an additional screw, which is located on a common shaft behind the turbine, the wing elements of the profile structure on the edge of the rotor blades are oriented radially so that the trailing edge of each profile is curved by the flow.