公开(公告)号：US20090272094A1

公开(公告)日：2009-11-05

申请号：US12498794

申请日：2009-07-07

Applicant: Alexander M. Zink ,  Alexander S. Zink ,  Michael M. Zink

Inventor： Alexander M. Zink ,  Alexander S. Zink ,  Michael M. Zink

IPC: F02C3/14

CPC classification number: F01C1/46 ,  F01C11/006 ,  F02C3/16

Abstract: A tangential combustion turbine is disclosed which is based on a casing, a rotor, and moving levers. A radial compressor is attached to the rotor and creates air pressure which pushes air into the combustion chamber based on the position and design of the combustion lever. The combustion chamber is defined by spaces between rotor lobes, and by combustion levers and exhaust levers which follow the rotor surface. A premix fuel system or direct fuel injection is used to create combustion. The exhaust gases then pass through the exhaust lever into the exhaust piping as the rotor rotates.

Abstract translation: 公开了一种基于壳体，转子和移动杆的切向燃烧涡轮机。 径向压缩机附接到转子并产生空气压力，其基于燃烧杆的位置和设计将空气推入燃烧室。 燃烧室由转子叶片之间的空间以及跟随转子表面的燃烧杆和排气杆构成。 使用预混燃料系统或直接燃料喷射来产生燃烧。 随着转子旋转，废气然后通过排气杆进入排气管道。

公开(公告)号：US09920688B2

公开(公告)日：2018-03-20

申请号：US15100458

申请日：2014-12-05

Applicant: Alexander M. Zink

Inventor： Alexander M. Zink

IPC: F02B55/14 ,  F02B53/12 ,  F02B53/10 ,  F02B53/04 ,  F02B53/02 ,  F16J9/12 ,  F02B53/00 ,  F01C1/46 ,  F01C20/14

CPC classification number: F02B55/14 ,  F01C1/46 ,  F01C20/14 ,  F02B53/00 ,  F02B53/02 ,  F02B53/04 ,  F02B53/10 ,  F02B53/12 ,  F16J9/12 ,  Y02T10/17

Abstract: Combustion engine having a rotor, a housing and at least two combustion chambers which are formed between the rotor and the housing, wherein the housing has at least one ignition recess on the side thereof which faces the rotor, into which ignition recess a fuel feed and ignition system opens. At least one valve device which is mounted rotatably in the housing is configured for dividing the combustion chambers at least temporarily into an ignition chamber and a compression chamber. The valve device has at least one rotor passage section, at least one closing section and at least one gas passage section. Alternatively, the valve device temporarily at the same time disconnects a compression chamber from a first combustion chamber and an ignition chamber from a second combustion chamber, wherein there is a fluidic connection during this time between the ignition chamber and the compression chamber.

公开(公告)号：US08061327B2

公开(公告)日：2011-11-22

申请号：US12498794

申请日：2009-07-07

Applicant: Alexander M. Zink ,  Alexander S. Zink ,  Michael M. Zink

Inventor： Alexander M. Zink ,  Alexander S. Zink ,  Michael M. Zink

IPC: F02B53/00

CPC classification number: F01C1/46 ,  F01C11/006 ,  F02C3/16

Abstract: A tangential combustion turbine is disclosed which is based on a casing, a rotor, and moving levers. A radial compressor is attached to the rotor and creates air pressure which pushes air into the combustion chamber based on the position and design of the combustion lever. The combustion chamber is defined by spaces between rotor lobes, and by combustion levers and exhaust levers which follow the rotor surface. A premix fuel system or direct fuel injection is used to create combustion. The exhaust gases then pass through the exhaust lever into the exhaust piping as the rotor rotates.

Abstract translation: 公开了一种基于壳体，转子和移动杆的切向燃烧涡轮机。 径向压缩机附接到转子并产生空气压力，其基于燃烧杆的位置和设计将空气推入燃烧室。 燃烧室由转子叶片之间的空间以及跟随转子表面的燃烧杆和排气杆构成。 使用预混燃料系统或直接燃料喷射来产生燃烧。 随着转子旋转，废气然后通过排气杆进入排气管道。