公开(公告)号：US20050247282A1

公开(公告)日：2005-11-10

申请号：US10514147

申请日：2003-05-15

Applicant: Galip Yuksel

Inventor： Galip Yuksel

IPC: F01L7/02 ,  F01C1/073 ,  F01C11/00 ,  F02B53/00 ,  F02B53/04 ,  F02B53/10

CPC classification number: F01C1/073 ,  F01C11/002 ,  F02B53/00

Abstract: The aim of the invention is to dispense with the disadvantages of previous engines either fully or partially. This is achieved by means of two cylindrical parts (1,3,5) which rotate into each other, respectively possessing a wing (2,4) and which can rotate about an axis at different speeds. Similar to a four-stroke engine, the following occurs: induction of an air-fuel mixture, compression until self-ignition, creation of a working stroke and discharge of combustion gases. The variable inlet and outlet opening times are controlled according to a control bushing (12) and a special stepper motor (62). The rotating wings are controlled by freewheeling and by unilaterally acting hydrodynamic brakes or secured against reversed rotation. In relation to the cylinder core (13), two functional variable work chambers arise for each disk discharge elements which were not possible with the previously rigid engine structure. As a result new technical options are provided, especially regarding the use of novel (ceramic) materials. The engine can be used as a drive engine or, when modified, as a steam engine, compressor or pump.

Abstract translation: 本发明的目的是完全或部分地省去以前的发动机的缺点。 这通过两个相互旋转的圆柱形部件（1,3,5）实现，它们分别具有翼（2,4）并且可以以不同的速度围绕轴线旋转。 类似于四冲程发动机，发生以下情况：感应空气 - 燃料混合物，压缩直到自点火，产生工作冲程和排放燃烧气体。 根据控制衬套（12）和特殊的步进电机（62）来控制可变的入口和出口打开时间。 旋转翼由空转和单向作用的流体动力制动器控制或抵抗反向旋转。 相对于气缸芯（13），对于每个盘排出元件出现两个功能可变的工作室，这对于先前刚性的发动机结构是不可能的。 因此，提供了新的技术选择，特别是关于使用新型（陶瓷）材料。 发动机可用作驱动发动机，或者在修改时可用作蒸汽机，压缩机或泵。