公开(公告)号：US20240133389A1

公开(公告)日：2024-04-25

申请号：US17769961

申请日：2021-08-26

Applicant: Foshan Shenfeng Aviation Technology Co., Ltd.

Inventor： Zhicheng WANG

IPC: F04D25/00 ,  A63B21/008 ,  B63G8/08 ,  B64C27/32 ,  F04D13/00

CPC classification number: F04D25/00 ,  A63B21/0084 ,  B63G8/08 ,  B64C27/32 ,  F04D13/00

Abstract: The present disclosure discloses a device and a method for converting reciprocating motion into continuous rotation, and application includes: a central shaft and rotating discs, each rotating disc is connected to the central shaft through a bearing, the rotating disc is arranged concentrically with the bearing, wings are arranged on a circumference of rotating disc, upper wing surfaces of the wings are of convex structures. According to the device for converting reciprocating motion into continuous rotation of the present disclosure, the rotating directions of the wings can be kept unchanged all the time during the reciprocating motion of the device by using airfoil structures of the wings in the device and limiting mounting angles of the wings, so as to obtain a continuous lifting force with a constant direction.

公开(公告)号：US20240229808A9

公开(公告)日：2024-07-11

申请号：US17769961

申请日：2021-08-27

Applicant: Foshan Shenfeng Aviation Technology Co., Ltd.

Inventor： Zhicheng WANG

IPC: F04D25/00 ,  A63B21/008 ,  B63G8/08 ,  B64C27/32 ,  F04D13/00

CPC classification number: F04D25/00 ,  A63B21/0084 ,  B63G8/08 ,  B64C27/32 ,  F04D13/00

Abstract: The present disclosure discloses a device and a method for converting reciprocating motion into continuous rotation, and application includes: a central shaft and rotating discs, each rotating disc is connected to the central shaft through a bearing, the rotating disc is arranged concentrically with the bearing, wings are arranged on a circumference of rotating disc, upper wing surfaces of the wings are of convex structures. According to the device for converting reciprocating motion into continuous rotation of the present disclosure, the rotating directions of the wings can be kept unchanged all the time during the reciprocating motion of the device by using airfoil structures of the wings in the device and limiting mounting angles of the wings, so as to obtain a continuous lifting force with a constant direction.