Title:
AN AEROPLANE MULTIPURPOSE WING STABILITY SYSTEM
Document Type and Number:
WIPO Patent Application WO/2016/132302
Kind Code:
A3
Abstract:
Exemplary embodiment of the present disclosure is directed towards an aeroplane multipurpose wing stability system. The system includes a wing shell connected to a fuselage of the aeroplane configured with a wing socket for providing flexible movements to the wings of the aeroplane, whereby the wings coupled to the fuselage of the aeroplane depend on center of gravity. The system further includes a yaw line socket internally incorporated on top side and lower side of the wing shell with a yaw line axis configured to allow free rotation in both sides of the yaw line socket, whereby the rotation of the yaw line socket supported by a plurality of bearings and an actuator connected at an inside of the yaw line socket. The system also includes a saw wheel coupled to the actuator by a wheel connector configured to provide rotations to the aeroplane wings in required directions by keeping the fuselage of the aeroplane in stable and a wing roll wheel coupled to a elevated pitch axis line configured to maintain sustainable of heavy pressure and weight of the aeroplane wings and the wing roll wheel freely hanged in longitudinal direction in a provided space in the wing shell at certain height.
Inventors:
BHUKYA ASHOK KUMAR (IN)
Application Number:
PCT/IB2016/050849
Publication Date:
October 27, 2016
Filing Date:
February 17, 2016
Export Citation:
Assignee:
BHUKYA ASHOK KUMAR (IN)
International Classes:
B64C39/00; B64C3/38; B64C3/40
Foreign References:
| US4998689A | 1991-03-12 | |||
| US3064928A | 1962-11-20 | |||
| US2668026A | 1954-02-02 | |||
| US2822995A | 1958-02-11 |
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