Abstract An Airplane model design without a vertical stabilizer comprising, a fuselage, twisted wings and horizontal stabilizer, wherein, said fuselage is connected with the twisted wings and the horizontal stabilizer; said horizontal stabilizer having an elevator, and a power system for thrust and controlling; characterized in that, the twisted wings made up of airfoil that is twisted in a negative angle wherein twist increases towards the extreme end of the wing, away from the fuselage so as to provide balancing of the adverse yaw. Application No: Applicant Name: (1) Abhishek S. Pawar (2) Atharva Mahajan (3) Vrushal Modake (4) Ashish Dharme Total No of Sheets: 05 Page 4 of 5 Figure 4 Sectional View of the wing of the airplane without vertical tail assembly (1) Abhishek S. Pawar (2) Atharva Mahajan (3) Vrushal Modake (4) Ashish Dharme Applicant Applicant Applicant Applicant
AN AIRPLANE DESIGN STUCTURE WITHOUT VERTICAL STABILIZER
2021-04-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Airplane vertical tail stabilizer composite leading edge structure
European Patent Office | 2023
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