AN IMPROVED DRONE STRUCTURE
First Claim
Patent Images
1. A structure of drone (100) comprising:
- a frame (110) comprising an engagement portion (110′
), said engagement portion (110′
) being a strip having a predetermined geometry;
a plurality of propulsion elements (120);
characterized in that each propulsion element (120) is arranged, in use, to be engaged in a removable way to said engagement portion (110′
) at any point of said strip, in such a way to easily change the number and the arrangement of said propulsion elements (120) present on said engagement portion (110′
).
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Accused Products
Abstract
A structure of drone (100) comprises a frame (110) comprising an engagement portion (110′), said engagement portion (110′) being a strip having a predetermined geometry. The structure of drone (100) also comprises a plurality of propulsion elements (120). Each propulsion element (120) is arranged, in use, to be engaged in a removable way to the engagement portion (110′) at a any point of the strip, in such a way to easily change the number and the arrangement of the propulsion elements (120) present on the engagement portion (110′).
27 Citations
12 Claims
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1. A structure of drone (100) comprising:
-
a frame (110) comprising an engagement portion (110′
), said engagement portion (110′
) being a strip having a predetermined geometry;a plurality of propulsion elements (120); characterized in that each propulsion element (120) is arranged, in use, to be engaged in a removable way to said engagement portion (110′
) at any point of said strip, in such a way to easily change the number and the arrangement of said propulsion elements (120) present on said engagement portion (110′
). - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A structure of drone (100) comprising:
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a frame (110) comprising an engagement portion (110′
), said engagement portion (110′
) being a strip having a predetermined geometry and being equipped with a plurality of engagement positions;a plurality of propulsion elements (120); characterized in that each propulsion element (120) of said plurality is adapted to be engaged to said engagement portion (110′
) at any of said engagement positions, in order to obtain a predetermined propulsion configuration among a plurality of possible obtainable propulsion configurations.
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Specification