Rotary-Wing Aircraft
First Claim
1. Rotary-wing aircraft (100), comprising at least four rotors (110), which are disposed on girder elements (120a, 120b),wherein said rotors (110) and girder elements (120a, 120b) are disposed such that a free field of vision (S) is defined along a longitudinal axis (L) of said rotary-wing aircraft (100) at least between two terminal rotors.
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Accused Products
Abstract
The invention relates to a rotary-wing aircraft (100), comprising at least four rotors (110), which are disposed on girder elements (120a, 120b), wherein said rotors (110) and girder elements (120a, 120b) are disposed such that a free field of vision (S) is defined along a longitudinal axis (L) of said rotary-wing aircraft (100) at least between two terminal rotors.
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Citations
10 Claims
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1. Rotary-wing aircraft (100), comprising at least four rotors (110), which are disposed on girder elements (120a, 120b),
wherein said rotors (110) and girder elements (120a, 120b) are disposed such that a free field of vision (S) is defined along a longitudinal axis (L) of said rotary-wing aircraft (100) at least between two terminal rotors.
Specification