USD813143SActiveUtility

Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors

Assignee: AEROVIRONMENT INCPriority: Nov 4, 2016Filed: Nov 4, 2016Granted: Mar 20, 2018
Est. expiryNov 4, 2036(~10.3 yrs left)· nominal 20-yr term from priority
93
PatentIndex Score
56
Cited by
44
References
1
Claims

Claims

exact text as granted — not AI-modified
CLAIM 
     
       The ornamental design for a vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors, as shown and described.

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