Patent · US Active

Unmanned aerial vehicle structures and methods

US10017237B2 · kind B2 · utility

6Cited by
2References
26Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 3, 2016
Grant dateJul 10, 2018
Priority date
Expiry dateDec 1, 2036

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16F15/04
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Embodiments described herein relates to an Unmanned Aerial Vehicle (UAV) having vibration dampening and isolation capabilities, the UAV including a first frame portion, a second frame portion, and a third frame portion. Each of the first frame portion, the second frame portion, and the third frame portion is separated from one another. At least one first support member inelastically coupling the first frame portion and the third frame portion. At least one second support member elastically coupling the second frame portion and one or more of the first frame portion or the third frame portion to isolate the first frame portion and the third frame portion from vibration of the second frame portion.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.