Patent · US Active

Structure of an electric aircraft including a boom joint with an airfoil-shaped hole, and method of manufacturing the same

US12037125B1 · kind B1 · utility

0Cited by
9References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 13, 2023
Grant dateJul 16, 2024
Priority date
Expiry dateJan 13, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64U20/00
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A structure of an electric aircraft is disclosed. The structure may include a wing, wherein the wing is a single component that runs from a left side of the electric aircraft to a right side of the electric aircraft. The wing may include an airfoil. The structure may include at least a boom, wherein the at least a boom is configured to carry at least a propulsor. The at least a boom may include a boom joint attached to the wing. The at least a boom may further include at least a first boom segment attached to a first end of the boom joint. The at least a boom may further include at least a second boom segment attached to a second end of the boom joint.

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