Patent · US Active

Parallel hybrid propulsion system

US11685537B1 · kind B1 · utility

0Cited by
1References
9Claims
0Family size

Assignee

Inventor

Key dates

Filing dateAug 19, 2022
Grant dateJun 27, 2023
Priority date
Expiry dateAug 19, 2042

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D27/026
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Systems and methods for controlling flight via a parallel hybrid aircraft having an electric propulsion system and a combustion propulsion system are disclosed. Exemplary implementations may include: a combustion propulsion system including a combustion engine; an electric propulsion system including a motor and an electric power source, wherein the motor comprises a stator, a rotor coupled to the engine shaft, and support bearings between the rotor and the stator; a mechanical link coupled to the stator and the combustion engine, wherein the mechanical link substantially prevents movement of the stator in a rotational degree of freedom; and a propeller coupled to the engine shaft, wherein the rotor is coupled to the engine shaft between the propeller and the combustion engine.

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