The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 11, 2025

Filed:

Sep. 29, 2023
Applicant:

Korea Aerospace Research Institute, Daejeon, KR;

Inventor:

Keun Bae Kim, Daejeon, KR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 31/18 (2024.01); B60W 10/02 (2006.01); B64D 27/02 (2006.01); B64D 27/33 (2024.01); F02B 63/04 (2006.01); F16D 41/12 (2006.01); H02K 7/108 (2006.01); H02K 21/22 (2006.01);
U.S. Cl.
CPC ...
B64D 27/33 (2024.01); F02B 63/042 (2013.01); F16D 41/12 (2013.01); H02K 7/108 (2013.01); H02K 21/22 (2013.01); B64D 27/026 (2024.01);
Abstract

A power unit includes an engine including a driving shaft, a power generator provided on the driving shaft and configured to supply electric energy to a flight vehicle, and a thrust generator provided on an outer side of the power generator and configured to provide a propulsion force to the flight vehicle. When a temperature of the power generator is greater than or equal to a first temperature, the power generator and the thrust generator are decoupled from each other, and the power generator is driven by an output of the engine and supplies the electric energy to the flight vehicle. When the temperature of the power generator is less than the first temperature, the power generator and the thrust generator are coupled to each other, and the thrust generator is driven by the output of the engine and provides the propulsion force to the flight vehicle.


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