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:
Jul. 01, 2025

Filed:

Sep. 28, 2023
Applicants:

Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, DE;

Rolls-royce Plc, London, GB;

Inventors:

Stephen Mountain, Derby, GB;

Christian Seydel, Stahsdorf, DE;

Gideon Daniel Venter, Berlin, DE;

Sebastian Kopp, Berlin, DE;

Assignee:

Rolls-Royce Deutschland Ltd & Co KG, Blankenfelde-Mahlow, DE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); B64D 41/00 (2006.01); F01D 15/10 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); B64D 41/00 (2013.01); F01D 15/10 (2013.01); F05D 2220/76 (2013.01); F05D 2260/4031 (2013.01);
Abstract

An apparatus for an aircraft includes an electric machine and a gas turbine. The gas turbine includes a compressor, a turbine unit having a high-pressure turbine and a low-pressure turbine, and a combustion chamber. The compressor is connected via a high-pressure shaft to the high-pressure turbine, and the low-pressure turbine is connected via a low-pressure shaft directly to an output shaft of the electric machine. The high-pressure shaft and the low-pressure shaft are rotatable in different directions. The electric machine is operable as a generator and may be operated as a motor to start the gas turbine. The output shaft is connected via a gear box unit and a free-wheel to the high-pressure shaft. The free-wheel separates the connection between the output shaft of the electric machine and the high-pressure shaft in the presence of a torque flow from the high-pressure shaft in a direction of the output shaft.


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