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:
Oct. 08, 2024

Filed:

May. 23, 2022
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Michael Adam Zagrodnik, Singapore, SG;

Krishnamoorthi Sivalingam, Singapore, SG;

Satyanarayana Reddy Gajjela, Singapore, SG;

Vidor Veres-Székely, Mosdós, HU;

Daniel Lorincz, Singapore, SG;

István Örökös-Tóth, Egar, HU;

Anand Prabhu Mathivanan, Singapore, SG;

Umesh Mahajan, Derby, GB;

Rakesh Murali, Singapore, SG;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60L 58/26 (2019.01); B64C 29/00 (2006.01); B64D 33/08 (2006.01);
U.S. Cl.
CPC ...
B60L 58/26 (2019.02); B64C 29/0008 (2013.01); B64D 33/08 (2013.01); B60L 2200/10 (2013.01);
Abstract

Aircraft with battery thermal regulation systems, including: an aircraft air inlet and an aircraft air outlet; a battery pack including battery cells; and a battery thermal regulation system including a first air channel, a surface of which is in thermal communication with the battery cells so that air flowing through the first air channel exchanges heat with the cells through the surface; and an airflow device for driving an airflow. The battery thermal regulation system has a first and a second mode operation. In the first mode, the first air channel is fluidly connected with the aircraft air inlet and the aircraft air outlet whereby, during flight of the aircraft, air can enter the aircraft through the air inlet, flow through the first air channel and exit the aircraft through the air outlet. In the second mode, the airflow device drives an airflow through the first air channel.


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