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:
Apr. 13, 2021

Filed:

Dec. 14, 2017
Applicant:

Airbus Operations, S.l., Madrid, ES;

Inventors:
Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/268 (2006.01); F02C 7/06 (2006.01); F01D 25/20 (2006.01); F01D 25/10 (2006.01); F02C 7/14 (2006.01); F28D 7/00 (2006.01); B64D 41/00 (2006.01); F02C 7/22 (2006.01);
U.S. Cl.
CPC ...
F02C 7/06 (2013.01); F01D 25/10 (2013.01); F01D 25/20 (2013.01); F02C 7/14 (2013.01); F02C 7/268 (2013.01); F28D 7/0008 (2013.01); B64D 41/00 (2013.01); F02C 7/22 (2013.01); F05D 2220/323 (2013.01); F05D 2220/76 (2013.01); F05D 2260/213 (2013.01); F05D 2260/85 (2013.01); F05D 2260/98 (2013.01); F05D 2270/303 (2013.01); Y02T 50/60 (2013.01);
Abstract

An oil heating system in a turbine engine such as an aircraft turbojet or turboprop main engines, or in an aircraft auxiliary power unit (APU). The turbine oil heating system includes a turbine engine oil circuit for conducting lubricating oil to the turbine engine, an electric starter generator oil circuit for conducting cooling oil from the electric starter generator, and an oil-to-oil heat exchanger connected with the engine oil circuit and connectable with the electric starter generator oil circuit, for transferring heat from the starter generator oil to the engine oil as to warm-up the engine oil during turbine engine motoring prior to actual starting sequence. A low cost and highly integrated system is therefore provided for reducing drag torque of a turbine engine prior to the starting phase.


Find Patent Forward Citations

Loading…