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:
Jan. 18, 2022

Filed:

Nov. 30, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Thomas Roger Jacques Angevin, Alfortville, FR;

Arnaud Baudran, Paris, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); F02C 7/224 (2006.01); F02C 9/18 (2006.01); F02C 3/04 (2006.01); F01D 11/14 (2006.01); F02C 9/24 (2006.01); F15B 13/06 (2006.01); F15B 21/06 (2006.01); F02C 7/14 (2006.01);
U.S. Cl.
CPC ...
F02C 7/224 (2013.01); F01D 11/14 (2013.01); F02C 3/04 (2013.01); F02C 7/14 (2013.01); F02C 9/18 (2013.01); F02C 9/24 (2013.01); F15B 13/06 (2013.01); F15B 21/06 (2013.01); F05D 2220/32 (2013.01); F05D 2260/213 (2013.01); F05D 2260/601 (2013.01); F05D 2260/605 (2013.01); F05D 2270/64 (2013.01); F05D 2270/65 (2013.01); F15B 2211/426 (2013.01);
Abstract

A hydraulic and pneumatic control circuit for a turbojet, a main hydraulic line having an oil/fuel heat exchanger with a function of transferring heat from the oil flowing in an oil circuit of the turbojet to the fuel flowing in the main hydraulic line, the circuit having a first hydraulic line for feeding fuel to a combustion chamber of the turbojet, a second hydraulic line for feeding fuel to one or more actuators for controlling variable geometry equipment, each actuator being fed with fuel via an electrohydraulic servovalve, a pneumatic line for feeding air to a pneumatic control member for bleed valves of a compressor and a blade tip clearance control valve of a turbine of the turbojet, and a fuel/air heat exchanger positioned on the second hydraulic line upstream from the hydraulic servovalve and on the pneumatic line upstream from the pneumatic control member.


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