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.

Patent No.:

US 10428739 B1

PDF
Full Text
Expired
Date of Patent:
Oct. 01, 2019

Filed:

Jun. 10, 2016
Applicant:

Safran Helicopter Engines, Bordes, FR;

Inventor:

Jean-Michel Haillot, Beuste, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); B64D 41/00 (2006.01); F02C 3/13 (2006.01); F02C 6/08 (2006.01); F02C 9/18 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); B64D 41/00 (2013.01); F02C 3/13 (2013.01); F02C 6/08 (2013.01); F02C 9/18 (2013.01); B64D 2013/0611 (2013.01); F05D 2220/50 (2013.01); Y02T 50/53 (2013.01);
Abstract

A main power unit implements an optimization method in an aircraft including energy-consuming equipments, a cabin in which air is renewed and temperature and/or pressure of which are regulated by a regulation system, main power-generating engines, and a flight control unit. The main power unit is built into a compartment which is insulated from other zones of the aircraft with a fireproof bulkhead and fitted with an outside-air intake and an exhaust nozzle. The main power unit includes an engine-type power unit as a main power source, fitted with a gas generator and with a power turbine for driving equipments including a supercharger. The supercharger is coupled, via a regulation control which communicates with the control unit, with the regulation system in order to supply a necessary pneumatic energy to the cabin.


Find Patent Forward Citations

Haillot, Jean-Michel. (2019). Self-contained power unit for implementing a method for optimizing the operability of an aircraft propulsive unit (U.S. Patent No. 10428739). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10428739

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