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:
Aug. 02, 2016

Filed:

Jan. 23, 2013
Applicant:

Airbus Helicopters, Marignane, FR;

Inventor:

Laurent Martin, Chateaurenard, FR;

Assignee:

Airbus Helicopters, Marignane, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F02C 9/56 (2006.01);
U.S. Cl.
CPC ...
F02C 9/00 (2013.01); F02C 9/56 (2013.01); F05D 2220/329 (2013.01); F05D 2270/303 (2013.01); F05D 2270/304 (2013.01); F05D 2270/305 (2013.01);
Abstract

A regulator device () for regulating a turbine engine (). The regulator device () includes mechanical power take-off means () for taking off power mechanically from a gas generator (), and an engine computer () controlling said engine () to comply with at least a first limitation (LimTET, LimT45) of a temperature (TET, T45) of the gas within the engine, and with a second limitation (LimNg) of a speed of rotation (Ng) of the gas generator (). The engine computer () determines whether the speed of rotation (Ng) of the gas generator has reached said second limitation (LimNg), and whether said temperature (TET, T45) has reached said first limitation (LimTET, LimT45). An avionics computer () causes the mechanical power take-off means () to operate if the speed of rotation (Ng) of the gas generator () has reached said second limitation (LimNg), and if said temperature (TET, T45) has not reached said first limitation (LimTET, LimT45).


Find Patent Forward Citations

Martin, Laurent. (2016). Device and a method of regulating a power plant including at least one turbine engine, and an aircraft (U.S. Patent No. 9404425). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/9404425

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

Loading…