Abstract: An apparatus for activating a valve of an ejector in order to adapt the pressurization of a chamber in an aircraft turbojet engine comprising a device constructed and arranged to trigger the opening and/or closing of valve and/or the power of the valve as a function of the altitude at which the valve is located.
Type:
Grant
Filed:
August 15, 2012
Date of Patent:
December 15, 2015
Assignee:
SNECMA
Inventors:
Giuliana Elisa Rossi, Eddy Stéphane Joël Fontanel, Marie Gentilhomme