Improved ground testing device for a turbomachine

A ground testing device for a turbomachine, including an aircraft engine (12) extending axially from an air inlet to a nozzle, a shroud (20) having an axis of revolution (A) and surrounding at least partially the engine (12) so as to create an annular air flow between the engine (12) and the shroud...

Full description

Saved in:
Bibliographic Details
Main Authors Josselin David Florian Regnard, Louis Robert Baudoin
Format Patent
LanguageEnglish
Published 22.05.2019
Subjects
MEASURING
PHYSICS
TESTING
TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES
TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
Online AccessGet full text

Cover

Be the first to leave a comment!
You must be logged in first