Test cell for an aircraft turbine engine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10226651
APP PUB NO 20170216637A1
SERIAL NO

15415939

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Abstract

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A test cell for an aircraft turbojet, wherein the test cell comprises a U-shaped configuration, with a passageway in the form of an elongated corridor, an inlet chimney, and an outlet chimney. The corridor includes a securing area with a securing arm for holding the turbojet during its test. The passageway furthermore reveals an upstream shutter and a downstream shutter, the two shutters including one pivoting flap or a series of pivoting flaps. In the event of a fire, the shutters close due to autonomous return means. Gravity allows the flap(s) to come down to the closed position and to confine the turbojet in order to rapidly stifle the fire.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AERO BOOSTERS SAROUTE DE LIERS 121 HERSTAL (MILMORT) B-4041

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Raimarckers, Nicolas Tourinne, BE 23 259
Taccogna, Gaetano Bassenge, BE 2 6

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