EXHAUST COOLING SYSTEM OF AN AIRCRAFT WITH MODULATED EXHAUST COOLING

EXHAUST COOLING SYSTEM OF AN AIRCRAFT WITH MODULATED EXHAUST COOLING

Aspects of the disclosure are directed to a system 200 of an aircraft, comprising: at least one fairing 260, 262, a liner 230, and an actuator 220 configured to cause the at least one fairing 260, 262 to be translated relative to the liner 230 in order to obtain a modulation of a metering area 240 b...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BANGERTER, James P, PETERS, Donald W
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:Aspects of the disclosure are directed to a system 200 of an aircraft, comprising: at least one fairing 260, 262, a liner 230, and an actuator 220 configured to cause the at least one fairing 260, 262 to be translated relative to the liner 230 in order to obtain a modulation of a metering area 240 between the liner 230 and the at least one fairing 260, 262.