COMPRESSION COWL FOR JET ENGINE EXHAUST

A compression inner core cowling 76 for a jet engine 10 can have a concave annular section 90 of the core cowling 76. The concave section 76 can begin within the expanse of an outer fan cowl 40 and extend aft of the fan cowl 40 toward the tail cone 94, defining an annular bypass section 80 between t...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	IGLEWSKI, Tomasz
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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