Rectangular adjusting thrust nozzle for gas turbine drive with adjusting flaps adjusted parallel to each other to set thrust vector for fast maneuverability

Rectangular adjusting thrust nozzle for gas turbine drive with adjusting flaps adjusted parallel to each other to set thrust vector for fast maneuverability

The thrust nozzle has two parallel side walls, two flaps to adjust the nozzle section, and an adjusting drive. The adjusting flaps (36,37) move via joint parts (32,33) in a link guide with a curved central section (26d). The adjusting drive (68,70) engages on the joint parts in such a way, that the...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: RODGERS, LEONARD JOHN
Format: Patent
Sprache:eng ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
COSMONAUTICS
HEATING
HELICOPTERS
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
TRANSPORTING
WEAPONS
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Beschreibung
Zusammenfassung:The thrust nozzle has two parallel side walls, two flaps to adjust the nozzle section, and an adjusting drive. The adjusting flaps (36,37) move via joint parts (32,33) in a link guide with a curved central section (26d). The adjusting drive (68,70) engages on the joint parts in such a way, that the flaps are pivoted in the same or the opposite direction. The flaps have are fastened to upstream flap sections (32b,c,d) and have rigid arms (40,41) with free ends hinged to angled levers (48,60) of the adjusting drive. The flaps are pivoted downwards relative to the flap sections, to adjust the divergence angle of the exhaust gas path.