STAUSTRAHLTRIEBWERK FÜR ÜBER- UND HYPERSCHALLFLUGZEUG

The ramjet engine consists of an elongated body with two flat and parallel side walls, a fixed upper wall (4) and a sliding lower wall (5) with an obtuse-angled inverted V-section profile and front (11A, 11B) and rear (12) faces, an intake (16) for an oxidant flow, a combustion chamber (15) and an o...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: FALEMPIN, FRANCOIS, BOUCHEZ, MARC, LEVINE, VADIM
Format: Patent
Sprache:ger
Schlagworte:
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Beschreibung
Zusammenfassung:The ramjet engine consists of an elongated body with two flat and parallel side walls, a fixed upper wall (4) and a sliding lower wall (5) with an obtuse-angled inverted V-section profile and front (11A, 11B) and rear (12) faces, an intake (16) for an oxidant flow, a combustion chamber (15) and an outlet duct (17). The engine's fuel injector (9) is situated close to the edge (8) of the upper fixed wall, and the sliding lower wall has two faces (11A, 11B) with an inclined connecting surface (14). The first face (11A) lies parallel to the opposite surface of the upper wall, and the second face (11B) is inclined relative to the first.