Supplementary air inlet openings for gas turbine in supersonic aeroplane

The air inlet comprises an aperture in the engine's lateral housing (13) which is closed by sliding (15) and pivoting (14) flaps. The sliding flap is made with the same thickness as the engine housing, apart from sections where it meets the housing and the pivoted flap. Each pivoting flap has a...

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Bibliographische Detailangaben
Hauptverfasser:	JOURDAIN, GERARD ERNEST ANDRE, BARDAGI, THIERRY PASCAL
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The air inlet comprises an aperture in the engine's lateral housing (13) which is closed by sliding (15) and pivoting (14) flaps. The sliding flap is made with the same thickness as the engine housing, apart from sections where it meets the housing and the pivoted flap. Each pivoting flap has a projection on its inner front edge and the sliding flap has a recess to receive it, and there is an elastic seal between the two.