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US Patent 8418964 Fuel supply installation of an aircraft turbojet

Patent 8418964 was granted and assigned to Snecma on April, 2013 by the United States Patent and Trademark Office.

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Patent abstract

A fuel supply installation for a turbojet including two volumetric pumps for combining their flow rates is disclosed. The pumps include a main pump dimensioned for the full gas rate and an auxiliary pump controlled and dimensioned to provide the supplementary flow rate necessary on ignition.

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