Abstract: A fuel intake tube passes radially through an engine casing. It is surrounded between the casing and an injector head by a second tube attached to the casing. Guidance means and a sealing element are provided between the fuel intake tube and the second tube. The device is equipped with one or more injector heads. The guidance means consist of two elements: a cap and cylindrical projections.
Type:
Grant
Filed:
December 4, 1980
Date of Patent:
October 18, 1983
Assignee:
Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, "S.N.E.L.M.A."
Inventors:
Gerard E. A. Jourdain, Marcel R. Soligny