Accumulator integrated into a fuel line
AssigneeSafran Aircraft Engines
InventorsYannick Schini, Arnaud Baudran, Eric Charles Pean
Life of this patent
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AssigneeSafran Aircraft Engines
InventorsYannick Schini, Arnaud Baudran, Eric Charles Pean
Estimating the term…
A fuel pressure accumulator for a fuel supply circuit of a turbine engine having at least one pipe is provided. The fuel pressure accumulator generally includes at least one housing adjacent to said pipe and receiving at least one deformable enclosure confining a gas and having at least one movable wall in contact with the fuel in order to dampen a fuel overpressure, where the housing is coaxial with the pipe and the accumulator has a permeable chamber delimited at least partially by the housing, pressurizing the deformable enclosure and communicating with the main fuel flow via a grid with staged walls tilted, with respect to a direction of the flow flowing along the grid, substantially in the direction of the deformable enclosure.
A fuel pressure accumulator for a fuel supply circuit of a turbine engine having a pipe in which a main flow of fuel flows from upstream to downstream, the fuel pressure accumulator comprising:
Dependencies are inferred from the claim text.