Invention Grant
- Patent Title: Accumulator integrated into a fuel line
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Application No.: US16206618Application Date: 2018-11-30
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Publication No.: US10731784B2Publication Date: 2020-08-04
- Inventor: Yannick Schini , Arnaud Baudran , Eric Charles Pean
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Christensen O'Connor Johnson Kindness PLLC
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@7c8e00a8
- Main IPC: F16L55/054
- IPC: F16L55/054 ; F02C7/22 ; F16L55/053 ; F02M37/00 ; F16L55/045 ; F16L55/052 ; F16L55/04 ; F16L55/02

Abstract:
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.
Public/Granted literature
- US20190170096A1 ACCUMULATOR INTEGRATED INTO A FUEL LINE Public/Granted day:2019-06-06
Information query
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