Title:
FUEL CONDITIONING SYSTEM AND METHOD FOR POWERING A TURBOMACHINE
Document Type and Number:
WIPO Patent Application WO/2024/083502
Kind Code:
A1
Abstract:
The invention relates to a fuel conditioning system (SC) configured to power an aircraft turbomachine (M) with fuel (Q) from a cryogenic tank (R), the conditioning system (SC) comprising: a fuel circuit (1); a distribution valve (5) configured to divide a main fuel flow (Q) into a primary fuel flow (Q1) flowing through a primary branch (11) of the fuel circuit (1) and a secondary fuel flow (Q2) flowing through a secondary branch (12); a manifold (6) configured to mix the primary fuel flow (Q1) and the secondary fuel flow (Q2) and reform the main fuel flow (Q); a third mechanical pump (23) and a recirculating heat exchanger (4) installed in the secondary branch (12).
Inventors:
MAALOUF SAMER (FR)
CAHUZAC ADRIEN (FR)
CAHUZAC ADRIEN (FR)
Application Number:
PCT/EP2023/077392
Publication Date:
April 25, 2024
Filing Date:
October 04, 2023
Export Citation:
Assignee:
SAFRAN (FR)
International Classes:
F02C3/22; F02C7/224; F02C9/40
Foreign References:
| FR3110937A1 | 2021-12-03 | |||
| GB2240813A | 1991-08-14 | |||
| US20200088098A1 | 2020-03-19 |
Attorney, Agent or Firm:
ARGYMA (FR)
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