US 11,754,020 B2
Heat exchanger for a turbomachine and manufacturing thereof
Lancelot Guillou, Moissy-Cramayel (FR); and Stéphane Louis Lucien Auberger, Moissy-Cramayel (FR)
Assigned to SAFRAN AIRCRAFT ENGINES, Paris (FR)
Appl. No. 17/264,636
Filed by Safran Aircraft Engines, Paris (FR)
PCT Filed Jul. 30, 2019, PCT No. PCT/FR2019/051871
§ 371(c)(1), (2) Date Jan. 29, 2021,
PCT Pub. No. WO2020/025895, PCT Pub. Date Feb. 6, 2020.
Claims priority of application No. 1857152 (FR), filed on Jul. 31, 2018.
Prior Publication US 2021/0310443 A1, Oct. 7, 2021
Int. Cl. F02K 3/115 (2006.01); F01D 25/12 (2006.01); F02C 7/14 (2006.01); F28F 1/02 (2006.01); F28F 1/26 (2006.01)
CPC F02K 3/115 (2013.01) [F01D 25/12 (2013.01); F02C 7/14 (2013.01); F28F 1/022 (2013.01); F28F 1/26 (2013.01); F05D 2240/81 (2013.01); F05D 2260/213 (2013.01); F05D 2260/22141 (2013.01); F28F 2220/00 (2013.01)] 10 Claims
OG exemplary drawing
 
1. An annular heat exchanger of a longitudinal axis for a turbomachine, comprising:
a one-piece annular part comprising a first fluid circuit comprising a first conduit and a second conduit extending annularly, wherein the first conduit and the second conduit open into a first cavity formed at a circumferential first end of said annular part, wherein a plurality of removable sealing means is attached to said first end are configured to allow a flow of fluid from the second conduit, into the first cavity and then into the first conduit, wherein a second fluidic circuit comprising a third conduit and a fourth conduit is arranged on either side of the first conduit and the second conduit of the first fluid circuit in a circumferential direction extending annularly and perpendicular to the longitudinal axis, and wherein the third conduit and the fourth conduit of the second fluidic circuit open into a second cavity formed at the first circumferential end of said annular part and arranged radially outside the first cavity in a direction perpendicular to the longitudinal axis and the circumferential direction, the plurality of removable sealing means also being attached at said first end so as to allow a flow of fluid from the fourth conduit of the second fluidic circuit, into the second cavity and then into the third conduit of the second fluidic circuit.