Back to results
US 11,125,511 B2Granted
Matrix for an air/oil heat exchanger of a jet engine
AssigneeSafran Aero Boosters SA
InventorsVincent Thomas, Bruno Servais, Roel Vleugels
Life of this patent
Estimating the term…
Abstract
Matrix (30) for a heat exchanger to exchange heat between a first fluid and a second fluid, the first fluid being for instance air and the second fluid being for instance oil. The matrix (30) comprises: a channel for the first fluid. an array of passages for the second fluid, the passages extending in the channel. The array supports at least two cooling fins. The matrix is made by a process of additive manufacturing. The fins are inclined with respect to each other along the direction of the flow of the first fluid.
Claims4
Matrix for a heat exchanger of a turbojet engine, the matrix comprising:
- a channel for a first fluid, the channel defining a main direction along which the first fluid flows;
- an array of tubes defining passages for a second fluid, the tubes extending in the channel, the array of tubes comprising three tubes arranged in a staggered manner, each tube of the three tubes being parallel to each other tube of the three tubes, the three tubes being constituted by a first tube, a second tube and a third tube;
- wherein the three tubes support at least two fins arranged one behind the other in the main direction;
- wherein the at least two fins are planar, extend in parallel with the main direction and are inclined relative to one another;
- wherein each fin of the at least two fins has a first end and a second end;
- wherein the first end of a first fin of the at least two fins is connected to the first tube, the first end of a second fin of the at least two fins is connected to the third tube;
- and
- wherein the second end of the first fin and the second end of the second fin are connected to the second tube.
5 more elements
Dependencies are inferred from the claim text.