초록 ▼

An aircraft includes a heat exchanger between a first fluid that flows into the narrow pipes of the exchanger and that is able to contain solid elements that can melt, and, a second fluid to be cooled. The heat exchanger includes a device for preheating the first fluid upstream from the pipes of the

An aircraft includes a heat exchanger between a first fluid that flows into the narrow pipes of the exchanger and that is able to contain solid elements that can melt, and, a second fluid to be cooled. The heat exchanger includes a device for preheating the first fluid upstream from the pipes of the exchanger, a number of pipes arranged in at least one plane that intersects the direction of flow of the first fluid, whereby the spacing between two adjacent pipes is suitable for retaining the solid elements of large dimensions and for allowing them to pass only when they have melted at least partially.

대표청구항 ▼

1. An aircraft that comprises: a liquid-liquid heat exchanger between a first liquid fluid which is fuel that flows into a plurality of first pipes (22) of said exchanger and that is able to contain ice crystals that can melt, and a second liquid heat exchange fluid to be cooled;the first liquid flu

1. An aircraft that comprises: a liquid-liquid heat exchanger between a first liquid fluid which is fuel that flows into a plurality of first pipes (22) of said exchanger and that is able to contain ice crystals that can melt, and a second liquid heat exchange fluid to be cooled;the first liquid fluid being canalized in a supply pipe (24); anda preheating device configured for preheating the first fluid upstream from the plurality of first pipes (22) of the exchanger, the preheating device being arranged in the supply pipe (24), the preheating device comprising a plurality of second pipes (28) arranged in at least one plane that intersects a direction of flow of the first fluid, a spacing between two adjacent second pipes of the device for preheating being suitable for retaining the ice crystals having dimensions larger than the spacing and for allowing the ice crystals to pass only when the ice crystals have melted at least partially,at least two series of the plurality of second pipes (28), whereby the spacing between said plurality of second pipes (28) decreases from one series to the next in the direction of flow of the first fluid, andD being a diameter of the first pipes (22), the pipes of a last series of pipes of the pre-heating device are separated from one another by a distance greater than or at least equal to D. 2. The aircraft according to claim 1, wherein the preheating device is arranged at a level of a pipe (24) for supply of the first fluid of the exchanger. 3. The aircraft according to claim 1, wherein the preheating device further comprises: a first series (30.1) of the plurality of second pipes (28) with a spacing D1 between them that is less than or equal to approximately three times a diameter of the plurality first pipes (22) of the exchanger; anda second series (30.2) of the plurality of second pipes (28) with a spacing D2 between them that is less than or equal to two times the diameter of the plurality of first pipes (22) of the exchanger. 4. The aircraft according to claim 3, wherein the preheating circuit further comprises a third series (30.3) of the plurality of second pipes (28) with a spacing D3 between them that is less than or equal to approximately 1.3 times the diameter of the plurality of first pipes (22) of the exchanger. 5. The aircraft according to claim 1, wherein a plate (26) separates a chamber (10) that contains the second fluid and a pipe (24) for supply of the first fluid, and said plate comprises a plurality of openings that each work with a pipe (22) of the plurality of first pipes of the exchanger, wherein ends of the plurality of first pipes (22) of the exchanger or openings of the plate (26) are flared in a direction of the supply pipe (24). 6. The aircraft according to claim 5, wherein a widest cross-section of ends of the plurality of first pipes (22) of the exchanger or openings of the plate (26) has a diameter on the order of 1.5 times the diameter of the pipes of the exchanger. 7. The aircraft according to claim 1, wherein the second fluid is oil. 8. A liquid-liquid heat exchanger, comprising: a plurality of first pipes, the plurality of first pipes being adapted to contain a first liquid fluid and meltable solid elements, the first liquid fluid being canalized in a supply pipe, and a second liquid heat exchange fluid to be cooled; anda preheater upstream from the plurality of first pipes, the preheater being arranged in a supply pipe, the preheater comprising a plurality of second pipes arranged in a plane intersecting a direction of flow of the first fluid, andand a spacing between two adjacent second pipes of the preheater is suitable for retaining the solid elements having dimensions larger than the spacing and for allowing the solid elements to pass only when the solid elements have melted at least partially, whereina preheating circuit comprises at least two series of the plurality of pipes, and the spacing between said plurality of pipes decreases from one series to the next in the direction of flow of the first fluid, andD being a diameter of the first pipes, the pipes of a last series of pipes of the preheater are separated from one another by a distance greater than or at least equal to D. 9. The liquid-liquid heat exchanger according to claim 8, wherein the preheater is arranged at a level of a pipe for supply of the first fluid of the exchanger. 10. The liquid-liquid heat exchanger according to claim 8, wherein the preheating circuit further comprises: a first series of pipes with a spacing D1 between them that is less than or equal to approximately three times a diameter of the pipes of the exchanger; anda second series of pipes with a spacing D2 between them that is less than or equal to two times the diameter of the pipes of the exchanger. 11. The liquid-liquid heat exchanger according to claim 10, wherein the preheating circuit further comprises a third series of pipes with a spacing D3 between them that is less than or equal to approximately 1.3 times the diameter of the pipes of the exchanger. 12. The liquid-liquid heat exchanger according to claim 10, wherein a plate separates a chamber that contains the second fluid and a supply pipe of the first fluid, and said plate comprises a plurality of openings that each work with a pipe of the plurality of first pipes of the exchanger, wherein ends of the plurality of first pipes of the exchanger or openings of the plate are flared in a direction of the supply pipe. 13. The liquid-liquid heat exchanger according to claim 12, wherein a widest cross-section of the plurality of first pipes of the exchanger or openings of the plate has a diameter on the order of 1.5 times the diameter of the pipes of the exchanger. 14. The liquid-liquid heat exchanger according to claim 8, wherein the first fluid is fuel and the solid elements are ice crystals. 15. The liquid-liquid heat exchanger according to claim 8, wherein the second fluid is oil. 16. A liquid-liquid heat exchanger, comprising: a plurality of first pipes, the plurality of first pipes being adapted to contain a liquid fuel and meltable ice crystals, and heat exchange oil to be cooled, the liquid fuel being canalized in a supply pipe; anda preheater upstream from the plurality of first pipes, the preheater being arranged in the supply pipe, the preheater comprising a plurality of second pipes arranged in a plane intersecting a direction of flow of the liquid fuel, andand a spacing between two adjacent second pipes of the preheater is suitable for retaining the ice crystals having dimensions larger than the spacing and for allowing the solid elements to pass only when the ice crystals have melted at least partially, whereina preheating circuit comprises: a first series of the plurality of second pipes with a spacing D1 between them that is less than or equal to approximately three times a diameter of the plurality first pipes of the exchanger; anda second series of the plurality of second pipes with a spacing D2 between them that is less than or equal to two times the diameter of the plurality of first pipes of the exchanger, andD being a diameter of the first pipes, the pipes of a last series of pipes of the preheater are separated from one another by a distance greater than or at least equal to D.