Heat exchanger

Patent metadata

Field	Value
Publication number	US-2018335263-A1
Application number	US-201815981887-A
Country	US
Kind code	A1
Filing date	May 16, 2018
Priority date	May 17, 2017
Publication date	Nov 22, 2018
Grant date	—

Abstract

A heat exchanger may include a tubular housing, a flange ring, two bases, and heat exchanger tubes running through the housing and respectively held at a longitudinal end side in the bases, a first flow channel formed therein, and a second flow channel formed between the tubes and the housing. The housing may be formed from first and second housing parts each being pot-shaped and having a housing portion, an outwardly widened flange ring portion, and a base. The housing parts may be connected to one another via the flange ring portions that may delimit an annular space. On the first housing part, inlet and outlet connecting-pieces for coolant may be provided. Between the housing and the heat exchanger tubes, at least one separator may be arranged, on which at least one blade may be provided, the blade engaging at least partly into the annular space and at least reducing a circumferential flow therein.

First claim

1 . A heat exchanger comprising:
a tubular housing; a flange ring; two bases; and heat exchanger tubes, which run through the housing and are respectively held at a longitudinal end side in the bases, wherein in the heat exchanger tubes, a first flow channel is formed, and a second flow channel is formed between the heat exchanger tubes and the housing;
wherein the housing is formed from a first housing part and a second housing part each being pot-shaped and having a housing portion, an outwardly widened flange ring portion, and a base, and wherein the first and second housing parts are connected to one another via the flange ring portions, wherein the flange ring portions delimit an annular space;
wherein on the first housing part, an inlet connecting-piece and an outlet connecting-piece for coolant are provided; and
wherein between the housing and the heat exchanger tubes, at least one separator is arranged, on which at least one blade is provided, the at least one blade engages at least partly into the annular space and at least reduces a circumferential flow therein.

2 . The heat exchanger according to claim 1 , wherein the at least one blade is stamped out from the separator and shaped.

3 . The heat exchanger according to claim 1 , wherein an external geometry of the at least one blade is configured in a complementary manner to an internal geometry of the annular space.

4 . The heat exchanger according to claim 1 , wherein at least one of:
the at least one separator has at least one injector opening; and the at least one separator has at least one NACA (National Advisory Committee for Aeronautics) opening.

5 . The heat exchanger according to claim 1 , wherein the at least one blade includes at least two blades having identical radial heights.

6 . The heat exchanger according to claim 1 , wherein one of:
the at least one separator is securely connected to at least one of the first housing part and the second housing part; or the at least one blade serves as positioning contour for aligning and positioning the at least one separator in the housing.

7 . The heat exchanger according to claim 1 , wherein the first and second housing parts are soldered, welded or joined to one another on the flange ring portions.

8 . The heat exchanger according to claim 1 , wherein the heat exchanger is configured as an exhaust gas heat exchanger.

9 . The heat exchanger according to claim 1 , wherein at least one of the first and second housing parts is configured as a one-piece, shaped, sheet-metal stamped part.

10 . The heat exchanger according to claim 9 , wherein the at least one of the first and second housing parts is produced by deep-drawing.

11 . The heat exchanger according to claim 1 , wherein the at least one blade includes at least two blades having different radial heights.

12 . The heat exchanger according to claim 2 , wherein an external geometry of the at least one blade is configured in a complementary manner to an internal geometry of the annular space.

13 . The heat exchanger according to claim 2 , wherein at least one of:
the at least one separator has at least one injector opening; and the at least one separator has at least one NACA (National Advisory Committee for Aeronautics) opening.

14 . The heat exchanger according to claim 2 , wherein the at least one blade includes at least two blades having identical radial heights or having different radial heights.

15 . The heat exchanger according to claim 2 , wherein one of:
the at least one separator is securely connected to at least one of the first housing part and the second housing part; or the at least one blade serves as positioning contour for aligning and positioning the at least one separator in the housing.

16 . The heat exchanger according to claim 2 , wherein the first and second housing parts are soldered, welded or joined to one another on the flange ring portions.

17 . A heat exchanger comprising:
a tubular housing formed from a first housing part and a second housing part each being pot-shaped and having a housing portion, an outwardly widened flange ring portion, and a base, the first and second housing parts being connected to one another via the flange ring portions, wherein the flange ring portions delimit an annular space; an inlet connecting-piece and an outlet connecting-piece for coolant on the first housing part; a flange ring; two bases; and heat exchanger tubes, which run through the housing and are respectively held at a longitudinal end side in the bases, wherein in the heat exchanger tubes, a first flow channel is formed, and a second flow channel is formed between the heat exchanger tubes and the housing; and at least one separator arranged between the housing and the heat exchanger tubes, at least two blades being provided on the at least one separator, the at least one blade engaging at least partly into the annular space and at least reducing a circumferential flow therein; wherein an external geometry of the at least two blades is configured in a complementary manner to an internal geometry of the annular space; and wherein the least two blades have identical radial heights or differing radial heights.

18 . The heat exchanger according to claim 17 , wherein at least one of:
the at least one separator has at least one injector opening; and the at least one separator has at least one NACA (National Advisory Committee for Aeronautics) opening.

19 . The heat exchanger according to claim 17 , wherein one of:
the at least one separator is securely connected to at least one of the first housing part and the second housing part; or the at least one blade serves as positioning contour for aligning and positioning the at least one separator in the housing.

20 . The heat exchanger according to claim 17 , wherein the first and second housing parts are soldered, welded or joined to one another on the flange ring portions.

Assignees

• Mahle Int Gmbh

Inventors

• Faber Christian
• Hund Simon
• Kraemer Bernd
• Siegel Albrecht

Classifications

• F02G5/02

  Profiting from waste heat of exhaust gases · CPC title

• F28D21/0003 Primary

  the heat being recuperated from exhaust gases (F28D21/0014 takes precedence) · CPC title

• F28F1/40

  the means being only inside the tubular element · CPC title

• F28D7/1684

  the conduits having a non-circular cross-section · CPC title

• F28F13/06

  by affecting the pattern of flow of the heat-exchange media {(F28F13/003 takes precedence; static flow control means in header boxes F28F9/026)} · CPC title