Sound-attenuating heat exchangers and methods of utilizing the same

Patent metadata

Field	Value
Publication number	US-11060480-B2
Application number	US-201715812946-A
Country	US
Kind code	B2
Filing date	Nov 14, 2017
Priority date	Nov 14, 2017
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

Sound-attenuating heat exchangers and methods of utilizing the same are disclosed herein. The sound-attenuating heat exchangers include an aerodynamically shaped layer, a base, an intermediate layer, and a cooled fluid containment body. The aerodynamically shaped layer defines an aerodynamically shaped surface, an opposed intermediate layer-facing surface, and a plurality of apertures. The intermediate layer defines a shaped layer-facing surface and an opposed base-facing surface. The base defines a base surface. The intermediate layer-facing surface at least partially defines a sound-attenuating volume. The base surface at least partially defines an elongate cooling conduit. The sound-attenuating volume is distinct from the elongate cooling conduit and the intermediate layer at least partially fluidly isolates the sound-attenuating volume from the elongate cooling conduit. The cooled fluid containment body at least partially defines a cooled fluid containment conduit. The methods include methods of utilizing the sound-attenuating heat exchangers.

First claim

The invention claimed is:

1. A sound-attenuating heat exchanger, comprising:
an aerodynamically shaped layer;
a base;
an intermediate layer extending at least partially between the aerodynamically shaped layer and the base; and
a cooled fluid containment body;
wherein:
(i) the aerodynamically shaped layer defines an aerodynamically shaped surface, which is shaped to direct flow of a first fluid stream that includes a first fluid, an opposed intermediate layer-facing surface, which faces toward the intermediate layer, and a plurality of apertures;
(ii) the intermediate layer defines a shaped layer-facing surface, which faces toward the aerodynamically shaped layer, and an opposed base-facing surface, which faces toward the base;
(iii) the base defines a base surface, which faces toward the intermediate layer;
(iv) the intermediate layer-facing surface of the aerodynamically shaped layer and the shaped layer-facing surface of the intermediate layer together at least partially define a sound-attenuating volume that is configured to be in fluid communication with the first fluid stream, via the plurality of apertures, and is configured to attenuate sound energy from the first fluid stream;
(v) the base surface of the base and the base-facing surface of the intermediate layer together at least partially define an elongate cooling conduit that extends between a cooling conduit inlet and a cooling conduit outlet and is configured to receive a cooling stream, which includes the first fluid, in heat exchange relationship with the cooled fluid containment body;
(vi) the sound-attenuating volume is distinct from the elongate cooling conduit and the intermediate layer at least partially fluidly isolates the sound-attenuating volume from the elongate cooling conduit;
(vii) the cooled fluid containment body at least partially defines a cooled fluid containment conduit that extends between a cooled fluid containment conduit inlet and a cooled fluid containment conduit outlet and is configured to receive a cooled stream that includes a second fluid;
the sound-attenuating volume is defined between the aerodynamically shaped layer and the intermediate layer;
the elongate cooling conduit is defined between the intermediate layer and the base; and
the cooled fluid containment body includes a plurality of distinct cooled fluid containment tubulars that extends within the elongate cooling conduit.

2. The sound-attenuating heat exchanger of claim 1 , wherein the cooled fluid containment body includes a cooled fluid containment layer, and further wherein the cooled fluid containment conduit is defined between the cooled fluid containment layer and the intermediate layer.

3. The sound-attenuating heat exchanger of claim 2 , wherein the sound-attenuating volume is defined between the aerodynamically shaped layer and the intermediate layer.

4. The sound-attenuating heat exchanger of claim 2 , wherein the elongate cooling conduit is defined between the cooled fluid containment body and the base.

5. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating heat exchanger includes a unitary structure that defines at least two of the aerodynamically shaped layer, the base, the intermediate layer, and the cooled fluid containment conduit.

6. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating volume is defined between the aerodynamically shaped layer and intermediate layer, and further wherein the elongate cooling conduit is defined entirely between the intermediate layer and the base.

7. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating heat exchanger further includes a plurality of supporting elements that extends between the plurality of distinct cooled fluid containment tubulars and at least one of the intermediate layer and the base.

8. The sound-attenuating heat exchanger of claim 7 , wherein at least a subset of the plurality of supporting elements is fluid-permeable.

9. The sound-attenuating heat exchanger of claim 7 , wherein at least a subset of the plurality of supporting elements is fluid-impermeable.

10. The sound-attenuating heat exchanger of claim 1 , wherein the plurality of distinct cooled fluid containment tubulars is a plurality of distinct first cooled fluid containment tubulars, wherein the sound-attenuating heat exchanger includes a plurality of distinct second cooled fluid containment tubulars that extends within the sound-attenuating volume, wherein the sound-attenuating heat exchanger further includes a plurality of second supporting elements that extends between the plurality of distinct second cooled fluid containment tubulars and at least one of the intermediate layer and the aerodynamically shaped layer, and further wherein at least a subset of the plurality of second supporting elements is fluid-permeable.

11. The sound-attenuating heat exchanger of claim 10 , wherein at least a subset of the plurality of second supporting elements is fluid-impermeable.

12. The sound-attenuating heat exchanger of claim 1 , wherein a transverse cross-sectional shape of at least one of the sound-attenuating volume and the elongate cooling conduit, as measured transverse to a longitudinal axis of the elongate cooling conduit, is at least one of:
(i) triangular;
(ii) isosceles triangular; and
(iii) rectangular.

13. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating volume defines a Helmholtz resonator.

14. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating volume is configured to receive sound waves from the first fluid stream via the apertures and to attenuate the sound waves therewithin.

15. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating heat exchanger further includes a plurality of heat transfer-enhancing structures configured to enhance heat transfer between the cooled stream and the cooling stream, wherein at least a subset of the plurality of heat transfer-enhancing structures at least one of:
(i) projects from the base-facing surface of the intermediate layer and within the elongate cooling conduit;
(ii) projects from the base surface of the base and within the elongate cooling conduit; and
(iii) projects from the cooled fluid containment body and within the elongate cooling conduit.

16. The sound-attenuating heat exchanger of claim 1 , wherein the sound-attenuating heat exchanger includes a plurality of distinct sound-attenuating volumes and a plurality of distinct elongate cooling conduits.

17. The sound-attenuating heat exchanger of claim 1 , wherein the cooled fluid containment body includes a plurality of dendritic tubulars that extends within the cooled fluid containment conduit and defines a plurality of distinct elongate cooling conduits.

18. A jet engine installation, comprising:
a fan;
a fan housing;
a turbine assembly mechanically coupled to, and configured to rotate with, the fan;
a turbine housing at least partially surrounding the turbine assembly and defining a housing aerodynamically shaped surface;
a nacelle at least partially surrounding the fan, the turbine assembly, and the turbine housing and defining a nacelle aerodynamically shaped surface; and
the sound-attenuating heat exchanger of claim 1 , wherein the aerodynamically shaped surface of the sound-attenuating heat exchanger forms at least a portion of at least one of the housing aerodynamically shaped surface, the fan housing, and the nacelle aerodynamically shaped surface.

19. An

Assignees

• Boeing Co

Inventors

• Foutch David William
• Shivashankara Belur

Classifications

• F28D9/0025

  the conduits being formed by zig-zag bend plates · CPC title

• F28F2210/02

  with particular branching, e.g. fractal conduit arrangements · CPC title

• F28D9/0043

  the plates having openings therein for circulation of at least one heat-exchange medium from one conduit to another · CPC title

• F05D2260/963

  by Helmholtz resonators · CPC title

• F02C7/045 Primary

  having provisions for noise suppression · CPC title