Vapor-to-air heat exchanger for aircraft powerplant

Patent metadata

Field	Value
Publication number	US-11945598-B2
Application number	US-202217669536-A
Country	US
Kind code	B2
Filing date	Feb 11, 2022
Priority date	Feb 11, 2022
Publication date	Apr 2, 2024
Grant date	Apr 2, 2024

Abstract

A vapor-to-air heat exchanger for an aircraft powerplant that includes: a pressurized vapor source supplying vapor; and a condenser including a condenser inlet in fluid communication with the pressurized vapor source to receive the vapor, a condenser outlet, and at least one pneumatic vessel defining a cavity in fluid communication between the condenser inlet and the condenser outlet. The pneumatic vessel is reversibly inflatable to be configurable between a collapsed vessel configuration and an inflated vessel configuration. A volume of the cavity is greater in the inflated vessel configuration than in the collapsed vessel configuration. The pneumatic vessel is inflatable from the collapsed vessel configuration to the inflated vessel configuration when the cavity is pressurized by the vapor.

First claim

The invention claimed is:

1. A vapor-to-air heat exchanger for an aircraft powerplant, comprising:
a pressurized vapor source supplying vapor; and
a condenser including a condenser inlet in fluid communication with the pressurized vapor source to receive the vapor, a condenser outlet, and at least one pneumatic vessel defining a cavity in fluid communication between the condenser inlet and the condenser outlet, the at least one pneumatic vessel being reversibly inflatable to be configurable between a collapsed vessel configuration and an inflated vessel configuration, a volume of the cavity being greater in the inflated vessel configuration than in the collapsed vessel configuration, the at least one pneumatic vessel being inflatable from the collapsed vessel configuration to the inflated vessel configuration when the cavity is pressurized by the vapor.

2. The vapor-to-air heat exchanger of claim 1 , wherein the at least one pneumatic vessel is formed of flexible film sheets welded to one another.

3. The vapor-to-air heat exchanger of claim 2 , wherein at least one sheet of the flexible film sheets includes one or more of: a metallic layer; and a composite layer.

4. The vapor-to-air heat exchanger of claim 1 , wherein the at least one pneumatic vessel includes a top tubular portion proximate to the condenser inlet, a bottom tubular portion proximate to the condenser outlet, and at least one transverse tubular portion fluidly connected between the top tubular portion and the bottom tubular portion.

5. The vapor-to-air heat exchanger of claim 4 , wherein the condenser comprises a plurality of pneumatic vessels including the at least one pneumatic vessel, and the top tubular portion defines a portion of a supply manifold of the condenser.

6. The vapor-to-air heat exchanger of claim 4 , wherein the condenser comprises a plurality of pneumatic vessels including the at least one pneumatic vessel, and the bottom tubular portion defines a portion of a drainage manifold of the condenser.

7. The vapor-to-air heat exchanger of claim 1 , further comprising one or more of: a pressure regulating valve between the pressurized vapor source and the condenser inlet; and a pump between the condenser outlet and the pressurized vapor source.

8. The vapor-to-air heat exchanger of claim 1 , further comprising a support structure attached to the at least one pneumatic vessel for holding the at least one pneumatic vessel in a deployed position.

9. The vapor-to-air heat exchanger of claim 8 , wherein the support structure is configurable between a collapsed support configuration and an inflated support configuration, the support structure being inflatable from the collapsed support configuration to the inflated support configuration.

10. The vapor-to-air heat exchanger of claim 1 , wherein the at least one pneumatic vessel is in the inflated vessel configuration when the cavity is pressurized by the vapor to at least a nominal pressure, the pressurized vapor source supplying the vapor at a source pressure of at least the nominal pressure.

11. A vapor-to-air heat exchanger for an aircraft powerplant, comprising:
an evaporator supplying vapor; and
a condenser including:
a condenser inlet in fluid communication with the evaporator to receive vapor therefrom;
a condenser outlet; and
an array of pneumatic vessels spaced from one another in an array orientation so as to define at least one air flow path along a path orientation transverse to the array orientation, at least one pneumatic vessel of the array of pneumatic vessels defining an cavity, a plane transverse to the array orientation extending through the cavity, the cavity being in fluid communication between the condenser inlet and the condenser outlet, the at least one pneumatic vessel being inflatable when the cavity is pressurized by the vapor to transition from a collapsed vessel configuration to an inflated vessel configuration, a size of the at least one pneumatic vessel in the array orientation being greater in the inflated vessel configuration than in the collapsed vessel configuration.

12. The vapor-to-air heat exchanger of claim 11 , wherein the at least one pneumatized vessel includes a top tubular portion proximate to the condenser inlet, a bottom tubular portion proximate to the condenser outlet, and a plurality of transverse tubular portions fluidly connected between the top and the bottom tubular portions and spaced from one another in the path orientation.

13. The vapor-to-air heat exchanger of claim 12 , wherein the at least one pneumatic vessel includes a first vessel and a second vessel next to one another on either side of the at least one flow path, a first plurality of transverse tubular portions of the first vessel and a second plurality of transverse tubular portions of the second vessel being in a staggered relationship in the path orientation.

14. A powerplant for an aircraft, comprising:
a power unit rejecting heat at a nominal heat rejection rate; and
a vapor-to-air heat exchanger including:
an evaporator thermally coupled to the power unit so as to supply vapor at a nominal pressure upon the power unit rejecting heat at the nominal heat rejection rate; and
a condenser including a condenser inlet downstream of the evaporator, a condenser outlet, and at least one pneumatic vessel being inflatable and defining an cavity in fluid communication between the condenser inlet and the condenser outlet, the at least one pneumatic vessel being configurable between a collapsed vessel configuration and an inflated vessel configuration, the at least one pneumatic vessel being inflatable from the collapsed vessel configuration to the inflated vessel configuration upon the cavity being pressurized up to the nominal pressure.

15. The powerplant of claim 14 , wherein the at least one pneumatic vessel is constructed of a pair of flexible film sheets welded to one another.

16. The powerplant of claim 14 , wherein the at least one pneumatic vessel includes a top tubular portion proximate to the condenser inlet, a bottom tubular portion proximate to the condenser outlet, and at least one transverse tubular portion fluidly connected between the top and the bottom tubular portions.

17. The powerplant of claim 16 , wherein the condenser comprises a plurality of pneumatic vessels including the at least one pneumatic vessel, and the top tubular portion defines a portion of a supply manifold of the condenser.

18. The powerplant of claim 14 , further comprising one or more of: a pressure regulating valve between the evaporator and the condenser inlet; and a pump between the condenser outlet and the evaporator.

19. The powerplant of claim 14 , further comprising a support structure supporting the at least one pneumatic vessel and a carcass defining an air cavity, the support structure affixed to the carcass so as to orient the at least one pneumatic vessel relative to the air cavity.

20. The powerplant of claim 19 , wherein the support structure is configurable between a collapsed support configuration and an inflated support configuration, the support structure being inflatable from the collapsed support configuration to the inflated support configuration.

Assignees

• Pratt & Whitney Canada

Inventors

• Alecu Daniel

Classifications

• B64D33/12 Primary

  of retractable type · CPC title

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title

• F28D9/0031 Primary

  the conduits for one heat-exchange medium being formed by paired plates touching each other (F28D9/0012, F28D9/0025, F28D9/0081, F28D9/04 take precedence) · CPC title

• F28F21/08

  of metal · CPC title

• F28F2275/06

  by welding · CPC title