ECS dual entry ram inlet plenum

Patent metadata

Field	Value
Publication number	US-11396378-B2
Application number	US-201815879108-A
Country	US
Kind code	B2
Filing date	Jan 24, 2018
Priority date	Jan 24, 2018
Publication date	Jul 26, 2022
Grant date	Jul 26, 2022

Abstract

An environmental control system of an aircraft with a power turbine includes a heat exchanger and a plenum attached to and in fluid communication with the heat exchanger. The plenum includes a housing with a first inlet fluidly connected to the power turbine, a second inlet fluidly connected to a source of ram air, and an outlet fluidly connected to the heat exchanger.

First claim

The invention claimed is:

1. An environmental control system of an aircraft, the environmental control system comprising:
a heat exchanger comprising:
a cold layer having an inlet face and an outlet face; and
a hot layer disposed adjacent to the cold layer;
wherein the heat exchanger is configured to transfer thermal energy from the hot layer to cool air flowing through the cold layer;

a power turbine; and
an inlet plenum attached to and in fluid communication with the inlet face of the cold layer of the heat exchanger, wherein the inlet plenum includes a housing comprising:
a first inlet fluidly connected to the power turbine and configured to intake a first stream of cool air;
a second inlet fluidly connected to a source of ram air and configured to intake a second stream of cool air; and
an outlet fluidly connected to the inlet face of the cold layer of the heat exchanger, wherein:
the first and second inlets are disposed in a portion of the inlet plenum;
the first and second inlets are fluidly connected to the outlet such that the outlet is configured to provide the first and second streams of cool air to the cold layer of the heat exchanger;
a direction of airflow through the cold layer of the heat exchanger is perpendicular to an axis of the environmental control system;
the first inlet extends along a first inlet axis parallel to the axis of the environmental control system; and
the second inlet extends on a second inlet axis parallel to the axis of the environmental control system and the first inlet axis.

2. The environmental control system of claim 1 , further comprising a nozzle disposed within the inlet plenum housing.

3. The environmental control system of claim 2 , wherein the nozzle is configured to disperse a cooling fluid into air passing through the inlet plenum housing.

4. The environmental control system of claim 1 , wherein the first inlet is located on an upper portion of the plenum housing, and the second inlet is located on a lower portion of the plenum housing.

5. The environmental control system of claim 1 , further comprising:
a detachable access panel disposed along an outer surface of the inlet plenum housing; and
a gasket disposed around an exterior of the detachable access panel such that the gasket forms a seal between the detachable access panel and the outer surface of the inlet plenum housing.

6. The environmental control system of claim 1 , wherein the inlet plenum housing further comprises a sidewall opposite the outlet, wherein the sidewall includes a tapered contour configured to direct a flow of fluid from the second inlet towards the outlet.

7. The environmental control system of claim 1 , wherein the heat exchanger comprises a bleed air heat exchanger, a fresh air heat exchanger, and a chiller heat exchanger.

8. The environmental control system assembly of claim 7 , wherein the chiller, fresh air, and bleed air heat exchangers are brazed together to form a single unitized tri-heat exchanger.

9. The environmental control system of claim 1 , wherein the housing is configured to direct a mixed air stream of air sources from both of the first inlet and the second inlet to the outlet and to the inlet face of the heat exchanger.

10. An environmental control system for an aircraft, the environmental control system comprising:
a heat exchanger comprising:
a cold layer having an inlet face and an outlet face; and
a hot layer disposed adjacent to the cold layer;
wherein the heat exchanger is configured to transfer thermal energy from the hot layer to cool air flowing through the cold layer;

an inlet plenum fluidly connected to the inlet face of the heat exchanger and attached to the heat exchanger, wherein the inlet plenum includes a housing comprising:
a first inlet disposed in the housing and configured to intake a first stream of cool air;
a second inlet disposed in the housing and configured to intake a second stream of cool air; and
an outlet fluidly connected to the inlet face of the cold layer of the heat exchanger, wherein:
the first and second inlets are disposed in a portion of the inlet plenum;
the first and second inlets are fluidly connected to the outlet such that the outlet is configured to provide the first and second streams of cool air to the cold layer of the heat exchanger;
a direction of airflow through the cold layer of the heat exchanger is perpendicular to an axis of the environmental control system;
the first inlet extends along a first inlet axis parallel to the axis of the environmental control system; and
the second inlet extends on a second inlet axis parallel to the axis of the environmental control system and the first inlet axis;

a power turbine fluidly connected to the first inlet of the inlet plenum;
a ram air inlet that is fluidly connected to a source of ambient air, wherein the ram air inlet is fluidly connected to the second inlet of the inlet plenum; and
a water extractor fluidly connected to the heat exchanger.

11. The environmental control system of claim 10 , further comprising a nozzle disposed in the inlet plenum, wherein the nozzle is fluidly connected to the water extractor and is configured to disperse water from the water extractor into air passing through the inlet plenum.

12. The environmental control system of claim 10 , wherein the heat exchanger comprises a bleed air heat exchanger, a fresh air heat exchanger, and a chiller heat exchanger, wherein the chiller, fresh air, and bleed air heat exchangers are brazed together to form a single unitized tri-heat exchanger.

13. The environmental control system of claim 10 , wherein the inlet plenum further comprises a sidewall opposite the outlet, wherein the sidewall includes a tapered contour configured to direct a flow of fluid from the second inlet towards the outlet.

14. A method of transferring thermal energy in an environmental control system, the method comprising:
passing a first stream of cool air through a first inlet of a housing of an inlet plenum of a heat exchanger assembly of the environmental control system;
passing a second stream of cool air through a second inlet of the inlet plenum, wherein:
the first and second inlets are disposed in a portion of the inlet plenum;
the first and second inlets are fluidly connected to an outlet;
a direction of airflow through the cold layer of the heat exchanger is perpendicular to an axis of the environmental control system;
the first inlet extends along a first inlet axis parallel to the axis of the environmental control system; and
the second inlet extends on a second inlet axis parallel to the axis of the environmental control system and the first inlet axis;

combining the first stream of cool air and the second stream of cool air into a mixed cool air stream;
directing, with the housing, the mixed cool air stream to the outlet of the inlet plenum that is fluidly connected to an inlet face of a cold layer of the heat exchanger assembly; and
transferring thermal energy from a hot layer of the heat exchanger assembly to the mixed cool air stream.

15. The method of claim 14 , further comprising drawing the second air stream from a ram air circuit.

16. The method of claim 14 , further comprising drawing the first air stream from a power turbine of the environmental control system.

17. The method of claim 14 , further comprising dispersing a cooling fluid into the inlet plenum housing via a nozzle that is mounted in the inlet plenum housing.

18. The method of claim 14 , wherein directing the mixed air stream to an ou

Assignees

• Hamilton Sundstrand Corp

Inventors

• Mccord Patrick
• Tokas Christopher
• Army Donald E

Classifications

• Y02T50/50

  On board measures aiming to increase energy efficiency · CPC title

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title

• F28F9/0207

  the longitudinal or transversal partitions being separate elements attached to header boxes (F28F9/0212, F28F9/0217 take precedence) · CPC title

• B64D2013/0648

  with energy recovery means, e.g. using turbines · CPC title

• F28F9/02

  Header boxes; End plates · CPC title